WEBVTT

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JUDY HOYT: Go ahead
and get started.

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We want to start with
looking at the schedule,

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get ourselves reoriented.

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This is November 16.

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And we'll have our final
lecture today on chapter 9.

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Chapter 9 has three lectures.

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We'll talk about modeling
the topography of deposition.

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And you're working on--
hopefully everybody's working

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on homework number five.

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That homework is due
next lecture on the 18th.

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And does anybody have any
questions on the homework?

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Or if you do, make sure
you see me after class

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or send me an email.

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In addition to the
homework, everyone

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has now-- except one person on
the clipboard-- has a topic.

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And I had my
assistant type it up.

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I'll put it on the web.

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Everybody's signed up
for a final report topic.

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And you can verify
that she got it right.

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And then if you're doing
an oral presentation,

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this week I'll start
making up a schedule

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so you know which day
you're going to speak.

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OK.

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So hopefully everybody
recovered from the snowstorm

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we had over the weekend.

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And we'll go ahead
and start this lecture

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with handout number 32.

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As I mentioned, this is the
final lecture on chapter 9.

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So far we've by way of
thin film deposition

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and epitaxy we've talked
at least a little bit

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about silicon epitaxial growth.

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We discussed the low pressure
chemical vapor deposition

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of the three most important
films in front end processing.

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That's polysilicon, oxide,
low temperature oxide,

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and silicon nitride.

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And we introduced some PVD
techniques such as sputtering.

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We talked about systems
for DC and RF sputtering,

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which is the most commonly used
PVD technique in modern fabs.

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The nice thing
about it is it can

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be adjusted to give
reasonably good step coverage.

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This is in contrast
to evaporation.

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And thermal evaporation
is typically

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not used in CMOS processing.

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Today, what I want
to talk about,

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though, is modeling
of these processes.

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And you'll see how these models
are a little bit different.

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They're much more
quasi-empirical than the models

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we had for ion implantation.

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But there are methods to do
modeling of these processes.

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And we'll give a couple
of specific examples.

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OK, let's go on
to slide number 2.

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Within the last 10 to
15 years ago or so,

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there have been a number
of simulation tools

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have been developed for
topography simulation.

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Now, I want to make clear,
topography simulation

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is not what SUPREM-IV does.

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You've all been using SUPREM-IV
to model ion implantation,

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oxidation, diffusion, a lot
of the front end processing.

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SUPREM-IV doesn't have
any topography simulation

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of any sort.

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If you tell it to
make an etch, it

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assumes it's etched
at a certain angle.

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You tell it the angle.

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It doesn't make any effort
to calculate those angles.

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Or if you tell it that
something is deposited,

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it assumes
conformable deposition

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unless you say otherwise.

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So it's not a simulator
for topography.

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There are other simulators.

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And one of the ones that
also came out of Stanford

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is called SPEEDIE.

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And there are some
examples in this lecture

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from the SPEEDIE simulator
and from in your textbook.

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OK, so what is it that we
need to think about if we want

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to do topography simulation?

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Let's say we are trying to model
the topography of deposition

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of some film.

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This particular
example on slide 2

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is shown assuming we're
doing deposition of aluminum,

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say, in a sputtering chamber.

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And this is the
surface that we're

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depositing the aluminum,
for instance, onto.

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That surface has some
starting initial topography.

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Well, this is a
generalized picture

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of what's involved
in the deposition.

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And you'll see that
modeling topography ends up

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being a lot of bookkeeping of
the different fluxes involved.

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In general, we are not going
to consider gas phase boundary

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layer in these simple models.

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So this picture will
not be accurate,

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for example,
atmospheric pressure

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CVD where diffusion
through a boundary layer

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is very important.

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We're not taking
that into account.

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But it will be reasonably useful
for modeling low pressure CVD

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or for modeling sputtering,
which also takes place

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at reasonably low pressures.

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So these are the
fluxes involved.

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For example, if we're depositing
aluminum on this surface,

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we have a direct flux to the
surface of neutral aluminum

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atoms.

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We also have a
direct flux of ions

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that we need to keep track of.

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Aluminum can come down
and it can actually--

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we can have a desorb.

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It can desorb aluminum
that had already

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been deposited at a point.

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And then we have a
desorbed or emitted flux

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that can be redeposited
elsewhere on the surface.

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So that's a flux we
need to take account of.

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Argon ions, because again this
is in the sputtering system,

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argon is nominally supposed to
be directed towards the target,

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not towards the wafer.

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But it's possible that
it would be directed

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towards the wafer,
argon ion, some of them,

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and that they would sputter
off aluminum that had already

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been deposited.

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And then that can
redeposit elsewhere.

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And there's a surface
diffusion flux.

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Aluminum can diffuse
along the surface

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a certain distance and then
deposit at a different point.

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So we end up just doing
a lot of bookkeeping

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on all the different fluxes.

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And it'd be good if you
think about this picture

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because we're going to use
the exact same picture when

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we talk about etching.

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When you think about
it in this terminology,

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etching is sort of
just the opposite.

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Instead of depositing,
we're talking about fluxes

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coming down and reacting
and removing films.

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But it's not that
much difference.

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It's mathematically the
inverse of deposition.

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So in order to simulate
that process that I just

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showed on slide 3
here, we need some kind

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of mathematical description
of all of these fluxes.

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And then we need
to add them all up

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and see what we get
at any given point.

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So what we write is
this equation shown

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at the top of slide 3 that we
say the net flux at any point

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I.

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So point I, point I is
just-- if I go back one,

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point I is just at some
point on the surface.

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It could be at this
point right here.

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It could be at that
point right there.

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It's just at some
point on the surface.

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The net flux is,
well, it's the flux

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deposited at that
point minus everything

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that was emitted, right?

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And that gives you the total
atoms per square centimeter

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per unit time.

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So you add up the direct flux
of neutrals, the direct flux

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of ions, any flux that's
redeposited that's coming off

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from another area,
any flux that's

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due to surface diffusion.

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All of those are positive terms.

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You subtract off any flux
that's emitted from that point,

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any flux that diffuses out or
that sputter from that point

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by virtue of argon ions
coming down or something.

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So you can see, this is
going to amount to basically

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a lot of bookkeeping.

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And this is something
that computers

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are very good at doing.

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And you can and you
can model those fluxes

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across the surface.

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So usually, what we need to
do for a specific system--

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let' say you're doing
LPCVD or something--

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we have to figure out which one
of these fluxes is important

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and ignore all the
others so we can simplify

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the models to a certain extent.

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And this picture
gives you a rough idea

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of how we do the modeling.

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What we consider is we draw
this dashed line here right

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above the surface of the wafer.

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And so it's a plane
just above the surface.

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And the first thing
we need to look at

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is what's the arrival angle
distribution of atoms and ions

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that are coming
down on that plane?

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And then later on,
the next step will

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take into account topography.

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So first, you do it assuming
you have a plane just

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above the surface.

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And now what we need
to take into account

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are these direct
flux of neutrals

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and the direct flux of ions.

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These we generally
model with some kind

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of arrival angle distribution
just above the wafer.

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And I've noted here
what it says is

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it doesn't model the equipment.

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What that means is you have
to put in the arrival angle

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distribution.

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You can't say to the
simulator, oh, yes, I

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have an applied materials
sputtering tool in the endura,

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and now tell me what
it's going to look like.

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It doesn't have that
level of knowledge

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of the individual tools.

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What you do is you put
in flux, the direct flux,

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as a function of the
angle theta and that's

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measured with respect
to the normal.

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And you give it usually--

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it's some normal flux times a
cosine theta to the n power.

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So that's a variable that you
need to put into the simulator.

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But there are some guidelines
for different systems,

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different types of
systems, what kind

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of arrival angle distribution
for neutrals and ions

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you might use.

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So let's look at a
couple different types

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of flux distributions.

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The first one here shown
on the slide number 4

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is what we call
isotropic flux arrival.

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As the name suggests, the
flux is essentially isotropic.

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And in this we use an n equals
1 in the formula of cosine theta

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to the n.

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So what we get is
that the direct flux

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f as a function of angle theta.

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So if theta is measured
with respect to the normal,

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is whatever the flux is in
the normal direction f0.

00:09:35.900 --> 00:09:41.660 align:middle line:84%
So it's this flux number here
times cosine of theta to the n.

00:09:41.660 --> 00:09:44.210 align:middle line:84%
So what's happening is
I'm moving from normal.

00:09:44.210 --> 00:09:46.250 align:middle line:90%
I have a certain flux in.

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And as I go this
direction, as I coming in

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at shallower and
shallower angles,

00:09:51.520 --> 00:09:55.010 align:middle line:84%
the flux goes down according
to this cosine theta.

00:09:55.010 --> 00:09:58.820 align:middle line:84%
And this little derivation
that I've shown mathematically,

00:09:58.820 --> 00:10:01.370 align:middle line:84%
the second half of
slide 4 kind of explains

00:10:01.370 --> 00:10:03.140 align:middle line:90%
where that comes from.

00:10:03.140 --> 00:10:05.660 align:middle line:84%
What we're interested in when
we're looking at deposition,

00:10:05.660 --> 00:10:10.520 align:middle line:84%
we're interested in the normal
component of the flux, OK?

00:10:10.520 --> 00:10:12.710 align:middle line:84%
So let's say this is
my wafer down here.

00:10:12.710 --> 00:10:17.150 align:middle line:84%
This solid line here represents
the wafer or the surface

00:10:17.150 --> 00:10:18.570 align:middle line:90%
that I'm depositing on.

00:10:18.570 --> 00:10:21.230 align:middle line:84%
And if we look at this
little red region,

00:10:21.230 --> 00:10:23.390 align:middle line:84%
that represents a certain
normal flux coming.

00:10:23.390 --> 00:10:25.580 align:middle line:90%
And that would be my f super 0.

00:10:25.580 --> 00:10:28.760 align:middle line:84%
And this, I'm drawing this
for the n equals 1 case.

00:10:28.760 --> 00:10:32.360 align:middle line:84%
So I have a certain flux
coming in normal in normal.

00:10:32.360 --> 00:10:36.110 align:middle line:84%
Now, at some other angle
theta I have that same flux.

00:10:36.110 --> 00:10:38.280 align:middle line:84%
You notice I drew those
same number of arrows.

00:10:38.280 --> 00:10:43.340 align:middle line:84%
So it's coming in this direction
normal to this plane here,

00:10:43.340 --> 00:10:44.330 align:middle line:90%
normal to this plane.

00:10:44.330 --> 00:10:47.870 align:middle line:84%
I have the same number of atoms
per square centimeter per unit

00:10:47.870 --> 00:10:49.200 align:middle line:90%
time.

00:10:49.200 --> 00:10:53.430 align:middle line:84%
But I need to project that
now onto this surface.

00:10:53.430 --> 00:10:58.580 align:middle line:84%
So when I project this
distance here of length l

00:10:58.580 --> 00:11:01.790 align:middle line:84%
onto the surface, I have
this sort of distance--

00:11:01.790 --> 00:11:06.910 align:middle line:84%
it's spread out over
a lateral dimension h.

00:11:06.910 --> 00:11:09.340 align:middle line:84%
Now, we have right triangles
here with angle theta

00:11:09.340 --> 00:11:12.160 align:middle line:90%
here and theta here.

00:11:12.160 --> 00:11:13.690 align:middle line:84%
And you can write--
it's very simply

00:11:13.690 --> 00:11:15.640 align:middle line:84%
that the cosine
of the angle theta

00:11:15.640 --> 00:11:20.180 align:middle line:84%
is just this distance l
divided by the distance h,

00:11:20.180 --> 00:11:22.870 align:middle line:84%
where h represents how
far that unit flux is

00:11:22.870 --> 00:11:27.240 align:middle line:90%
spread across the wafer.

00:11:27.240 --> 00:11:28.860 align:middle line:84%
OK, so now it's
just bookkeeping.

00:11:28.860 --> 00:11:33.300 align:middle line:84%
If I want to know what is
the flux here in this region,

00:11:33.300 --> 00:11:35.700 align:middle line:84%
it's just a number per
unit area per unit time

00:11:35.700 --> 00:11:40.170 align:middle line:84%
that's going to be proportional
to the number per unit

00:11:40.170 --> 00:11:43.350 align:middle line:84%
time divided by h,
right, because it's

00:11:43.350 --> 00:11:45.210 align:middle line:90%
spread out over the distance h.

00:11:45.210 --> 00:11:51.480 align:middle line:84%
But you can substitute in
for h is cosine theta over l

00:11:51.480 --> 00:11:54.370 align:middle line:84%
or l over cosine theta, Right
so you can substitute that in.

00:11:54.370 --> 00:11:57.120 align:middle line:84%
So you get the fact
that for isotropic,

00:11:57.120 --> 00:12:00.600 align:middle line:84%
so assuming you have just as
much intensity in this red bar

00:12:00.600 --> 00:12:05.790 align:middle line:84%
as I had in this direction
theta in the black bar,

00:12:05.790 --> 00:12:08.940 align:middle line:84%
assuming that, then I get
this simple formula, which

00:12:08.940 --> 00:12:10.980 align:middle line:84%
shows that the flux
as a function of theta

00:12:10.980 --> 00:12:15.150 align:middle line:84%
is just the normal flux
times the cosine of theta.

00:12:15.150 --> 00:12:18.690 align:middle line:84%
And that's assuming that the
source is isotropic like this.

00:12:18.690 --> 00:12:20.460 align:middle line:84%
If for some reason
your source varies,

00:12:20.460 --> 00:12:21.990 align:middle line:84%
and you have much
greater intensity

00:12:21.990 --> 00:12:23.910 align:middle line:84%
over here and over
here or whatever,

00:12:23.910 --> 00:12:26.040 align:middle line:84%
this cosine theta
term will be modified.

00:12:26.040 --> 00:12:32.340 align:middle line:84%
But again, this is assuming
isotropic, an isotropic source.

00:12:32.340 --> 00:12:35.773 align:middle line:84%
And the cosine theta just
comes from the geometry factor.

00:12:35.773 --> 00:12:38.190 align:middle line:84%
OK, you can sit down and stare
at that for a little while.

00:12:38.190 --> 00:12:41.900 align:middle line:84%
Hopefully, it'll
make sense to you.

00:12:41.900 --> 00:12:44.000 align:middle line:90%
Go to slide 5.

00:12:44.000 --> 00:12:46.700 align:middle line:84%
So in contrast to
that, on the left side

00:12:46.700 --> 00:12:49.130 align:middle line:84%
I show what I just derived,
which is the isotropic flux

00:12:49.130 --> 00:12:50.660 align:middle line:90%
arrival distribution.

00:12:50.660 --> 00:12:53.000 align:middle line:84%
On the right side,
for some systems

00:12:53.000 --> 00:12:55.340 align:middle line:84%
you may have very
anisotropic flux.

00:12:55.340 --> 00:12:57.410 align:middle line:84%
Most of the atoms
or ions coming down

00:12:57.410 --> 00:12:59.660 align:middle line:84%
may be directed mostly
normal to the surface.

00:12:59.660 --> 00:13:02.210 align:middle line:84%
There may be very few
coming out at shallow angles

00:13:02.210 --> 00:13:04.980 align:middle line:84%
depending on the particular
machine that you're using.

00:13:04.980 --> 00:13:07.400 align:middle line:84%
So here in the cosine
theta to the n,

00:13:07.400 --> 00:13:08.618 align:middle line:90%
we make n greater than 1.

00:13:08.618 --> 00:13:10.160 align:middle line:84%
And you can see just
based on the way

00:13:10.160 --> 00:13:12.140 align:middle line:84%
these arrows are
distributed most of them

00:13:12.140 --> 00:13:13.160 align:middle line:90%
are coming in normal.

00:13:13.160 --> 00:13:16.340 align:middle line:84%
The flux coming in at
angles, higher angles theta,

00:13:16.340 --> 00:13:17.213 align:middle line:90%
is much smaller.

00:13:17.213 --> 00:13:19.130 align:middle line:84%
You can see that from
the length of the arrow.

00:13:19.130 --> 00:13:20.810 align:middle line:84%
So the length of
these arrows here

00:13:20.810 --> 00:13:26.320 align:middle line:84%
is supposed to represent
the flux at any given angle.

00:13:26.320 --> 00:13:28.680 align:middle line:84%
So generally, we have this
arrival angle distribution

00:13:28.680 --> 00:13:30.390 align:middle line:90%
at a plane just above the wafer.

00:13:30.390 --> 00:13:34.530 align:middle line:84%
It has some cosine theta to
the n type of dependence.

00:13:34.530 --> 00:13:36.300 align:middle line:84%
And again, it's the
normal component,

00:13:36.300 --> 00:13:39.060 align:middle line:84%
normal to the surface, that
strikes the surface that

00:13:39.060 --> 00:13:40.485 align:middle line:90%
determines the deposition rate.

00:13:40.485 --> 00:13:44.850 align:middle line:90%


00:13:44.850 --> 00:13:50.000 align:middle line:84%
So let's take a look at examples
of distribution of flux arrival

00:13:50.000 --> 00:13:52.410 align:middle line:90%
distribution functions.

00:13:52.410 --> 00:13:55.220 align:middle line:84%
Here's that formula
I just mentioned.

00:13:55.220 --> 00:13:59.360 align:middle line:84%
And for example, if you
have a high pressure system,

00:13:59.360 --> 00:14:00.980 align:middle line:84%
reasonably high
pressure, you're going

00:14:00.980 --> 00:14:04.010 align:middle line:84%
to have a lot of gas phase
collisions, which means you

00:14:04.010 --> 00:14:05.420 align:middle line:90%
have a short mean free path.

00:14:05.420 --> 00:14:07.730 align:middle line:84%
And you're going to tend
to get isotropic arrival

00:14:07.730 --> 00:14:09.590 align:middle line:84%
because those atoms are
all bouncing around.

00:14:09.590 --> 00:14:11.450 align:middle line:84%
And regardless of where
they're coming from,

00:14:11.450 --> 00:14:12.992 align:middle line:84%
it's just sort of
the flux is equally

00:14:12.992 --> 00:14:15.290 align:middle line:90%
distributed for all angles.

00:14:15.290 --> 00:14:17.870 align:middle line:84%
If you're in a very
low pressure system

00:14:17.870 --> 00:14:21.920 align:middle line:84%
where you have very fewer
gas phase collisions, a long

00:14:21.920 --> 00:14:24.628 align:middle line:84%
the mean free path, and is
going to be closer to 1,

00:14:24.628 --> 00:14:26.420 align:middle line:84%
you're going to get
more like line of sight

00:14:26.420 --> 00:14:28.745 align:middle line:84%
from the source, whatever
that source happens to be.

00:14:28.745 --> 00:14:29.870 align:middle line:90%
It could be a point source.

00:14:29.870 --> 00:14:31.820 align:middle line:84%
It could be a plane
if it's sputtering.

00:14:31.820 --> 00:14:35.600 align:middle line:84%
But you're going to
have n greater than 1.

00:14:35.600 --> 00:14:36.860 align:middle line:90%
That's all assuming neutrals.

00:14:36.860 --> 00:14:39.553 align:middle line:84%
If you have ionic species
and the wafer is biased,

00:14:39.553 --> 00:14:41.720 align:middle line:84%
imagine the wafer has some
bias and you have an ion,

00:14:41.720 --> 00:14:44.690 align:middle line:84%
the ion can be attracted to
it by the electric field,

00:14:44.690 --> 00:14:45.680 align:middle line:90%
OK, that's set up.

00:14:45.680 --> 00:14:47.510 align:middle line:84%
In that case, for
ionized species,

00:14:47.510 --> 00:14:50.750 align:middle line:84%
it tends to be very anisotropic
because, again, there's

00:14:50.750 --> 00:14:53.420 align:middle line:84%
a force driving it
towards the wafer

00:14:53.420 --> 00:14:56.570 align:middle line:84%
so it doesn't tend
to bounce around.

00:14:56.570 --> 00:14:58.670 align:middle line:84%
The species tend to
go right to the wafer.

00:14:58.670 --> 00:15:02.640 align:middle line:84%
So these are just some
examples of flux distribution

00:15:02.640 --> 00:15:07.180 align:middle line:84%
so you can see what it looks
like for different values of n

00:15:07.180 --> 00:15:08.960 align:middle line:90%
So this is the relative flux.

00:15:08.960 --> 00:15:12.070 align:middle line:84%
So it's the flux
at any given angle

00:15:12.070 --> 00:15:16.570 align:middle line:84%
theta divided by the
normal flux, divided by f0.

00:15:16.570 --> 00:15:17.930 align:middle line:90%
And this is what it looks like.

00:15:17.930 --> 00:15:20.080 align:middle line:84%
So it starts here
at theta equals 0.

00:15:20.080 --> 00:15:22.270 align:middle line:90%
So that's normal is one.

00:15:22.270 --> 00:15:24.580 align:middle line:84%
And you can see for n
equals 1 it drops down

00:15:24.580 --> 00:15:26.020 align:middle line:90%
and the flux finally goes to 0.

00:15:26.020 --> 00:15:28.270 align:middle line:84%
At 90 degrees, you're just
skimming along the surface.

00:15:28.270 --> 00:15:31.060 align:middle line:84%
Obviously, the normal
component is 0.

00:15:31.060 --> 00:15:35.095 align:middle line:84%
n equals 3, which is
slight anisotropy.

00:15:35.095 --> 00:15:36.315 align:middle line:90%
It looks something like this.

00:15:36.315 --> 00:15:38.440 align:middle line:84%
It's starting to flux really
dies down dramatically

00:15:38.440 --> 00:15:39.790 align:middle line:90%
after 60 degrees.

00:15:39.790 --> 00:15:44.500 align:middle line:84%
n equals 15, which could be
appropriate for some ionized

00:15:44.500 --> 00:15:46.990 align:middle line:84%
deposition systems, you
can see really the flux

00:15:46.990 --> 00:15:49.340 align:middle line:84%
goes to 0 by the time you
get to about 30 degrees.

00:15:49.340 --> 00:15:54.680 align:middle line:84%
So it's very anisotropic
arrival at that plane.

00:15:54.680 --> 00:15:58.487 align:middle line:84%
And again, in most models,
these are inputs that--

00:15:58.487 --> 00:15:59.695 align:middle line:90%
parameters that you can vary.

00:15:59.695 --> 00:16:03.200 align:middle line:90%


00:16:03.200 --> 00:16:05.930 align:middle line:84%
OK, so that gives us an
idea of the direct fluxes

00:16:05.930 --> 00:16:07.880 align:middle line:90%
and their angular dependence.

00:16:07.880 --> 00:16:11.300 align:middle line:84%
The next thing we have to
do is to take into account

00:16:11.300 --> 00:16:13.040 align:middle line:90%
the surface topography.

00:16:13.040 --> 00:16:15.560 align:middle line:84%
And just to give you
an example of that,

00:16:15.560 --> 00:16:18.060 align:middle line:84%
I'm showing here-- imagine
your surface is not flat,

00:16:18.060 --> 00:16:21.050 align:middle line:84%
but that you have a wafer and
you are sputtering aluminum

00:16:21.050 --> 00:16:24.260 align:middle line:84%
into it and you have a via or
you have a hole, contact hole.

00:16:24.260 --> 00:16:27.500 align:middle line:84%
So it's like this, and then
you have this hole right here.

00:16:27.500 --> 00:16:32.480 align:middle line:84%
Well if you have imagined each
one of these little regions

00:16:32.480 --> 00:16:35.900 align:middle line:84%
corresponds to an emitter
with a certain flux,

00:16:35.900 --> 00:16:40.190 align:middle line:84%
depending at any point i
on this vertical surface,

00:16:40.190 --> 00:16:42.770 align:middle line:84%
it's going to have a
certain viewing angle.

00:16:42.770 --> 00:16:44.750 align:middle line:84%
And if you're beyond
that viewing angle,

00:16:44.750 --> 00:16:46.040 align:middle line:90%
you're going to be shadowed.

00:16:46.040 --> 00:16:49.940 align:middle line:84%
So this is a shadowing effect
on the sidewall of the trench.

00:16:49.940 --> 00:16:53.210 align:middle line:84%
It's not that uncommon depending
on the depth and the aspect

00:16:53.210 --> 00:16:56.532 align:middle line:90%
ratio of the trench.

00:16:56.532 --> 00:16:58.490 align:middle line:84%
So we have to take into
account the orientation

00:16:58.490 --> 00:17:01.310 align:middle line:84%
of the surface, what
its angle is, this

00:17:01.310 --> 00:17:03.920 align:middle line:90%
viewing angle, and shadowing.

00:17:03.920 --> 00:17:09.530 align:middle line:84%
And typically, in the near
certain way for surface region

00:17:09.530 --> 00:17:13.760 align:middle line:84%
we will neglect the gas
phase collisions on that.

00:17:13.760 --> 00:17:16.160 align:middle line:84%
So if you will, you
can think of this--

00:17:16.160 --> 00:17:18.450 align:middle line:90%
imagine my reference plane.

00:17:18.450 --> 00:17:21.230 align:middle line:84%
Remember that reference
plane is sort of a plane just

00:17:21.230 --> 00:17:23.579 align:middle line:90%
above the wafer surface.

00:17:23.579 --> 00:17:27.260 align:middle line:84%
And each small area on
this reference plane

00:17:27.260 --> 00:17:29.730 align:middle line:84%
can be treated as
an emission source.

00:17:29.730 --> 00:17:32.390 align:middle line:84%
So if you have a
emission coming down,

00:17:32.390 --> 00:17:35.990 align:middle line:84%
you have all these
little emission sources.

00:17:35.990 --> 00:17:40.250 align:middle line:84%
And each source is emitting
to the topography below it.

00:17:40.250 --> 00:17:44.330 align:middle line:84%
And then the total direct
flux at any point i

00:17:44.330 --> 00:17:46.070 align:middle line:84%
can be calculated
by just adding up

00:17:46.070 --> 00:17:48.920 align:middle line:84%
the flux from each one of
these little miniature emission

00:17:48.920 --> 00:17:52.370 align:middle line:84%
sources, which each one of
which has its certain angular

00:17:52.370 --> 00:17:55.100 align:middle line:84%
distribution depending
on the type of system

00:17:55.100 --> 00:17:58.330 align:middle line:90%
that you're modeling.

00:17:58.330 --> 00:18:00.940 align:middle line:84%
So you can now begin to
see how in a computer model

00:18:00.940 --> 00:18:03.640 align:middle line:84%
you can build
equations and you can

00:18:03.640 --> 00:18:06.130 align:middle line:84%
build structures that
would be able to model

00:18:06.130 --> 00:18:09.360 align:middle line:90%
this type of deposition.

00:18:09.360 --> 00:18:10.490 align:middle line:90%
Let's go on to slide 8.

00:18:10.490 --> 00:18:12.900 align:middle line:84%
And I'd wanted to give
you a practical example.

00:18:12.900 --> 00:18:14.983 align:middle line:84%
We're talking about all
these mathematical things.

00:18:14.983 --> 00:18:19.610 align:middle line:84%
But a practical example, which
should be somewhat intuitive,

00:18:19.610 --> 00:18:22.310 align:middle line:84%
here on slide 8 is the impact
of having a finite target

00:18:22.310 --> 00:18:25.940 align:middle line:84%
size compared to the
wafer and if you're

00:18:25.940 --> 00:18:30.040 align:middle line:84%
doing sputter deposition on
asymmetry across a wafer.

00:18:30.040 --> 00:18:31.540 align:middle line:84%
So if you look at
this illustration,

00:18:31.540 --> 00:18:34.240 align:middle line:84%
imagine I have a target
that I'm doing sputtering.

00:18:34.240 --> 00:18:35.470 align:middle line:90%
And this could be aluminum.

00:18:35.470 --> 00:18:36.350 align:middle line:90%
And it's up here.

00:18:36.350 --> 00:18:38.110 align:middle line:90%
It has this dimension.

00:18:38.110 --> 00:18:40.270 align:middle line:84%
It's relatively small
compared to, say,

00:18:40.270 --> 00:18:43.240 align:middle line:90%
I'm doing a 6 or 8 inch wafer.

00:18:43.240 --> 00:18:44.800 align:middle line:90%
So what's going to happen?

00:18:44.800 --> 00:18:46.570 align:middle line:84%
And you have the
wafer sitting there,

00:18:46.570 --> 00:18:49.150 align:middle line:84%
and you're sputtering into
a trench on the left side

00:18:49.150 --> 00:18:51.430 align:middle line:84%
of the wafer, and you
have a dye over here

00:18:51.430 --> 00:18:52.780 align:middle line:90%
on the right side of the wafer.

00:18:52.780 --> 00:18:55.360 align:middle line:84%
And let's say for now
you're not rotating

00:18:55.360 --> 00:18:56.587 align:middle line:90%
the wafers or anything.

00:18:56.587 --> 00:18:59.170 align:middle line:84%
So you can imagine what's going
to happen here on this trench.

00:18:59.170 --> 00:19:02.030 align:middle line:84%
This white region indicates the
region that you've sputtered,

00:19:02.030 --> 00:19:03.280 align:middle line:90%
the material you've sputtered.

00:19:03.280 --> 00:19:06.400 align:middle line:84%
You get an asymmetry
on the sidewall

00:19:06.400 --> 00:19:08.560 align:middle line:84%
because you've got here
at this point in the wafer

00:19:08.560 --> 00:19:11.623 align:middle line:84%
you have more flux coming
from this direction.

00:19:11.623 --> 00:19:12.790 align:middle line:90%
And so you're going to get--

00:19:12.790 --> 00:19:14.320 align:middle line:84%
because of shadowing
you're going to not get

00:19:14.320 --> 00:19:15.700 align:middle line:90%
much deposition on this wall.

00:19:15.700 --> 00:19:16.923 align:middle line:90%
You'll get more on this wall.

00:19:16.923 --> 00:19:18.340 align:middle line:84%
On the right side
of the wafer, we

00:19:18.340 --> 00:19:21.670 align:middle line:84%
have just the opposite
type of shadowing.

00:19:21.670 --> 00:19:24.630 align:middle line:84%
So you will tend to get
asymmetric deposition

00:19:24.630 --> 00:19:26.820 align:middle line:84%
on the left side of
the wafer as opposed

00:19:26.820 --> 00:19:29.590 align:middle line:84%
to the right side of the wafer
with this particular geometry.

00:19:29.590 --> 00:19:31.740 align:middle line:84%
So what do people
do in a real system?

00:19:31.740 --> 00:19:33.480 align:middle line:84%
Because obviously
this is not desirable.

00:19:33.480 --> 00:19:34.417 align:middle line:90%
We want to have it--

00:19:34.417 --> 00:19:36.250 align:middle line:84%
each side of the wafer
should look the same.

00:19:36.250 --> 00:19:38.220 align:middle line:84%
Well you can widen
the target size.

00:19:38.220 --> 00:19:40.500 align:middle line:84%
So I can take this target
and make it much bigger,

00:19:40.500 --> 00:19:43.690 align:middle line:90%
make it larger than the wafer.

00:19:43.690 --> 00:19:45.610 align:middle line:84%
Or you can take the
same size target

00:19:45.610 --> 00:19:48.700 align:middle line:84%
and move it further
from the wafer.

00:19:48.700 --> 00:19:52.300 align:middle line:84%
So in either case, you're
going to get an arrival angle

00:19:52.300 --> 00:19:56.890 align:middle line:84%
distribution that is more
symmetric across the wafer.

00:19:56.890 --> 00:19:59.900 align:middle line:84%
Another thing people sometimes
do is to rotate the wafers.

00:19:59.900 --> 00:20:01.450 align:middle line:84%
So you can put the
wafers on a plate

00:20:01.450 --> 00:20:03.820 align:middle line:84%
and that rotates with
respect to the source, which

00:20:03.820 --> 00:20:06.160 align:middle line:84%
is essentially similar
to widening, increasing

00:20:06.160 --> 00:20:08.080 align:middle line:84%
the effective size
of your target.

00:20:08.080 --> 00:20:10.717 align:middle line:84%
This is why sputtering systems
are very large because they

00:20:10.717 --> 00:20:11.800 align:middle line:90%
tend to have huge targets.

00:20:11.800 --> 00:20:14.380 align:middle line:84%
Imagine today people were
processing 6 inch wafers--

00:20:14.380 --> 00:20:15.070 align:middle line:90%
not 6 inch.

00:20:15.070 --> 00:20:16.780 align:middle line:84%
Here at MTL we're
processing 6 inch,

00:20:16.780 --> 00:20:18.340 align:middle line:90%
12 inch wafers in industry.

00:20:18.340 --> 00:20:21.040 align:middle line:84%
That target has to
be huge basically.

00:20:21.040 --> 00:20:22.790 align:middle line:84%
And then you would be
rotating the wafers.

00:20:22.790 --> 00:20:24.902 align:middle line:84%
And so this is why the
equipment in the fabs

00:20:24.902 --> 00:20:26.110 align:middle line:90%
is getting larger and larger.

00:20:26.110 --> 00:20:29.020 align:middle line:84%
You're fundamentally limited
by some of these processes

00:20:29.020 --> 00:20:31.190 align:middle line:90%
to obtain uniformity.

00:20:31.190 --> 00:20:33.050 align:middle line:84%
And on slide 9, in
fact, there's just

00:20:33.050 --> 00:20:35.780 align:middle line:84%
an example of how
we would ameliorate

00:20:35.780 --> 00:20:38.332 align:middle line:84%
this asymmetry from the left
and the right side of the wafer.

00:20:38.332 --> 00:20:40.040 align:middle line:84%
Here's an example
where the target's been

00:20:40.040 --> 00:20:41.360 align:middle line:90%
made as large as the wafer.

00:20:41.360 --> 00:20:43.700 align:middle line:84%
In fact, most targets
today are much bigger

00:20:43.700 --> 00:20:44.903 align:middle line:90%
than the size of the wafer.

00:20:44.903 --> 00:20:46.820 align:middle line:84%
And this is also why
they cost a lot of money.

00:20:46.820 --> 00:20:48.080 align:middle line:84%
If you have a
target of platinum,

00:20:48.080 --> 00:20:49.455 align:middle line:84%
if you're sputtering
platinum, it

00:20:49.455 --> 00:20:53.060 align:middle line:84%
has to be 2 feet by 10
inches or something like.

00:20:53.060 --> 00:20:54.140 align:middle line:90%
That's a lot of platinum.

00:20:54.140 --> 00:20:55.920 align:middle line:84%
That's a very large
sheet of platinum.

00:20:55.920 --> 00:20:57.295 align:middle line:84%
So it costs quite
a bit of money.

00:20:57.295 --> 00:20:59.685 align:middle line:84%
Or if you want, instead
of making a target so big

00:20:59.685 --> 00:21:01.310 align:middle line:84%
you can move it
further away and you'll

00:21:01.310 --> 00:21:03.367 align:middle line:84%
get a little better
symmetry between the left

00:21:03.367 --> 00:21:04.700 align:middle line:90%
and the right side of the wafer.

00:21:04.700 --> 00:21:07.250 align:middle line:84%
But that makes the
machine really big.

00:21:07.250 --> 00:21:09.590 align:middle line:84%
And you can only have so
much size in your clean room.

00:21:09.590 --> 00:21:11.340 align:middle line:90%
So they kind of trade offs here.

00:21:11.340 --> 00:21:13.730 align:middle line:84%
So in practice, people
use larger targets

00:21:13.730 --> 00:21:17.150 align:middle line:84%
at some reasonable distance,
and scale the tool size,

00:21:17.150 --> 00:21:21.413 align:middle line:90%
and rotate the wafers to help.

00:21:21.413 --> 00:21:22.580 align:middle line:90%
There's a practical example.

00:21:22.580 --> 00:21:26.920 align:middle line:84%
OK, so we talked about how
to calculate the direct flux.

00:21:26.920 --> 00:21:29.420 align:middle line:84%
Basically, you're just taking--
it's like a geometry problem

00:21:29.420 --> 00:21:30.080 align:middle line:90%
essentially.

00:21:30.080 --> 00:21:32.840 align:middle line:84%
And you have to have a cosine
theta to the end dependence.

00:21:32.840 --> 00:21:34.730 align:middle line:90%
How about the indirect flux?

00:21:34.730 --> 00:21:37.220 align:middle line:84%
First of all, on slide 10,
what do I mean by indirect?

00:21:37.220 --> 00:21:40.370 align:middle line:84%
Well, I mean all those processes
that occur on the surface

00:21:40.370 --> 00:21:43.640 align:middle line:84%
or near the surface of the
wafer during the deposition.

00:21:43.640 --> 00:21:47.400 align:middle line:84%
So these indirect fluxes
include surface diffusion.

00:21:47.400 --> 00:21:51.650 align:middle line:84%
So I could have an aluminum
atom that's that started here.

00:21:51.650 --> 00:21:53.210 align:middle line:84%
But it can diffuse
along the surface

00:21:53.210 --> 00:21:54.720 align:middle line:90%
and end up somewhere else.

00:21:54.720 --> 00:21:57.650 align:middle line:84%
So that represents a
flux to that point.

00:21:57.650 --> 00:22:01.570 align:middle line:84%
Emission, species come down,
but they don't always stick.

00:22:01.570 --> 00:22:03.910 align:middle line:84%
They don't always
stick where they land.

00:22:03.910 --> 00:22:07.110 align:middle line:84%
They might actually go there
and then be re-emitted.

00:22:07.110 --> 00:22:10.320 align:middle line:84%
So that's an indirect
flux called re-emission.

00:22:10.320 --> 00:22:12.750 align:middle line:84%
Sputtering, incoming
atoms can knock off--

00:22:12.750 --> 00:22:15.240 align:middle line:84%
you could have a film of
aluminum already on the wafer,

00:22:15.240 --> 00:22:17.010 align:middle line:84%
but incoming atoms
could knock them off.

00:22:17.010 --> 00:22:20.370 align:middle line:84%
And redeposition,
sputtered atoms

00:22:20.370 --> 00:22:22.090 align:middle line:90%
can be redeposited elsewhere.

00:22:22.090 --> 00:22:23.110 align:middle line:90%
Here's an example.

00:22:23.110 --> 00:22:24.330 align:middle line:90%
Aluminum comes down.

00:22:24.330 --> 00:22:26.160 align:middle line:84%
It hits an aluminum
atom that was already

00:22:26.160 --> 00:22:27.450 align:middle line:90%
deposited on the surface.

00:22:27.450 --> 00:22:33.155 align:middle line:84%
It's then desorbed or emitted
and redeposited down here.

00:22:33.155 --> 00:22:34.530 align:middle line:84%
So there's a number
of processes.

00:22:34.530 --> 00:22:36.655 align:middle line:84%
We call these indirect
because they're not directly

00:22:36.655 --> 00:22:38.458 align:middle line:90%
coming from the source.

00:22:38.458 --> 00:22:40.500 align:middle line:84%
They're coming from other
regions on the surface,

00:22:40.500 --> 00:22:44.945 align:middle line:84%
but that need to be taken into
account in the topography.

00:22:44.945 --> 00:22:46.820 align:middle line:84%
So let's go through each
one of these surface

00:22:46.820 --> 00:22:50.450 align:middle line:84%
processes, the diffusion, and
the redeposition, and things,

00:22:50.450 --> 00:22:53.330 align:middle line:84%
and talk about how
we might model them.

00:22:53.330 --> 00:22:57.860 align:middle line:84%
If we go on to slide 11,
to surface diffusion,

00:22:57.860 --> 00:23:00.467 align:middle line:84%
well, surface diffusion--
and I'll refer to your text.

00:23:00.467 --> 00:23:02.050 align:middle line:84%
I'm not going to
derive this equation.

00:23:02.050 --> 00:23:04.583 align:middle line:84%
But it turns out
diffusion along a surface

00:23:04.583 --> 00:23:06.250 align:middle line:84%
is different from
diffusion in the bulk.

00:23:06.250 --> 00:23:09.220 align:middle line:84%
We spent a lot of time talking
about diffusion in the bulk

00:23:09.220 --> 00:23:12.070 align:middle line:90%
of single crystal silicon.

00:23:12.070 --> 00:23:15.700 align:middle line:84%
Surface diffusion has slightly
different driving forces.

00:23:15.700 --> 00:23:18.310 align:middle line:84%
Not always just
driven by a gradient,

00:23:18.310 --> 00:23:20.920 align:middle line:84%
but it can actually be driven
by the shape of the surface.

00:23:20.920 --> 00:23:22.390 align:middle line:84%
It can actually
be-- diffusion can

00:23:22.390 --> 00:23:25.138 align:middle line:84%
be driven by the local
curvature of the surface,

00:23:25.138 --> 00:23:26.680 align:middle line:84%
if you're depositing
a film, in order

00:23:26.680 --> 00:23:29.210 align:middle line:90%
to minimize surface free energy.

00:23:29.210 --> 00:23:31.570 align:middle line:84%
So we have a different
type of equation

00:23:31.570 --> 00:23:34.600 align:middle line:84%
from what you're used to
seeing perhaps for diffusion.

00:23:34.600 --> 00:23:39.070 align:middle line:84%
We see that if there's a flux
into a point on the surface,

00:23:39.070 --> 00:23:42.430 align:middle line:84%
minus the diffusion flux out,
so that's the net diffusion flux

00:23:42.430 --> 00:23:46.630 align:middle line:84%
to a point, it actually
depends on a surface diffusion

00:23:46.630 --> 00:23:49.720 align:middle line:84%
coefficient d sub
s, diffusivity.

00:23:49.720 --> 00:23:53.667 align:middle line:84%
But it also depends on this
curvature, this derivative,

00:23:53.667 --> 00:23:55.750 align:middle line:84%
which has to do with the
curvature of the surface.

00:23:55.750 --> 00:23:57.178 align:middle line:90%
And what I would do--

00:23:57.178 --> 00:23:59.220 align:middle line:84%
I don't want to go through
it in detail in class.

00:23:59.220 --> 00:24:04.760 align:middle line:84%
But if you look at equation
11.37 in the associated texts,

00:24:04.760 --> 00:24:07.190 align:middle line:84%
in chapter 11, they
talk a little bit more

00:24:07.190 --> 00:24:11.310 align:middle line:84%
about surface diffusion and
where this equation comes from.

00:24:11.310 --> 00:24:15.210 align:middle line:84%
But the main point is because
it increases with curvature

00:24:15.210 --> 00:24:19.140 align:middle line:84%
during deposition, filling in
of corners may be enhanced.

00:24:19.140 --> 00:24:23.340 align:middle line:84%
And you can sometimes get
more smoother, more conformal

00:24:23.340 --> 00:24:23.850 align:middle line:90%
deposition.

00:24:23.850 --> 00:24:26.100 align:middle line:84%
Of course, you have to be
at a high enough temperature

00:24:26.100 --> 00:24:27.480 align:middle line:90%
that these species can diffuse.

00:24:27.480 --> 00:24:30.000 align:middle line:84%
And depending on the
material and the temperature,

00:24:30.000 --> 00:24:31.710 align:middle line:90%
it may not be diffusing.

00:24:31.710 --> 00:24:34.920 align:middle line:84%
You may have to raise the
wafer temperature slightly

00:24:34.920 --> 00:24:37.690 align:middle line:84%
if you want to get
more surface diffusion.

00:24:37.690 --> 00:24:39.310 align:middle line:90%
So you can think of it this way.

00:24:39.310 --> 00:24:41.580 align:middle line:84%
If I raise the
temperature of the wafer,

00:24:41.580 --> 00:24:43.980 align:middle line:84%
I can smooth out and get
a little more conformal

00:24:43.980 --> 00:24:48.640 align:middle line:84%
deposition by virtue of
surface diffusion processes.

00:24:48.640 --> 00:24:50.410 align:middle line:84%
So that's something
that can be modeled

00:24:50.410 --> 00:24:52.930 align:middle line:90%
in topography simulators.

00:24:52.930 --> 00:24:55.700 align:middle line:90%


00:24:55.700 --> 00:24:58.820 align:middle line:84%
Page 12, a little bit
simpler, this is very much

00:24:58.820 --> 00:25:00.350 align:middle line:90%
a bookkeeping thing.

00:25:00.350 --> 00:25:05.240 align:middle line:84%
There's something called
surface sticking and emission

00:25:05.240 --> 00:25:07.650 align:middle line:90%
and a sticking coefficient.

00:25:07.650 --> 00:25:09.830 align:middle line:84%
So there's this flux
at any given point

00:25:09.830 --> 00:25:14.030 align:middle line:84%
i that's emitted that arises
because not all molecules stick

00:25:14.030 --> 00:25:15.900 align:middle line:90%
when they arrive at the surface.

00:25:15.900 --> 00:25:19.820 align:middle line:84%
And so in fact, we write the
emitted flux from any point

00:25:19.820 --> 00:25:23.510 align:middle line:84%
as being equal to
1 minus s sub c.

00:25:23.510 --> 00:25:26.450 align:middle line:84%
So the fraction emitted
is 1 minus s sub c,

00:25:26.450 --> 00:25:28.490 align:middle line:84%
where s sub c is called
a sticking coefficient,

00:25:28.490 --> 00:25:31.180 align:middle line:90%
times the flux going in.

00:25:31.180 --> 00:25:32.770 align:middle line:90%
So what is s sub c.

00:25:32.770 --> 00:25:34.610 align:middle line:90%
Well, it's a very simple thing.

00:25:34.610 --> 00:25:36.880 align:middle line:84%
It's the fraction
that stick basically.

00:25:36.880 --> 00:25:39.580 align:middle line:84%
So sticking coefficient
here, s sub c,

00:25:39.580 --> 00:25:41.740 align:middle line:84%
it's the flux that
react and stay

00:25:41.740 --> 00:25:45.230 align:middle line:84%
put divided by the
total incident flux.

00:25:45.230 --> 00:25:50.610 align:middle line:84%
So to give yourself an idea,
if you have a high s sub c--

00:25:50.610 --> 00:25:52.630 align:middle line:84%
s sub c is a number
between 0 and 1

00:25:52.630 --> 00:25:54.040 align:middle line:90%
really because it's a fraction.

00:25:54.040 --> 00:25:56.440 align:middle line:84%
If you have a high s sub
c, like s sub c equals 1,

00:25:56.440 --> 00:25:58.390 align:middle line:84%
basically you have line
of sight deposition.

00:25:58.390 --> 00:26:00.760 align:middle line:84%
Everything that comes
down just stops and sticks

00:26:00.760 --> 00:26:01.930 align:middle line:90%
on the surface.

00:26:01.930 --> 00:26:04.030 align:middle line:84%
If you have a type
of deposition with

00:26:04.030 --> 00:26:07.760 align:middle line:84%
a low sticking coefficient,
what happens is atoms come down.

00:26:07.760 --> 00:26:10.450 align:middle line:84%
They may touch the surface,
but they don't stick.

00:26:10.450 --> 00:26:11.290 align:middle line:90%
They don't react.

00:26:11.290 --> 00:26:14.590 align:middle line:84%
They're kind of inert, in which
case they'll be re-emitted.

00:26:14.590 --> 00:26:17.530 align:middle line:84%
They touch somewhere else,
and then they don't react.

00:26:17.530 --> 00:26:19.660 align:middle line:84%
And then finally they
might be emitted and stuck

00:26:19.660 --> 00:26:20.510 align:middle line:90%
at this point.

00:26:20.510 --> 00:26:23.210 align:middle line:84%
So when you have a low
sticking coefficient, much,

00:26:23.210 --> 00:26:26.440 align:middle line:84%
much less than 1-- and sticking
coefficients can be 0.001--

00:26:26.440 --> 00:26:29.260 align:middle line:84%
it means that things bounce
around a lot before they

00:26:29.260 --> 00:26:31.670 align:middle line:90%
actually stick on the surface.

00:26:31.670 --> 00:26:35.060 align:middle line:84%
So you're going to have more
conformal type deposition.

00:26:35.060 --> 00:26:38.200 align:middle line:84%
So this depends a lot on
the deposition system,

00:26:38.200 --> 00:26:39.850 align:middle line:84%
on the temperature,
on the chemistry.

00:26:39.850 --> 00:26:41.230 align:middle line:90%
Again, we don't model all that.

00:26:41.230 --> 00:26:44.110 align:middle line:84%
We don't say, oh, I'm putting
a wafer into an LPCVD system.

00:26:44.110 --> 00:26:48.220 align:middle line:84%
The sticking coefficient
must be 0.01 or 0.1.

00:26:48.220 --> 00:26:49.810 align:middle line:84%
We don't know that
for any given tool.

00:26:49.810 --> 00:26:51.700 align:middle line:84%
You can put it in as a
variable in the model

00:26:51.700 --> 00:26:54.020 align:middle line:84%
and then you can compare
that to what you get.

00:26:54.020 --> 00:26:56.028 align:middle line:84%
You can compare the
modeled deposition

00:26:56.028 --> 00:26:57.320 align:middle line:90%
to the profile of what you get.

00:26:57.320 --> 00:26:59.903 align:middle line:84%
And then you get an idea of what
your sticking coefficient is.

00:26:59.903 --> 00:27:01.660 align:middle line:84%
It's not a number
you can calculate

00:27:01.660 --> 00:27:05.070 align:middle line:84%
from a first principles
point of view.

00:27:05.070 --> 00:27:08.430 align:middle line:84%
But people have derived
sticking coefficients

00:27:08.430 --> 00:27:10.170 align:middle line:90%
for various types of deposition.

00:27:10.170 --> 00:27:12.990 align:middle line:90%


00:27:12.990 --> 00:27:15.960 align:middle line:84%
OK, so slide 13, so this
is the formula we said.

00:27:15.960 --> 00:27:20.100 align:middle line:84%
The flux emitted is just 1
minus the sticking coefficient.

00:27:20.100 --> 00:27:22.830 align:middle line:84%
It's those that don't stick
times the flux incident

00:27:22.830 --> 00:27:24.430 align:middle line:90%
at the point.

00:27:24.430 --> 00:27:25.720 align:middle line:90%
We make some assumptions.

00:27:25.720 --> 00:27:27.920 align:middle line:84%
Generally, we assume
that ions stick.

00:27:27.920 --> 00:27:29.560 align:middle line:84%
So if we have an
ion coming down,

00:27:29.560 --> 00:27:31.240 align:middle line:84%
we assume sticking
coefficient is 1.

00:27:31.240 --> 00:27:34.720 align:middle line:84%
Why is that? ions tend
to be very reactive

00:27:34.720 --> 00:27:37.670 align:middle line:84%
and they often come down with
a certain amount of energy.

00:27:37.670 --> 00:27:40.210 align:middle line:84%
So we usually say that they
have sticking coefficient of 1.

00:27:40.210 --> 00:27:44.350 align:middle line:84%
Neutrals can have any
number one or less.

00:27:44.350 --> 00:27:46.300 align:middle line:84%
And they're often
assumed to be emitted

00:27:46.300 --> 00:27:49.520 align:middle line:84%
with some kind of a cosine
theta angle distribution.

00:27:49.520 --> 00:27:53.650 align:middle line:84%
So that is they may have no
memory of their arrival angle.

00:27:53.650 --> 00:27:56.350 align:middle line:84%
So don't think of this,
for example, in here,

00:27:56.350 --> 00:28:00.652 align:middle line:84%
don't think of this as a
little trough like a pool

00:28:00.652 --> 00:28:02.110 align:middle line:84%
that we've taken
all the water out,

00:28:02.110 --> 00:28:04.480 align:middle line:84%
and you have a ping pong
ball and it's bouncing around

00:28:04.480 --> 00:28:06.070 align:middle line:84%
with billiard ball
kind of collisions.

00:28:06.070 --> 00:28:07.820 align:middle line:84%
It's not supposed to
be thought like that.

00:28:07.820 --> 00:28:09.940 align:middle line:84%
This atom is supposed
to come down.

00:28:09.940 --> 00:28:12.220 align:middle line:84%
And then atoms are
coming down continuously,

00:28:12.220 --> 00:28:14.470 align:middle line:84%
say at this point, and
then it's readmitting

00:28:14.470 --> 00:28:17.050 align:middle line:84%
at with some angular
distribution,

00:28:17.050 --> 00:28:19.690 align:middle line:84%
but it's not necessarily a
billiard ball kind of collision

00:28:19.690 --> 00:28:22.800 align:middle line:90%
type of thing happening.

00:28:22.800 --> 00:28:26.930 align:middle line:84%
So you need to put in a
re-emission flux distribution.

00:28:26.930 --> 00:28:29.530 align:middle line:90%


00:28:29.530 --> 00:28:35.430 align:middle line:84%
So at any point i we get a
flux of redeposited material

00:28:35.430 --> 00:28:39.840 align:middle line:84%
because the emitted flux
can land somewhere else

00:28:39.840 --> 00:28:40.990 align:middle line:90%
on the surface.

00:28:40.990 --> 00:28:44.440 align:middle line:84%
So we have this sort of, again,
this ends up being bookkeeping.

00:28:44.440 --> 00:28:46.530 align:middle line:84%
We have this
something we express

00:28:46.530 --> 00:28:51.420 align:middle line:90%
as f super ik redeposited.

00:28:51.420 --> 00:28:56.565 align:middle line:84%
And what this is you take the
flux, the direct flux, f sub k,

00:28:56.565 --> 00:28:58.440 align:middle line:84%
that's coming into a
point k on the surface--

00:28:58.440 --> 00:29:00.540 align:middle line:90%
let's say it's right here--

00:29:00.540 --> 00:29:04.920 align:middle line:84%
and we're looking
at then point i.

00:29:04.920 --> 00:29:09.330 align:middle line:84%
It's desorbed from point k and
it's redeposited at point i.

00:29:09.330 --> 00:29:14.938 align:middle line:84%
So this redeposited flux depends
on some geometry factor, gik.

00:29:14.938 --> 00:29:16.980 align:middle line:84%
So it has to do with the
geometry between point i

00:29:16.980 --> 00:29:21.090 align:middle line:84%
and point k times f
sub k that's emitted,

00:29:21.090 --> 00:29:26.100 align:middle line:84%
so times this emitted
flux from this point k.

00:29:26.100 --> 00:29:28.020 align:middle line:84%
Well, the emitted
flux from point k

00:29:28.020 --> 00:29:29.460 align:middle line:84%
just depends on
the incoming flux

00:29:29.460 --> 00:29:33.630 align:middle line:84%
to point k times the 1 minus
the sticking coefficient.

00:29:33.630 --> 00:29:38.630 align:middle line:84%
So the nice thing is here for
point i can take any point k

00:29:38.630 --> 00:29:40.610 align:middle line:84%
and figure out if
I know the geometry

00:29:40.610 --> 00:29:42.350 align:middle line:90%
factor between the two.

00:29:42.350 --> 00:29:46.640 align:middle line:84%
How much is deposited
at this point i

00:29:46.640 --> 00:29:52.100 align:middle line:84%
resulting from having come from
being emitted from point k?

00:29:52.100 --> 00:29:54.260 align:middle line:84%
And then what you
do is you take all

00:29:54.260 --> 00:29:57.020 align:middle line:84%
of these at this point i
you take redeposited fluxes

00:29:57.020 --> 00:30:00.350 align:middle line:84%
from all points of the surface
so that all points of a surface

00:30:00.350 --> 00:30:02.090 align:middle line:84%
could be redepositing
at this point.

00:30:02.090 --> 00:30:07.262 align:middle line:84%
So you sum up for all i
and k and you figure out

00:30:07.262 --> 00:30:07.970 align:middle line:90%
what's deposited.

00:30:07.970 --> 00:30:11.510 align:middle line:84%
So gik then accounts for the
geometry between any point i

00:30:11.510 --> 00:30:12.050 align:middle line:90%
and k.

00:30:12.050 --> 00:30:13.670 align:middle line:84%
Because, obviously,
if you're over here,

00:30:13.670 --> 00:30:15.170 align:middle line:84%
let's say I'm over
here, my point k.

00:30:15.170 --> 00:30:17.420 align:middle line:84%
We're up at the surface,
and it's re-emitting.

00:30:17.420 --> 00:30:20.750 align:middle line:84%
Well, chances of it coming
back down over to this point

00:30:20.750 --> 00:30:24.170 align:middle line:84%
are dramatically lower than if
it's re-emitting from the walls

00:30:24.170 --> 00:30:25.880 align:middle line:90%
just based on geometry.

00:30:25.880 --> 00:30:30.380 align:middle line:90%


00:30:30.380 --> 00:30:35.660 align:middle line:84%
OK, so let's take a look at
some examples on slide 14.

00:30:35.660 --> 00:30:37.550 align:middle line:84%
And hopefully this
will become intuitive.

00:30:37.550 --> 00:30:39.380 align:middle line:84%
But if you have a low
sticking coefficient,

00:30:39.380 --> 00:30:41.780 align:middle line:84%
s sub c much less
than 1, you can end up

00:30:41.780 --> 00:30:44.720 align:middle line:84%
with more conformal deposition
or conformal coverage

00:30:44.720 --> 00:30:49.380 align:middle line:84%
of the step because of
the redeposition process.

00:30:49.380 --> 00:30:51.910 align:middle line:84%
Redeposition and this
low sticking coefficient

00:30:51.910 --> 00:30:53.910 align:middle line:84%
is usually more important
than surface diffusion

00:30:53.910 --> 00:30:55.500 align:middle line:84%
because most of
the time in these

00:30:55.500 --> 00:30:58.950 align:middle line:84%
processes the wafer temperature
is low enough that the surface

00:30:58.950 --> 00:31:03.090 align:middle line:84%
diffusion is not all that high,
especially if you're doing PVD.

00:31:03.090 --> 00:31:08.113 align:middle line:84%
But let's just take a look
here at the case A where I have

00:31:08.113 --> 00:31:09.280 align:middle line:90%
a high sticking coefficient.

00:31:09.280 --> 00:31:10.697 align:middle line:84%
So it's sticking
coefficient is 1.

00:31:10.697 --> 00:31:12.330 align:middle line:84%
Everything comes
down and sticks.

00:31:12.330 --> 00:31:16.180 align:middle line:84%
So what do I get if I'm
depositing in this trench?

00:31:16.180 --> 00:31:18.240 align:middle line:84%
Well, I get very
non-conformal deposition.

00:31:18.240 --> 00:31:20.965 align:middle line:84%
I get a film deposited at
the bottom of the trench.

00:31:20.965 --> 00:31:22.590 align:middle line:84%
There'd probably be
a film up here too.

00:31:22.590 --> 00:31:23.673 align:middle line:90%
It should have been shown.

00:31:23.673 --> 00:31:26.610 align:middle line:84%
But we're only looking at
what's happening in the trench.

00:31:26.610 --> 00:31:29.520 align:middle line:90%
But nothing on the side walls.

00:31:29.520 --> 00:31:30.090 align:middle line:90%
Why?

00:31:30.090 --> 00:31:35.550 align:middle line:84%
Because I really don't have any
opportunity for redeposition.

00:31:35.550 --> 00:31:39.520 align:middle line:84%
Whereas, I can have that same
angular arrival distribution.

00:31:39.520 --> 00:31:41.988 align:middle line:84%
So with the exact same angle
of arrival distribution,

00:31:41.988 --> 00:31:43.530 align:middle line:84%
if I have a low
sticking coefficient,

00:31:43.530 --> 00:31:46.660 align:middle line:84%
things can move around a
lot and hit the side walls.

00:31:46.660 --> 00:31:50.160 align:middle line:84%
And then you can end up with
more conformal deposition.

00:31:50.160 --> 00:31:52.290 align:middle line:84%
And again, you would use
this type of equation

00:31:52.290 --> 00:31:54.870 align:middle line:84%
in the computer to be
able to model that.

00:31:54.870 --> 00:31:56.770 align:middle line:84%
You just vary the
sticking coefficient.

00:31:56.770 --> 00:31:59.520 align:middle line:84%
And you need to calculate
the geometry factor

00:31:59.520 --> 00:32:01.570 align:middle line:90%
as part of that.

00:32:01.570 --> 00:32:03.090 align:middle line:84%
So low sticking
coefficient is good

00:32:03.090 --> 00:32:04.298 align:middle line:90%
if you want to coat a trench.

00:32:04.298 --> 00:32:05.928 align:middle line:84%
Now, that may not
be what you want.

00:32:05.928 --> 00:32:07.720 align:middle line:84%
You may want to just
deposit at the bottom.

00:32:07.720 --> 00:32:09.540 align:middle line:84%
But again, it depends
on the process

00:32:09.540 --> 00:32:13.300 align:middle line:90%
that you're trying to do.

00:32:13.300 --> 00:32:15.580 align:middle line:84%
OK, so that has to do
with sticking coefficient.

00:32:15.580 --> 00:32:19.157 align:middle line:84%
That's an important concept
in basic surface physics.

00:32:19.157 --> 00:32:20.740 align:middle line:84%
And we talked about
surface diffusion.

00:32:20.740 --> 00:32:24.640 align:middle line:84%
The third concept is sputtering,
what happens on the surface.

00:32:24.640 --> 00:32:26.455 align:middle line:84%
And that we talk about
here on slide 15.

00:32:26.455 --> 00:32:29.540 align:middle line:90%


00:32:29.540 --> 00:32:31.840 align:middle line:84%
There's a sputtered
flux at any point

00:32:31.840 --> 00:32:35.380 align:middle line:84%
i is caused by energetic
usually incoming ions.

00:32:35.380 --> 00:32:36.550 align:middle line:90%
Why do we care about ions?

00:32:36.550 --> 00:32:39.520 align:middle line:84%
Well, the neutrals usually come
down with low enough energy.

00:32:39.520 --> 00:32:41.600 align:middle line:84%
They do a little bit of
sputtering but not much.

00:32:41.600 --> 00:32:43.780 align:middle line:84%
But an incoming ion
can come in and it

00:32:43.780 --> 00:32:46.180 align:middle line:84%
might have a couple hundred
electron volts of energy.

00:32:46.180 --> 00:32:49.630 align:middle line:84%
With enough energy, it can then
hit something at the surface

00:32:49.630 --> 00:32:52.630 align:middle line:84%
and cause it to be
sputtered or emitted.

00:32:52.630 --> 00:32:55.000 align:middle line:84%
So what we typically
say is any point

00:32:55.000 --> 00:32:59.785 align:middle line:84%
i the sputtered flux depends
on the sputtering yield, y.

00:32:59.785 --> 00:33:04.270 align:middle line:84%
y is just the number sputtered
divided by the number incident.

00:33:04.270 --> 00:33:06.820 align:middle line:84%
And this plot tells you how
the sputtering yield varies

00:33:06.820 --> 00:33:10.840 align:middle line:84%
with angle, depends
on y times the flux

00:33:10.840 --> 00:33:15.370 align:middle line:84%
of incident argon
ions, flux of argon,

00:33:15.370 --> 00:33:18.860 align:middle line:90%
and the direct flux of ions.

00:33:18.860 --> 00:33:22.580 align:middle line:84%
So the total ionic
flux is what we add up.

00:33:22.580 --> 00:33:24.580 align:middle line:84%
So you might be curious
to say, all right, well,

00:33:24.580 --> 00:33:26.663 align:middle line:84%
how does the sputtering
yield depend on the angle?

00:33:26.663 --> 00:33:28.690 align:middle line:84%
Because that's going
to tell you if you

00:33:28.690 --> 00:33:30.370 align:middle line:84%
have a trench with
a certain angle,

00:33:30.370 --> 00:33:32.820 align:middle line:84%
and the atoms are coming in,
and the ions are coming in,

00:33:32.820 --> 00:33:34.570 align:middle line:84%
how is the sputtering
yield going to vary.

00:33:34.570 --> 00:33:39.280 align:middle line:84%
Well, this is a typical
plot of yield versus angle.

00:33:39.280 --> 00:33:42.730 align:middle line:84%
So again, a yield of
1 means it's 1 to 1.

00:33:42.730 --> 00:33:47.690 align:middle line:84%
For every one that's incident
on that point, one comes off.

00:33:47.690 --> 00:33:48.470 align:middle line:90%
And you can see.

00:33:48.470 --> 00:33:50.970 align:middle line:84%
And this is all measured with
respect to the surface normal.

00:33:50.970 --> 00:33:53.660 align:middle line:84%
So theta equals 0 means
normal sputtering.

00:33:53.660 --> 00:33:56.890 align:middle line:90%
So it's coming straight down.

00:33:56.890 --> 00:34:00.110 align:middle line:84%
So at theta equals 0 for
this particular example,

00:34:00.110 --> 00:34:01.300 align:middle line:90%
the sputtering yield is one.

00:34:01.300 --> 00:34:02.290 align:middle line:90%
And look what happens.

00:34:02.290 --> 00:34:04.870 align:middle line:84%
As you increase theta-- so
you're coming in a little more

00:34:04.870 --> 00:34:07.390 align:middle line:90%
grazing, I'm increasing theta--

00:34:07.390 --> 00:34:11.230 align:middle line:84%
it peaks somewhere here
around 50 or 60, 65 degrees.

00:34:11.230 --> 00:34:15.250 align:middle line:84%
Gets up to about 2, 2 and
1/2, and then eventually

00:34:15.250 --> 00:34:16.943 align:middle line:84%
at your very glancing
incidence there's

00:34:16.943 --> 00:34:18.110 align:middle line:90%
really no sputtering at all.

00:34:18.110 --> 00:34:20.780 align:middle line:90%
It really drops dramatically.

00:34:20.780 --> 00:34:23.830 align:middle line:84%
So this angular
sensitive and you

00:34:23.830 --> 00:34:25.480 align:middle line:84%
can use this to
achieve more planar

00:34:25.480 --> 00:34:27.100 align:middle line:90%
surfaces during a deposition.

00:34:27.100 --> 00:34:28.810 align:middle line:84%
In fact, we'll
show some examples

00:34:28.810 --> 00:34:33.070 align:middle line:84%
where we use ionized species
during deposition to give you

00:34:33.070 --> 00:34:34.870 align:middle line:90%
a little better planarity.

00:34:34.870 --> 00:34:36.722 align:middle line:84%
But so this angular
dependence is something

00:34:36.722 --> 00:34:37.930 align:middle line:90%
that we want to keep in mind.

00:34:37.930 --> 00:34:42.480 align:middle line:90%


00:34:42.480 --> 00:34:44.679 align:middle line:84%
OK, and now on slide
16, so what happens?

00:34:44.679 --> 00:34:46.320 align:middle line:84%
So let's say you do
sputter that off,

00:34:46.320 --> 00:34:48.900 align:middle line:84%
then you have redeposition
of the sputtered molecules,

00:34:48.900 --> 00:34:50.250 align:middle line:90%
how do you model that?

00:34:50.250 --> 00:34:52.123 align:middle line:84%
The exact same way
you modeled reemission

00:34:52.123 --> 00:34:53.790 align:middle line:84%
when you were just
coming off due to low

00:34:53.790 --> 00:34:55.260 align:middle line:90%
sticking coefficient.

00:34:55.260 --> 00:34:58.230 align:middle line:84%
You just say the
redeposited flux between i

00:34:58.230 --> 00:35:01.980 align:middle line:84%
at point i due to whatever is
sputtering off from point k

00:35:01.980 --> 00:35:04.740 align:middle line:84%
is just a geometry
factor gik, which

00:35:04.740 --> 00:35:07.230 align:middle line:84%
you which end up summing
over the surface,

00:35:07.230 --> 00:35:10.140 align:middle line:84%
times the sputter
flux from point k.

00:35:10.140 --> 00:35:12.480 align:middle line:84%
And that sputter
flux from point k

00:35:12.480 --> 00:35:17.070 align:middle line:84%
depends on the flux incident of
ions times the sputtering yield

00:35:17.070 --> 00:35:21.140 align:middle line:84%
y to see how the sputtering
yield comes into it.

00:35:21.140 --> 00:35:23.120 align:middle line:84%
And finally, if you
want to substitute

00:35:23.120 --> 00:35:25.460 align:middle line:84%
in the sticking
coefficients, what

00:35:25.460 --> 00:35:27.560 align:middle line:84%
you say is the
redeposited at point

00:35:27.560 --> 00:35:32.840 align:middle line:84%
i depends on the emitted
from k, which depends on 1

00:35:32.840 --> 00:35:35.430 align:middle line:90%
minus the sticking coefficient.

00:35:35.430 --> 00:35:39.200 align:middle line:84%
So we have this
redeposited due to emission

00:35:39.200 --> 00:35:41.510 align:middle line:84%
is very, very similar
to the redeposited

00:35:41.510 --> 00:35:45.020 align:middle line:90%
due to the sputtering.

00:35:45.020 --> 00:35:47.960 align:middle line:84%
And there's a final
term in a lot of these.

00:35:47.960 --> 00:35:49.460 align:middle line:84%
And this is the
biggest fudge factor

00:35:49.460 --> 00:35:52.730 align:middle line:84%
I would say in the whole model,
which is that ions coming down

00:35:52.730 --> 00:35:55.460 align:middle line:84%
on the surface can sometimes
enhance the deposition

00:35:55.460 --> 00:35:59.330 align:middle line:84%
rate in a way that's
not completely obvious.

00:35:59.330 --> 00:36:01.020 align:middle line:90%
The ions may come down.

00:36:01.020 --> 00:36:03.440 align:middle line:84%
They may supply
enough energy to drive

00:36:03.440 --> 00:36:06.360 align:middle line:84%
a chemical reaction that might
take place at the surface.

00:36:06.360 --> 00:36:09.390 align:middle line:90%
So we have a deposition flux.

00:36:09.390 --> 00:36:11.390 align:middle line:84%
So we can have a
deposition rate that

00:36:11.390 --> 00:36:17.340 align:middle line:84%
is called ion enhanced or ion
induced chemical reaction.

00:36:17.340 --> 00:36:18.680 align:middle line:90%
So it's kind of a fudge factor.

00:36:18.680 --> 00:36:22.100 align:middle line:84%
We have an additional flux
and a term with a k sub i,

00:36:22.100 --> 00:36:23.990 align:middle line:84%
where k sub i is a
fitting parameter,

00:36:23.990 --> 00:36:27.180 align:middle line:84%
times the flux of ions
coming in at any given point.

00:36:27.180 --> 00:36:31.400 align:middle line:84%
So you can have this extra
ion induced deposition rate.

00:36:31.400 --> 00:36:35.120 align:middle line:84%
Obviously, that's only important
in systems with ionized type

00:36:35.120 --> 00:36:38.130 align:middle line:90%
of deposition.

00:36:38.130 --> 00:36:40.110 align:middle line:84%
OK, so those are all
the different processes

00:36:40.110 --> 00:36:41.580 align:middle line:84%
at the surface and
the direct flux.

00:36:41.580 --> 00:36:43.753 align:middle line:84%
And now, starting
on slide 17, I want

00:36:43.753 --> 00:36:46.170 align:middle line:84%
to give a couple of examples
because it seems like there's

00:36:46.170 --> 00:36:47.378 align:middle line:90%
a lot of different equations.

00:36:47.378 --> 00:36:51.640 align:middle line:84%
But it turns out a lot of them
simplify for most systems.

00:36:51.640 --> 00:36:53.490 align:middle line:84%
So let's do an example
of low pressure CVD.

00:36:53.490 --> 00:37:00.000 align:middle line:84%
Remember, LPCVD is probably the
most common deposition process

00:37:00.000 --> 00:37:02.430 align:middle line:84%
in a fab, typically takes
place in a furnace that's

00:37:02.430 --> 00:37:06.690 align:middle line:84%
pumped down to low pressure,
say 10 to 100 millitorr.

00:37:06.690 --> 00:37:09.420 align:middle line:84%
Now, the wafers are
usually stacked in a batch.

00:37:09.420 --> 00:37:11.400 align:middle line:84%
People do 25 to 50
wafers at a time.

00:37:11.400 --> 00:37:14.460 align:middle line:84%
It's in a resistively
heated furnace.

00:37:14.460 --> 00:37:15.663 align:middle line:90%
There are no ions.

00:37:15.663 --> 00:37:16.830 align:middle line:90%
This is not a plasma system.

00:37:16.830 --> 00:37:19.048 align:middle line:84%
So we can get rid of
all ionized processes.

00:37:19.048 --> 00:37:21.090 align:middle line:84%
So we can ignore sputtering
because, again, we're

00:37:21.090 --> 00:37:23.250 align:middle line:84%
going to say that only
in the presence of ions

00:37:23.250 --> 00:37:26.320 align:middle line:84%
do you have enough energy
to sputter something off.

00:37:26.320 --> 00:37:28.530 align:middle line:90%
So we get rid of the sputtering.

00:37:28.530 --> 00:37:30.480 align:middle line:84%
Usually, long range
surface diffusion

00:37:30.480 --> 00:37:31.660 align:middle line:90%
is not that important.

00:37:31.660 --> 00:37:33.670 align:middle line:84%
So we can also ignore
the surface diffusion.

00:37:33.670 --> 00:37:37.380 align:middle line:84%
So if in my bookkeeping I have
all these different fluxes,

00:37:37.380 --> 00:37:39.390 align:middle line:84%
most of them are
all not present.

00:37:39.390 --> 00:37:42.060 align:middle line:84%
There's only two that
dominate at any point i.

00:37:42.060 --> 00:37:43.690 align:middle line:90%
It's the emitted flux.

00:37:43.690 --> 00:37:45.960 align:middle line:84%
Yes, because we have a
finite sticking coefficient,

00:37:45.960 --> 00:37:47.380 align:middle line:90%
and the redeposited flux.

00:37:47.380 --> 00:37:49.300 align:middle line:84%
Yes, we need to take
that into account,

00:37:49.300 --> 00:37:51.100 align:middle line:90%
and the neutral direct flux.

00:37:51.100 --> 00:37:52.830 align:middle line:84%
So really in this
example I really only

00:37:52.830 --> 00:37:54.622 align:middle line:84%
going to have three
fluxes I need to worry.

00:37:54.622 --> 00:37:57.330 align:middle line:84%
About all the rest
of these we don't

00:37:57.330 --> 00:38:01.380 align:middle line:84%
have to take into account
in the simulation.

00:38:01.380 --> 00:38:03.830 align:middle line:84%
So then we can write
down those fluxes

00:38:03.830 --> 00:38:07.980 align:middle line:84%
pretty simply, and the
net flux here on slide 18.

00:38:07.980 --> 00:38:12.350 align:middle line:84%
So at any point i on
the surface, f super i,

00:38:12.350 --> 00:38:15.650 align:middle line:84%
the net flux is again
the flux coming in

00:38:15.650 --> 00:38:16.970 align:middle line:90%
minus the flux going out.

00:38:16.970 --> 00:38:19.880 align:middle line:84%
So it's the flux of
directs, neutral species,

00:38:19.880 --> 00:38:22.220 align:middle line:84%
the redeposited flux that
comes from other areas

00:38:22.220 --> 00:38:25.490 align:middle line:84%
of the surface, minus
the flux that goes out.

00:38:25.490 --> 00:38:27.620 align:middle line:84%
Well, those that
don't stick, that's

00:38:27.620 --> 00:38:32.540 align:middle line:84%
1 minus the sticking coefficient
times the direct flux

00:38:32.540 --> 00:38:36.950 align:middle line:84%
of neutrals and the
redeposited direct flux.

00:38:36.950 --> 00:38:37.730 align:middle line:90%
OK?

00:38:37.730 --> 00:38:40.340 align:middle line:84%
So these are the
ones that come in,

00:38:40.340 --> 00:38:41.840 align:middle line:84%
and these are the
ones that go out.

00:38:41.840 --> 00:38:44.940 align:middle line:84%
And there's a negative
sign in between the two.

00:38:44.940 --> 00:38:46.940 align:middle line:84%
So you can rearrange
this a little bit

00:38:46.940 --> 00:38:49.160 align:middle line:84%
and you can write it
then as shown here,

00:38:49.160 --> 00:38:51.920 align:middle line:84%
the net flux at any point i
is the sticking coefficient

00:38:51.920 --> 00:38:57.200 align:middle line:84%
s sub c times the direct flux
at that point of neutrals

00:38:57.200 --> 00:38:59.780 align:middle line:90%
plus a term that relates--

00:38:59.780 --> 00:39:03.650 align:middle line:84%
a geometric term, this
gik times 1 minus s sub c.

00:39:03.650 --> 00:39:06.800 align:middle line:84%
That's those that don't
stick times the flux

00:39:06.800 --> 00:39:11.210 align:middle line:84%
into some other point
on the surface k.

00:39:11.210 --> 00:39:13.740 align:middle line:84%
And then we just
need to sum this up

00:39:13.740 --> 00:39:17.460 align:middle line:84%
over all points
k on the surface.

00:39:17.460 --> 00:39:19.940 align:middle line:84%
Now, what you can do to
simplify this a little bit,

00:39:19.940 --> 00:39:26.060 align:middle line:84%
you can define f sub d to be the
deposition flux at each point

00:39:26.060 --> 00:39:29.600 align:middle line:84%
to be equal to the
direct flux of neutrals

00:39:29.600 --> 00:39:33.200 align:middle line:84%
plus the redeposited flux
if you want to do that.

00:39:33.200 --> 00:39:36.170 align:middle line:84%
And then you can write the
deposition rate more simply

00:39:36.170 --> 00:39:39.360 align:middle line:90%
as the sticking coefficient.

00:39:39.360 --> 00:39:42.110 align:middle line:84%
So this is the dep rate,
then sticking coefficient

00:39:42.110 --> 00:39:46.520 align:middle line:84%
times the flux at any
given point i divided by n.

00:39:46.520 --> 00:39:48.770 align:middle line:84%
So we can then calculate
the deposition rate

00:39:48.770 --> 00:39:50.730 align:middle line:90%
at any point i on the surface.

00:39:50.730 --> 00:39:54.110 align:middle line:84%
And we use a cosine theta
to the n distribution

00:39:54.110 --> 00:39:55.410 align:middle line:90%
for the incoming molecules.

00:39:55.410 --> 00:39:59.385 align:middle line:84%
So it's a relatively simple
formula can be used for LPCVD.

00:39:59.385 --> 00:40:02.650 align:middle line:90%


00:40:02.650 --> 00:40:04.630 align:middle line:84%
And in fact, on slide
19, I just wanted

00:40:04.630 --> 00:40:05.830 align:middle line:90%
to go through an example.

00:40:05.830 --> 00:40:08.890 align:middle line:84%
This took directly
from your text.

00:40:08.890 --> 00:40:12.100 align:middle line:84%
What we're asked to do
is calculate the dep rate

00:40:12.100 --> 00:40:14.710 align:middle line:84%
using this LPCVD expression
that we just derived,

00:40:14.710 --> 00:40:18.430 align:middle line:84%
sticking coefficient times
a flux divided by density,

00:40:18.430 --> 00:40:20.090 align:middle line:90%
for silicon dioxide.

00:40:20.090 --> 00:40:21.520 align:middle line:84%
So this is low
temperature oxide.

00:40:21.520 --> 00:40:22.730 align:middle line:90%
And we have a flat surface.

00:40:22.730 --> 00:40:23.500 align:middle line:90%
So this is nice.

00:40:23.500 --> 00:40:25.690 align:middle line:90%
There's no topography.

00:40:25.690 --> 00:40:31.650 align:middle line:84%
We are told that the
sticking coefficient is 0.3

00:40:31.650 --> 00:40:34.290 align:middle line:84%
and that the maximum
unobstructed flux, so that's

00:40:34.290 --> 00:40:36.720 align:middle line:84%
the maximum flux that's
coming straight down,

00:40:36.720 --> 00:40:39.660 align:middle line:84%
is equal to 3 times 10
to the 15th molecules

00:40:39.660 --> 00:40:41.250 align:middle line:84%
per square centimeter
per second.

00:40:41.250 --> 00:40:43.933 align:middle line:90%
So that's a molecular flux.

00:40:43.933 --> 00:40:45.850 align:middle line:84%
And we're given the
density of the film that's

00:40:45.850 --> 00:40:50.930 align:middle line:84%
deposited, 2.27 grams
per cubic centimeter.

00:40:50.930 --> 00:40:54.120 align:middle line:84%
So this is a relatively
simple calculation.

00:40:54.120 --> 00:40:57.200 align:middle line:84%
We want to get the deposition
rate on a flat surface,

00:40:57.200 --> 00:40:59.460 align:middle line:84%
therefore there is
no shadowing effect.

00:40:59.460 --> 00:41:03.140 align:middle line:84%
There's no redeposited flux
because we're not coming off

00:41:03.140 --> 00:41:04.730 align:middle line:90%
of a side wall of a trench.

00:41:04.730 --> 00:41:08.310 align:middle line:84%
And each surface position is
in a horizontal orientation.

00:41:08.310 --> 00:41:12.100 align:middle line:84%
So we're only concerned
about the direct flux.

00:41:12.100 --> 00:41:17.410 align:middle line:84%
So f sub d, the deposited
flux, is just equal everywhere

00:41:17.410 --> 00:41:19.570 align:middle line:84%
to the maximum value,
which is this 3 times 10

00:41:19.570 --> 00:41:21.925 align:middle line:84%
to the 15th molecules per
square centimeter per second.

00:41:21.925 --> 00:41:25.240 align:middle line:90%


00:41:25.240 --> 00:41:27.880 align:middle line:84%
And you can look up
this equation 9.53.

00:41:27.880 --> 00:41:30.370 align:middle line:84%
In fact, that's
exactly what I just

00:41:30.370 --> 00:41:34.590 align:middle line:84%
was showing down here
for the dep rate.

00:41:34.590 --> 00:41:36.000 align:middle line:90%
So we have that equation.

00:41:36.000 --> 00:41:37.950 align:middle line:84%
The rate is just the
sticking coefficient

00:41:37.950 --> 00:41:39.720 align:middle line:90%
times the flux divided by n.

00:41:39.720 --> 00:41:44.610 align:middle line:84%
We need to do a little
bit of conversion here

00:41:44.610 --> 00:41:47.700 align:middle line:84%
to get ourselves from
grams per cubic centimeter

00:41:47.700 --> 00:41:48.992 align:middle line:90%
into molecules.

00:41:48.992 --> 00:41:50.700 align:middle line:84%
The way we do that is
we take the density

00:41:50.700 --> 00:41:53.538 align:middle line:84%
of SiO2 being 2.27 grams
per cubic centimeter.

00:41:53.538 --> 00:41:57.270 align:middle line:84%
And we multiply that
by Avogadro's number

00:41:57.270 --> 00:42:01.710 align:middle line:84%
divided by the number of
grams per mole of SiO2.

00:42:01.710 --> 00:42:03.270 align:middle line:84%
So we need to do a
little conversion

00:42:03.270 --> 00:42:06.390 align:middle line:84%
to convert this density of
grams per cubic centimeter

00:42:06.390 --> 00:42:09.570 align:middle line:84%
into a number of molecules
per cubic centimeter for SiO2.

00:42:09.570 --> 00:42:13.260 align:middle line:84%
So you get 2 times 10
to the 22 molecules

00:42:13.260 --> 00:42:17.902 align:middle line:84%
of SiO2, those units
per cubic centimeter.

00:42:17.902 --> 00:42:19.610 align:middle line:84%
And then you just use
the simple formula.

00:42:19.610 --> 00:42:21.235 align:middle line:84%
The rate is just a
sticking coefficient

00:42:21.235 --> 00:42:23.305 align:middle line:84%
times the flux, the
maximum flux over n.

00:42:23.305 --> 00:42:24.930 align:middle line:84%
You plug-in the
numbers you were given.

00:42:24.930 --> 00:42:32.790 align:middle line:84%
And you get about something
like 0.023 microns per minute.

00:42:32.790 --> 00:42:36.930 align:middle line:84%
But now, if you had a deposition
on a non-flat surface,

00:42:36.930 --> 00:42:39.700 align:middle line:84%
if you had a trench or something
like that on the side wall,

00:42:39.700 --> 00:42:41.830 align:middle line:84%
for example, the local
dep rate would be less.

00:42:41.830 --> 00:42:45.960 align:middle line:84%
So this gives you a maximum,
a rough idea of the maximum.

00:42:45.960 --> 00:42:48.150 align:middle line:90%
So it just gives you--

00:42:48.150 --> 00:42:50.700 align:middle line:84%
we'll talk later about
SPEEDIE simulations,

00:42:50.700 --> 00:42:51.840 align:middle line:90%
more complex topographies.

00:42:51.840 --> 00:42:54.573 align:middle line:84%
But it gives you a rough
idea of how you can model

00:42:54.573 --> 00:42:55.740 align:middle line:90%
this simple type of process.

00:42:55.740 --> 00:42:59.140 align:middle line:90%


00:42:59.140 --> 00:43:02.200 align:middle line:90%
OK, let's go on to slide 20.

00:43:02.200 --> 00:43:04.610 align:middle line:84%
And we'll give
some more examples.

00:43:04.610 --> 00:43:06.850 align:middle line:90%
Now we're going to do PVD.

00:43:06.850 --> 00:43:09.410 align:middle line:84%
So we've already talked about
physical vapor deposition

00:43:09.410 --> 00:43:09.910 align:middle line:90%
systems.

00:43:09.910 --> 00:43:14.410 align:middle line:84%
We said there could be DC or
RF sputtering or evaporation.

00:43:14.410 --> 00:43:18.190 align:middle line:84%
Typically, ions do not
play a significant role

00:43:18.190 --> 00:43:20.600 align:middle line:84%
in these kind of PVD
systems most of the time.

00:43:20.600 --> 00:43:25.150 align:middle line:84%
So the modeling of simple PVD
is very much analogous to LPCVD.

00:43:25.150 --> 00:43:28.390 align:middle line:84%
The parameters are
very different though.

00:43:28.390 --> 00:43:34.100 align:middle line:84%
So here's an example of a
simple DC sputtering system,

00:43:34.100 --> 00:43:36.410 align:middle line:84%
which we talked about a
couple of lectures ago.

00:43:36.410 --> 00:43:39.080 align:middle line:84%
And these are the
processes that go on.

00:43:39.080 --> 00:43:41.980 align:middle line:84%
So just like LPCVD,
we can say a rate

00:43:41.980 --> 00:43:44.620 align:middle line:84%
at any point on the surface is
a sticking coefficient times

00:43:44.620 --> 00:43:49.250 align:middle line:84%
the flux, the total deposited
flux divided by the density.

00:43:49.250 --> 00:43:53.410 align:middle line:84%
However, the key difference is
that the sticking coefficient

00:43:53.410 --> 00:43:56.170 align:middle line:84%
and the arrival
angle distribution,

00:43:56.170 --> 00:43:59.230 align:middle line:84%
cosine theta to the n, will be
very different between LPCVD

00:43:59.230 --> 00:44:00.550 align:middle line:90%
and PVD systems.

00:44:00.550 --> 00:44:03.625 align:middle line:84%
And that's where the real
differences tend to come about.

00:44:03.625 --> 00:44:07.400 align:middle line:90%


00:44:07.400 --> 00:44:08.995 align:middle line:84%
There is one other
type of system

00:44:08.995 --> 00:44:11.120 align:middle line:84%
for PVD, though, where you
do have to pay attention

00:44:11.120 --> 00:44:13.370 align:middle line:84%
to a little more complex
processes than you would

00:44:13.370 --> 00:44:14.030 align:middle line:90%
in LPCVD.

00:44:14.030 --> 00:44:17.210 align:middle line:84%
And that's shown on slide 21
when you have ionized PVD.

00:44:17.210 --> 00:44:20.810 align:middle line:84%
We did talk about the
case where we have

00:44:20.810 --> 00:44:24.090 align:middle line:90%
systems that are more complex.

00:44:24.090 --> 00:44:26.780 align:middle line:84%
This because ions and
neutrals both play a role.

00:44:26.780 --> 00:44:30.030 align:middle line:84%
Here's an example of
an ionized PVD system.

00:44:30.030 --> 00:44:32.542 align:middle line:84%
So you have
sputtering of aluminum

00:44:32.542 --> 00:44:33.500 align:middle line:90%
coming off this target.

00:44:33.500 --> 00:44:35.500 align:middle line:84%
But then you have an
additional-- in addition to

00:44:35.500 --> 00:44:39.080 align:middle line:84%
that, you have a
coil that goes around

00:44:39.080 --> 00:44:41.810 align:middle line:84%
that ionizes the
aluminum as it comes off.

00:44:41.810 --> 00:44:45.470 align:middle line:84%
Now you have a large density
of ions that are being created.

00:44:45.470 --> 00:44:46.850 align:middle line:84%
And then these
can be accelerated

00:44:46.850 --> 00:44:49.130 align:middle line:90%
towards the substrate.

00:44:49.130 --> 00:44:53.210 align:middle line:84%
So this is not that uncommon
for metal deposition.

00:44:53.210 --> 00:44:55.660 align:middle line:84%
So you have aluminum
or maybe titanium

00:44:55.660 --> 00:44:56.960 align:middle line:90%
ions that'll be present.

00:44:56.960 --> 00:44:58.420 align:middle line:84%
Therefore, when
you have ions, you

00:44:58.420 --> 00:45:01.000 align:middle line:84%
do have to take into account
sputtering and other processes

00:45:01.000 --> 00:45:05.680 align:middle line:84%
that will not be present
in LPCVD or the simpler PVD

00:45:05.680 --> 00:45:06.310 align:middle line:90%
systems.

00:45:06.310 --> 00:45:10.330 align:middle line:84%
So ionized PVD, inductively
coupled ionized PVD,

00:45:10.330 --> 00:45:14.170 align:middle line:84%
is a little bit more
complicated to model, just more

00:45:14.170 --> 00:45:18.330 align:middle line:90%
bookkeeping in the equations.

00:45:18.330 --> 00:45:20.810 align:middle line:84%
Here's an example,
in fact, on slide 22,

00:45:20.810 --> 00:45:24.120 align:middle line:84%
if we do ionize PVD, of all the
different fluxes that really do

00:45:24.120 --> 00:45:25.370 align:middle line:90%
need to be taken into account.

00:45:25.370 --> 00:45:28.310 align:middle line:84%
And you see we have
yes on all of them,

00:45:28.310 --> 00:45:31.580 align:middle line:84%
the direct neutrals,
the direct ions.

00:45:31.580 --> 00:45:34.083 align:middle line:84%
The only one we're not taking
into account in this case

00:45:34.083 --> 00:45:36.500 align:middle line:84%
because we're assuming the
wafer is low enough temperature

00:45:36.500 --> 00:45:38.780 align:middle line:84%
that we can ignore
surface diffusion.

00:45:38.780 --> 00:45:42.170 align:middle line:84%
But all these fluxes would
need to be taken into account.

00:45:42.170 --> 00:45:45.500 align:middle line:84%
And if you do that,
shown here on slide 22,

00:45:45.500 --> 00:45:48.080 align:middle line:84%
this is the example
of the possible terms

00:45:48.080 --> 00:45:50.400 align:middle line:84%
that could be included
in your computer model.

00:45:50.400 --> 00:45:53.530 align:middle line:84%
So you would say that
the rate at any point i

00:45:53.530 --> 00:45:55.290 align:middle line:84%
depends on the
sticking coefficient

00:45:55.290 --> 00:45:58.890 align:middle line:84%
times the direct
maximum deposited

00:45:58.890 --> 00:46:01.230 align:middle line:84%
flux, where fd
includes the direct

00:46:01.230 --> 00:46:03.780 align:middle line:84%
and the redeposited
neutral fluxes.

00:46:03.780 --> 00:46:08.723 align:middle line:84%
Plus f sub i includes the direct
redeposit and ion induced flux.

00:46:08.723 --> 00:46:09.640 align:middle line:90%
So there's an f sub i.

00:46:09.640 --> 00:46:11.960 align:middle line:84%
And again, f sub i doesn't
have a sticking coefficient

00:46:11.960 --> 00:46:12.460 align:middle line:90%
associated.

00:46:12.460 --> 00:46:14.680 align:middle line:84%
We say for ions, we
include all of them,

00:46:14.680 --> 00:46:17.800 align:middle line:84%
we say they just
come down and stick.

00:46:17.800 --> 00:46:20.500 align:middle line:84%
And then you have a minus
those that are sputtered off.

00:46:20.500 --> 00:46:24.620 align:middle line:84%
You have a sputter term
plus a redeposited term.

00:46:24.620 --> 00:46:28.120 align:middle line:84%
So this frd models the
redeposition due to sputtering.

00:46:28.120 --> 00:46:32.030 align:middle line:84%
So you have extra terms here
divided by the density n.

00:46:32.030 --> 00:46:34.450 align:middle line:84%
And so you have a positive
term and a negative term,

00:46:34.450 --> 00:46:37.810 align:middle line:84%
some of which depending on
the point i and the surface

00:46:37.810 --> 00:46:41.200 align:middle line:84%
and the angles involved
may cancel each other out.

00:46:41.200 --> 00:46:44.140 align:middle line:90%


00:46:44.140 --> 00:46:47.790 align:middle line:84%
OK so those are some
basic bookkeeping models.

00:46:47.790 --> 00:46:49.440 align:middle line:84%
I want to actually
do some examples

00:46:49.440 --> 00:46:51.810 align:middle line:84%
of the values of
these parameters

00:46:51.810 --> 00:46:53.730 align:middle line:84%
that are useful for
specific systems.

00:46:53.730 --> 00:46:55.920 align:middle line:84%
And so far, we've talked
about two parameters that

00:46:55.920 --> 00:46:59.520 align:middle line:84%
are most important,
the n value, which

00:46:59.520 --> 00:47:03.870 align:middle line:84%
is the exponent in the cosine
theta to the n arrival angle

00:47:03.870 --> 00:47:07.900 align:middle line:84%
distribution, and the
sticking coefficient s sub c.

00:47:07.900 --> 00:47:12.988 align:middle line:84%
Those are the two most critical
in modeling simple systems.

00:47:12.988 --> 00:47:15.280 align:middle line:84%
And there are a couple of
different model systems shown

00:47:15.280 --> 00:47:15.780 align:middle line:90%
here.

00:47:15.780 --> 00:47:17.890 align:middle line:84%
On the top we're talking
about sputter deposition,

00:47:17.890 --> 00:47:21.950 align:middle line:84%
either standard or
ionized, and evaporation.

00:47:21.950 --> 00:47:23.500 align:middle line:90%
So these are PVD systems.

00:47:23.500 --> 00:47:27.050 align:middle line:84%
In the bottom, we
have the CVD systems.

00:47:27.050 --> 00:47:28.600 align:middle line:90%
So let's look at PVD.

00:47:28.600 --> 00:47:30.850 align:middle line:84%
Well, physical
vapor deposition, it

00:47:30.850 --> 00:47:33.470 align:middle line:84%
tends to have much more vertical
arrival angle distribution.

00:47:33.470 --> 00:47:35.530 align:middle line:90%
So the n value is big, right?

00:47:35.530 --> 00:47:38.680 align:middle line:84%
Almost everything in PVD
is coming straight down.

00:47:38.680 --> 00:47:41.060 align:middle line:84%
Certainly in evaporation
you have very low pressure,

00:47:41.060 --> 00:47:42.220 align:middle line:90%
so you have line of sight.

00:47:42.220 --> 00:47:46.690 align:middle line:84%
Even in sputtering you tend to
have close very anisotropic.

00:47:46.690 --> 00:47:49.285 align:middle line:84%
So for sputter
deposition, depending,

00:47:49.285 --> 00:47:52.690 align:middle line:84%
you can have n equals
up to five maybe.

00:47:52.690 --> 00:47:58.590 align:middle line:84%
If you're ionized you can get
up into the range of 50 or so.

00:47:58.590 --> 00:48:03.540 align:middle line:84%
But in any case, n is usually
greater than 1 for PVD.

00:48:03.540 --> 00:48:07.500 align:middle line:84%
In contrast, CVD systems
tend to have pretty much

00:48:07.500 --> 00:48:09.920 align:middle line:90%
isotropic arrival angle.

00:48:09.920 --> 00:48:12.630 align:middle line:84%
PVD, again, takes
place you're sputtering

00:48:12.630 --> 00:48:16.410 align:middle line:84%
in 10 to the minus 5
torr, or 1 times 10

00:48:16.410 --> 00:48:19.540 align:middle line:84%
to the minus 3 torr,
or something like that.

00:48:19.540 --> 00:48:23.340 align:middle line:84%
CVD usually much higher,
hundreds of millitorr,

00:48:23.340 --> 00:48:25.270 align:middle line:90%
0.1 torr or something like that.

00:48:25.270 --> 00:48:27.450 align:middle line:84%
So you usually have
higher pressure.

00:48:27.450 --> 00:48:29.130 align:middle line:84%
You have a lot of
gas phase collisions

00:48:29.130 --> 00:48:31.410 align:middle line:84%
that randomize things
and mostly neutrals.

00:48:31.410 --> 00:48:33.460 align:middle line:84%
Usually, in CVD, you
don't have many ions.

00:48:33.460 --> 00:48:35.310 align:middle line:90%
So n is usually 1 in CVD.

00:48:35.310 --> 00:48:40.120 align:middle line:84%
So the cosine theta to the n
is usually fairly isotropic.

00:48:40.120 --> 00:48:41.440 align:middle line:90%
What about PVD?

00:48:41.440 --> 00:48:44.800 align:middle line:84%
Well, the sticking coefficient
in PVD tends to be close to 1.

00:48:44.800 --> 00:48:47.140 align:middle line:84%
There really isn't much
surface chemistry involved.

00:48:47.140 --> 00:48:50.080 align:middle line:84%
The aluminum or whatever it
is that's being evaporated

00:48:50.080 --> 00:48:55.120 align:middle line:84%
or sputtered usually comes down
and pretty close to sticks.

00:48:55.120 --> 00:48:56.260 align:middle line:90%
There isn't a whole lot.

00:48:56.260 --> 00:48:57.100 align:middle line:90%
There can be.

00:48:57.100 --> 00:49:00.190 align:middle line:84%
But most of the time the
atoms arrive and stick.

00:49:00.190 --> 00:49:02.680 align:middle line:84%
Very, very different, though,
in the case of LPCVD--

00:49:02.680 --> 00:49:04.960 align:middle line:84%
look at LPCVD, the
sticking coefficients,

00:49:04.960 --> 00:49:07.480 align:middle line:84%
depending on what your
chemistry using, if you're

00:49:07.480 --> 00:49:09.370 align:middle line:84%
using a silicon
source of silane,

00:49:09.370 --> 00:49:12.220 align:middle line:84%
you might have a sticking
coefficient of 0.5 or 0.3.

00:49:12.220 --> 00:49:15.400 align:middle line:84%
For TEOS, we mentioned
there's other ways of doing

00:49:15.400 --> 00:49:18.670 align:middle line:84%
low temperature oxide,
not just with silane,

00:49:18.670 --> 00:49:22.570 align:middle line:84%
but there's this
other silicon sources.

00:49:22.570 --> 00:49:26.780 align:middle line:84%
Sticking coefficient
can be much lower.

00:49:26.780 --> 00:49:28.730 align:middle line:84%
LPCVD tungsten or
polysilicon you

00:49:28.730 --> 00:49:31.500 align:middle line:84%
have much lower
sticking coefficients,

00:49:31.500 --> 00:49:34.910 align:middle line:90%
so very different from PVD.

00:49:34.910 --> 00:49:37.767 align:middle line:84%
That same chart is reproduced
here again on slide 23.

00:49:37.767 --> 00:49:38.850 align:middle line:90%
It's the exact same chart.

00:49:38.850 --> 00:49:41.183 align:middle line:84%
I just wanted to reproduce
it and talk a little bit more

00:49:41.183 --> 00:49:42.890 align:middle line:90%
about the CVD thing.

00:49:42.890 --> 00:49:45.650 align:middle line:84%
Because they have
surface chemistry,

00:49:45.650 --> 00:49:48.470 align:middle line:84%
sticking coefficient
much, much less than 1,

00:49:48.470 --> 00:49:52.380 align:middle line:84%
and things often evaporate
before they react.

00:49:52.380 --> 00:49:53.410 align:middle line:90%
What does this mean?

00:49:53.410 --> 00:49:55.510 align:middle line:84%
Well, just by looking
at these numbers,

00:49:55.510 --> 00:49:57.817 align:middle line:84%
you know that CVD systems
with their small sticking

00:49:57.817 --> 00:49:59.400 align:middle line:84%
coefficients are
going to tend to have

00:49:59.400 --> 00:50:01.350 align:middle line:90%
more conformal deposition.

00:50:01.350 --> 00:50:03.750 align:middle line:84%
If you want to
cover a step and you

00:50:03.750 --> 00:50:05.310 align:middle line:84%
want to cover it
very conformally,

00:50:05.310 --> 00:50:05.920 align:middle line:90%
what does that mean?

00:50:05.920 --> 00:50:08.250 align:middle line:84%
That means the thickness along
the flat part of the wafer

00:50:08.250 --> 00:50:09.660 align:middle line:84%
is exactly equal
to the thickness

00:50:09.660 --> 00:50:12.273 align:middle line:84%
of the film along
the trench wall is

00:50:12.273 --> 00:50:13.440 align:middle line:90%
exactly equal in the bottom.

00:50:13.440 --> 00:50:14.940 align:middle line:90%
It's just completely conformal.

00:50:14.940 --> 00:50:18.390 align:middle line:84%
In that case, you
probably want to use CVD.

00:50:18.390 --> 00:50:20.050 align:middle line:84%
Now, that may not
be what you want,

00:50:20.050 --> 00:50:22.590 align:middle line:84%
but this is what we mean
by conformal deposition,

00:50:22.590 --> 00:50:23.580 align:middle line:90%
that equal thickness.

00:50:23.580 --> 00:50:29.220 align:middle line:84%
And CVD tends to give you
more conformality just because

00:50:29.220 --> 00:50:33.870 align:middle line:84%
of this sticking
coefficient argument.

00:50:33.870 --> 00:50:36.630 align:middle line:84%
OK, now I want to show some
actual examples of simulations

00:50:36.630 --> 00:50:38.430 align:middle line:84%
to convince you of
some of these things

00:50:38.430 --> 00:50:39.680 align:middle line:90%
that we've been talking about.

00:50:39.680 --> 00:50:41.940 align:middle line:84%
And we're going to
vary the parameters n

00:50:41.940 --> 00:50:44.440 align:middle line:90%
and s sub c in the model.

00:50:44.440 --> 00:50:47.670 align:middle line:84%
So on slide 25, these are
topography simulations

00:50:47.670 --> 00:50:49.500 align:middle line:84%
that are taken
from the simulator

00:50:49.500 --> 00:50:50.940 align:middle line:90%
that I mentioned called SPEEDIE.

00:50:50.940 --> 00:50:52.710 align:middle line:84%
Again, that's a
topography simulator.

00:50:52.710 --> 00:50:55.950 align:middle line:84%
You cannot simulate this type
of topography in SUPREM-IV.

00:50:55.950 --> 00:50:59.110 align:middle line:90%
SUPREM-IV doesn't do topography.

00:50:59.110 --> 00:51:05.910 align:middle line:84%
So this is an example of you're
doing a deposition using LPCVD

00:51:05.910 --> 00:51:08.310 align:middle line:84%
of SiO2 and you originally
have a trench that you have

00:51:08.310 --> 00:51:10.150 align:middle line:90%
etched that looks like this.

00:51:10.150 --> 00:51:11.800 align:middle line:90%
And each contour line--

00:51:11.800 --> 00:51:13.410 align:middle line:90%
it's a little bit hard to see.

00:51:13.410 --> 00:51:17.070 align:middle line:84%
But each contour line represents
the deposited topography

00:51:17.070 --> 00:51:18.490 align:middle line:90%
at different time intervals.

00:51:18.490 --> 00:51:22.630 align:middle line:84%
So each one might be
after a 1 minute interval.

00:51:22.630 --> 00:51:26.910 align:middle line:84%
So you get an idea of how the
topography develops over time.

00:51:26.910 --> 00:51:29.430 align:middle line:84%
In this particular example,
we did a SPEEDIE simulation

00:51:29.430 --> 00:51:32.305 align:middle line:84%
with a sticking
coefficient of 1.

00:51:32.305 --> 00:51:33.930 align:middle line:84%
Actually, the sticking
coefficient of 1

00:51:33.930 --> 00:51:35.340 align:middle line:90%
is probably more typical of PVD.

00:51:35.340 --> 00:51:38.880 align:middle line:84%
So this really should
be PVD in your mind.

00:51:38.880 --> 00:51:40.980 align:middle line:84%
And all we did
mathematically is vary

00:51:40.980 --> 00:51:44.230 align:middle line:84%
the arrival angle
distribution, the n value.

00:51:44.230 --> 00:51:47.010 align:middle line:84%
So this is for n equals
1, that's isotropic.

00:51:47.010 --> 00:51:53.020 align:middle line:84%
Here's for n equals 3, somewhat
anisotropic, n equals 10.

00:51:53.020 --> 00:51:54.360 align:middle line:90%
So let's look at this.

00:51:54.360 --> 00:51:56.910 align:middle line:84%
Even for isotropic
arrival distribution,

00:51:56.910 --> 00:52:00.360 align:middle line:84%
because of shadowing
effects and things,

00:52:00.360 --> 00:52:01.962 align:middle line:84%
conformal coverage
is not achieved

00:52:01.962 --> 00:52:03.420 align:middle line:84%
with the sticking
coefficient of 1.

00:52:03.420 --> 00:52:05.860 align:middle line:84%
That is, what do I mean by
conformal coverage is not

00:52:05.860 --> 00:52:06.360 align:middle line:90%
achieved?

00:52:06.360 --> 00:52:07.980 align:middle line:84%
Well, the thickness
of the film here

00:52:07.980 --> 00:52:10.410 align:middle line:84%
at the surface on
the flat portions

00:52:10.410 --> 00:52:14.790 align:middle line:84%
is not equal to the thickness
along the side wall.

00:52:14.790 --> 00:52:18.060 align:middle line:84%
The side wall is thinner
even for n equals 1.

00:52:18.060 --> 00:52:20.890 align:middle line:90%


00:52:20.890 --> 00:52:25.720 align:middle line:84%
And so what this implies that if
you have a sticking coefficient

00:52:25.720 --> 00:52:30.940 align:middle line:84%
s sub c equal to 1, the geometry
and line of sight issues

00:52:30.940 --> 00:52:33.080 align:middle line:90%
are going to be very important.

00:52:33.080 --> 00:52:35.380 align:middle line:84%
So for example,
for PVD, you really

00:52:35.380 --> 00:52:37.270 align:middle line:84%
need to take into
account the geometry

00:52:37.270 --> 00:52:40.510 align:middle line:90%
of what you're depositing into.

00:52:40.510 --> 00:52:42.400 align:middle line:84%
Look at this one
for n equals 10.

00:52:42.400 --> 00:52:44.503 align:middle line:84%
You almost get no
deposition on the side wall.

00:52:44.503 --> 00:52:45.920 align:middle line:84%
You get quite a
bit on the bottom.

00:52:45.920 --> 00:52:48.940 align:middle line:84%
And notice this is for
an aspect ratio that's

00:52:48.940 --> 00:52:51.820 align:middle line:84%
pretty gentle, I mean, pretty
not that sophisticated.

00:52:51.820 --> 00:52:54.200 align:middle line:84%
This aspect ratio of
0.3, what does that mean?

00:52:54.200 --> 00:52:58.330 align:middle line:84%
That means the trench is 3
times wider than it is tall.

00:52:58.330 --> 00:53:01.270 align:middle line:84%
So it's only 1 micron tall,
but it's 3 microns wide.

00:53:01.270 --> 00:53:04.840 align:middle line:84%
And you're already seeing
these nonconformallity types

00:53:04.840 --> 00:53:07.200 align:middle line:90%
of issues.

00:53:07.200 --> 00:53:11.450 align:middle line:84%
So this is what you'd expect
from PVD with these parameters.

00:53:11.450 --> 00:53:14.270 align:middle line:84%
Just to remind you, on page
26 what we're talking about,

00:53:14.270 --> 00:53:16.700 align:middle line:84%
the n equals 1 the flux
as a function of angle

00:53:16.700 --> 00:53:18.050 align:middle line:90%
looks like this.

00:53:18.050 --> 00:53:20.060 align:middle line:84%
N equals 3 looks
something-- it cuts out

00:53:20.060 --> 00:53:21.450 align:middle line:90%
after about 60 degrees.

00:53:21.450 --> 00:53:24.900 align:middle line:84%
And the n equals 15 cuts
out after about 30 degrees.

00:53:24.900 --> 00:53:27.360 align:middle line:90%
So this is close to n equals 15.

00:53:27.360 --> 00:53:30.420 align:middle line:84%
So when I was getting more
than about 30 degrees,

00:53:30.420 --> 00:53:33.380 align:middle line:84%
so from a normal you can imagine
going on to this surface,

00:53:33.380 --> 00:53:35.600 align:middle line:84%
there is not a
whole lot of flux.

00:53:35.600 --> 00:53:36.720 align:middle line:90%
And that's the problem.

00:53:36.720 --> 00:53:38.405 align:middle line:84%
That's why we're
getting such low--

00:53:38.405 --> 00:53:40.920 align:middle line:90%


00:53:40.920 --> 00:53:42.943 align:middle line:84%
with the sticking
coefficient of 1,

00:53:42.943 --> 00:53:44.360 align:middle line:84%
you're getting
such low deposition

00:53:44.360 --> 00:53:45.485 align:middle line:90%
along those vertical walls.

00:53:45.485 --> 00:53:49.440 align:middle line:90%


00:53:49.440 --> 00:53:54.210 align:middle line:84%
Let's make it a little
more difficult even

00:53:54.210 --> 00:53:55.800 align:middle line:90%
let's take an aspect ratio.

00:53:55.800 --> 00:53:57.690 align:middle line:84%
We're going to take
those same parameters, so

00:53:57.690 --> 00:54:01.020 align:middle line:84%
the same parameters
that we just saw.

00:54:01.020 --> 00:54:05.650 align:middle line:84%
Sticking coefficient
equals 1 here on slide 27,

00:54:05.650 --> 00:54:08.530 align:middle line:84%
but now I've increased
the aspect ratio from 0.3

00:54:08.530 --> 00:54:11.060 align:middle line:90%
up to 1.3 or 1.25.

00:54:11.060 --> 00:54:15.913 align:middle line:84%
So now the trench
is 1.25 times tall

00:54:15.913 --> 00:54:17.080 align:middle line:90%
compared to what it is wide.

00:54:17.080 --> 00:54:18.580 align:middle line:84%
So it's much taller
than it is wide,

00:54:18.580 --> 00:54:20.205 align:middle line:84%
just the opposite of
what I had before.

00:54:20.205 --> 00:54:23.550 align:middle line:90%


00:54:23.550 --> 00:54:27.430 align:middle line:84%
Now, what you do see again is
less deposition on the side

00:54:27.430 --> 00:54:27.930 align:middle line:90%
walls.

00:54:27.930 --> 00:54:32.910 align:middle line:84%
Here, this is A here on the
left is for isotropic arrival,

00:54:32.910 --> 00:54:33.900 align:middle line:90%
n equals 1.

00:54:33.900 --> 00:54:37.540 align:middle line:84%
And b is for
anisotropic, n equals 10.

00:54:37.540 --> 00:54:39.030 align:middle line:90%
So let's look at the n equals 1.

00:54:39.030 --> 00:54:40.140 align:middle line:90%
Well, what's happening?

00:54:40.140 --> 00:54:43.350 align:middle line:84%
You see if for
isotropic arrival angle,

00:54:43.350 --> 00:54:44.970 align:middle line:84%
you're not getting
much material down

00:54:44.970 --> 00:54:47.430 align:middle line:84%
at the bottom of
that narrow trench.

00:54:47.430 --> 00:54:50.400 align:middle line:84%
Because, again, it's
reasonably isotropic arrival,

00:54:50.400 --> 00:54:53.340 align:middle line:84%
you're getting material
coming deposited along here

00:54:53.340 --> 00:54:55.740 align:middle line:84%
and you're sort of
developing these lobes up

00:54:55.740 --> 00:54:58.320 align:middle line:84%
at the top, which if you
had a narrow enough trench,

00:54:58.320 --> 00:55:00.000 align:middle line:84%
you can imagine
these might cut off

00:55:00.000 --> 00:55:02.370 align:middle line:90%
and you end up with a big void.

00:55:02.370 --> 00:55:05.220 align:middle line:84%
If you're more anisotropic,
you're coming down straight.

00:55:05.220 --> 00:55:07.470 align:middle line:84%
So you do get quite a bit
at the bottom of the trench.

00:55:07.470 --> 00:55:08.850 align:middle line:84%
You get quite a
bit on the flats.

00:55:08.850 --> 00:55:12.160 align:middle line:84%
But you get nothing or very
little on the side walls.

00:55:12.160 --> 00:55:14.410 align:middle line:84%
So as you go to narrower
and narrower trenches,

00:55:14.410 --> 00:55:16.120 align:middle line:84%
you can imagine you
might end up not

00:55:16.120 --> 00:55:17.140 align:middle line:90%
being able to fill them at all.

00:55:17.140 --> 00:55:19.807 align:middle line:84%
You might end up with voiding if
you have a sticking coefficient

00:55:19.807 --> 00:55:23.770 align:middle line:84%
of 1 is really what this boils
down to for high aspect ratio

00:55:23.770 --> 00:55:26.570 align:middle line:90%
trenches.

00:55:26.570 --> 00:55:30.090 align:middle line:84%
So if you want to
avoid that, let's

00:55:30.090 --> 00:55:32.580 align:middle line:84%
say the purpose
of your deposition

00:55:32.580 --> 00:55:33.930 align:middle line:90%
is to fill this trench.

00:55:33.930 --> 00:55:36.360 align:middle line:84%
You haven't done a very
good job in this case.

00:55:36.360 --> 00:55:37.920 align:middle line:84%
And you're not going to do a
good job in this case at all.

00:55:37.920 --> 00:55:39.128 align:middle line:90%
You're going to pinch it off.

00:55:39.128 --> 00:55:40.860 align:middle line:90%
What do we need to do?

00:55:40.860 --> 00:55:42.860 align:middle line:84%
Well, we need to lower
the sticking coefficient.

00:55:42.860 --> 00:55:45.870 align:middle line:84%
We need to have not such a
line of sight distribution.

00:55:45.870 --> 00:55:48.080 align:middle line:84%
We need for atoms to
come down, come in here,

00:55:48.080 --> 00:55:50.570 align:middle line:84%
and not stick, and move
around so they can eventually

00:55:50.570 --> 00:55:53.150 align:middle line:90%
cover these side walls.

00:55:53.150 --> 00:55:56.840 align:middle line:84%
And that's exactly
what is shown on slide

00:55:56.840 --> 00:55:59.270 align:middle line:90%
28 in the SPEEDIE simulations.

00:55:59.270 --> 00:56:02.690 align:middle line:84%
Here's an example
of now I've got

00:56:02.690 --> 00:56:06.110 align:middle line:84%
that same trench, that same
high aspect ratio, 1.25.

00:56:06.110 --> 00:56:08.630 align:middle line:84%
But on the left here, A, I
have the sticking coefficient

00:56:08.630 --> 00:56:09.810 align:middle line:90%
of 0.1.

00:56:09.810 --> 00:56:12.020 align:middle line:90%
So only 1 in 10 atoms sticks.

00:56:12.020 --> 00:56:15.323 align:middle line:84%
The other 9, when they hit a
point, they go somewhere else

00:56:15.323 --> 00:56:16.740 align:middle line:84%
and they continue
to bounce around

00:56:16.740 --> 00:56:18.240 align:middle line:90%
until they finally stick.

00:56:18.240 --> 00:56:19.670 align:middle line:90%
Here's 1 in 100 sticking.

00:56:19.670 --> 00:56:22.340 align:middle line:90%


00:56:22.340 --> 00:56:24.620 align:middle line:84%
so, again, this is
with n equals 1.

00:56:24.620 --> 00:56:26.973 align:middle line:84%
So it's isotropic arrival,
but with different values

00:56:26.973 --> 00:56:28.140 align:middle line:90%
of the sticking coefficient.

00:56:28.140 --> 00:56:30.020 align:middle line:84%
So sticking
coefficient is the knob

00:56:30.020 --> 00:56:33.500 align:middle line:84%
you want to turn if you
want to fill a trench.

00:56:33.500 --> 00:56:36.300 align:middle line:84%
Changing the n value
helped, but not a whole lot.

00:56:36.300 --> 00:56:39.560 align:middle line:84%
It was really lowering
the sticking coefficient.

00:56:39.560 --> 00:56:41.240 align:middle line:84%
You get much more
conformal coverage.

00:56:41.240 --> 00:56:43.400 align:middle line:84%
So you get on the sidewall
just about what you had.

00:56:43.400 --> 00:56:46.070 align:middle line:90%


00:56:46.070 --> 00:56:52.010 align:middle line:84%
So this is typical on A, this
view of things, the parameter

00:56:52.010 --> 00:56:52.580 align:middle line:90%
values.

00:56:52.580 --> 00:56:54.890 align:middle line:84%
n equals 1 and sticking
coefficient of 0.1

00:56:54.890 --> 00:57:00.290 align:middle line:84%
is very typical of LTL, so low
temperature oxide or CVD SiO2.

00:57:00.290 --> 00:57:02.930 align:middle line:84%
b with a sticking
coefficient of 1 and 100

00:57:02.930 --> 00:57:07.030 align:middle line:90%
is more typical of tungsten CVD.

00:57:07.030 --> 00:57:09.490 align:middle line:84%
So we need to reduce the
sticking coefficient if you

00:57:09.490 --> 00:57:14.710 align:middle line:90%
need more conformal deposition.

00:57:14.710 --> 00:57:16.300 align:middle line:90%
How about the sidewall angle?

00:57:16.300 --> 00:57:22.120 align:middle line:84%
So if I even go back
here, I look at this,

00:57:22.120 --> 00:57:23.920 align:middle line:84%
I didn't do a perfect
job in this case

00:57:23.920 --> 00:57:24.878 align:middle line:90%
of filling this trench.

00:57:24.878 --> 00:57:27.790 align:middle line:84%
It look like it's going to pinch
off and form a void before I

00:57:27.790 --> 00:57:29.218 align:middle line:90%
get the whole thing filled.

00:57:29.218 --> 00:57:31.510 align:middle line:84%
Even here it doesn't look
all necessarily that perfect.

00:57:31.510 --> 00:57:33.730 align:middle line:90%
So what can we do?

00:57:33.730 --> 00:57:36.260 align:middle line:84%
You only have so much latitude,
you're sticking coefficient.

00:57:36.260 --> 00:57:38.677 align:middle line:84%
You can change the pressure
and do things in your reactor.

00:57:38.677 --> 00:57:40.630 align:middle line:84%
But you only have
so much latitude.

00:57:40.630 --> 00:57:43.150 align:middle line:84%
Well, what you do is you
change the topography

00:57:43.150 --> 00:57:44.450 align:middle line:90%
that you're starting with.

00:57:44.450 --> 00:57:48.700 align:middle line:84%
So these examples are results
of SPEEDIE simulations

00:57:48.700 --> 00:57:52.658 align:middle line:84%
where you're doing
LPCVD into a trench.

00:57:52.658 --> 00:57:54.200 align:middle line:84%
And we've changed
the sidewall angle.

00:57:54.200 --> 00:57:55.890 align:middle line:84%
Here, the trench has
a 90 degree angle,

00:57:55.890 --> 00:57:57.590 align:middle line:84%
so the side walls
go straight down.

00:57:57.590 --> 00:58:00.600 align:middle line:84%
Here, it's opened up
slightly by 5 degrees.

00:58:00.600 --> 00:58:02.610 align:middle line:90%
So this is an 85 degree angle.

00:58:02.610 --> 00:58:06.380 align:middle line:84%
And here you open up a little
bit more, 80 degree angle.

00:58:06.380 --> 00:58:10.130 align:middle line:84%
This has a sticking coefficient
of 0.2 and an n of 1.

00:58:10.130 --> 00:58:14.150 align:middle line:84%
So this is very typical of low
temperature oxide deposition,

00:58:14.150 --> 00:58:16.580 align:middle line:90%
for example, into a trench.

00:58:16.580 --> 00:58:21.097 align:middle line:84%
So if you decrease the
angle from 90 to 80 degrees,

00:58:21.097 --> 00:58:22.430 align:middle line:90%
you greatly improve the filling.

00:58:22.430 --> 00:58:23.990 align:middle line:84%
See at 90 degrees you're
going to pinch off

00:58:23.990 --> 00:58:25.282 align:middle line:90%
and you're going to get a void.

00:58:25.282 --> 00:58:26.720 align:middle line:84%
At 80 degrees
you're not going to.

00:58:26.720 --> 00:58:30.380 align:middle line:84%
So it's very common
in etching, when

00:58:30.380 --> 00:58:33.633 align:middle line:84%
you go to etch, to try to
etch a contact hole in a via,

00:58:33.633 --> 00:58:35.300 align:middle line:84%
you never want to
etch it straight down.

00:58:35.300 --> 00:58:39.680 align:middle line:84%
You always want to have a slight
angle, say make it 80 degrees

00:58:39.680 --> 00:58:43.940 align:middle line:84%
to slope this so that you
can get much better filling

00:58:43.940 --> 00:58:44.720 align:middle line:90%
of the hole.

00:58:44.720 --> 00:58:47.330 align:middle line:90%
Or if you're trying to make--

00:58:47.330 --> 00:58:50.840 align:middle line:84%
you want metal lines to go
over a step on your wafer,

00:58:50.840 --> 00:58:53.500 align:middle line:84%
you never want to make
the step look like this.

00:58:53.500 --> 00:58:55.500 align:middle line:84%
You usually want to
have it more sloped.

00:58:55.500 --> 00:58:58.890 align:middle line:84%
So you somehow slope the
step when you etch it,

00:58:58.890 --> 00:59:01.120 align:middle line:84%
or you put in side wall
spacers, or do something.

00:59:01.120 --> 00:59:03.840 align:middle line:84%
So the general idea, if you
want good step coverage,

00:59:03.840 --> 00:59:07.380 align:middle line:90%
don't make such abrupt steps.

00:59:07.380 --> 00:59:10.770 align:middle line:84%
If you're doing vias, you
can just decrease your angle

00:59:10.770 --> 00:59:14.820 align:middle line:84%
from 90 to 80 and you get much
better filling of the trench.

00:59:14.820 --> 00:59:18.780 align:middle line:90%


00:59:18.780 --> 00:59:22.890 align:middle line:84%
OK, how about there are a little
bit more complicated cases?

00:59:22.890 --> 00:59:26.370 align:middle line:84%
I've just shown very simple
cases, PVD without ions

00:59:26.370 --> 00:59:28.200 align:middle line:90%
or LPCVD without ions.

00:59:28.200 --> 00:59:30.420 align:middle line:84%
How about the case where
you do have an ion flux?

00:59:30.420 --> 00:59:32.790 align:middle line:84%
And there are a couple
of cases like that.

00:59:32.790 --> 00:59:36.300 align:middle line:84%
There is what's called HDP,
high density plasma CVD.

00:59:36.300 --> 00:59:39.570 align:middle line:84%
This has a very
high ion flux, could

00:59:39.570 --> 00:59:41.070 align:middle line:84%
be three or four
orders of magnitude

00:59:41.070 --> 00:59:47.010 align:middle line:84%
higher than what you
have in ordinary CVD.

00:59:47.010 --> 00:59:49.360 align:middle line:90%
So how does this work?

00:59:49.360 --> 00:59:52.620 align:middle line:84%
Well, think we mentioned
this at one point.

00:59:52.620 --> 00:59:56.550 align:middle line:84%
This particular one
has a microwave source.

00:59:56.550 --> 01:00:00.090 align:middle line:84%
What we have is we
have a plasma up here.

01:00:00.090 --> 01:00:03.960 align:middle line:84%
And there's a microwave supply
that's creating those ions.

01:00:03.960 --> 01:00:06.802 align:middle line:90%
But then it's created remotely.

01:00:06.802 --> 01:00:08.760 align:middle line:84%
So this ionized plasma
has a very high density,

01:00:08.760 --> 01:00:11.710 align:middle line:84%
but it's created remotely,
not directly over the wafer.

01:00:11.710 --> 01:00:15.450 align:middle line:84%
And then you have an RF bias
and you extract those ions

01:00:15.450 --> 01:00:17.100 align:middle line:90%
towards the wafer.

01:00:17.100 --> 01:00:19.540 align:middle line:84%
So the nice thing
about this is that you

01:00:19.540 --> 01:00:22.450 align:middle line:84%
can get a very high
density without having

01:00:22.450 --> 01:00:27.890 align:middle line:84%
huge energies, huge voltages,
to extract them to the wafer

01:00:27.890 --> 01:00:31.580 align:middle line:90%
so you don't get so much damage.

01:00:31.580 --> 01:00:38.960 align:middle line:84%
And this high density plasma
can give you a very high CVD dep

01:00:38.960 --> 01:00:42.230 align:middle line:84%
rate, even down to
a room temperature

01:00:42.230 --> 01:00:44.940 align:middle line:90%
with relatively low pressures.

01:00:44.940 --> 01:00:46.670 align:middle line:84%
So the key is you
have a separate RF

01:00:46.670 --> 01:00:48.770 align:middle line:90%
bias applied to the substrate.

01:00:48.770 --> 01:00:50.600 align:middle line:84%
That controls the
angular dependence

01:00:50.600 --> 01:00:56.250 align:middle line:84%
of what comes down and of ion
sputtering during deposition.

01:00:56.250 --> 01:00:58.800 align:middle line:84%
So we have a direct
ion flux coming down

01:00:58.800 --> 01:01:00.150 align:middle line:90%
like this on the surface.

01:01:00.150 --> 01:01:02.910 align:middle line:84%
And we have ions that
come down and sputter off.

01:01:02.910 --> 01:01:04.740 align:middle line:84%
And now here's where
our resputter flux

01:01:04.740 --> 01:01:07.800 align:middle line:84%
becomes important for these
high density plasma systems.

01:01:07.800 --> 01:01:09.660 align:middle line:84%
And the thing that
we need to realize

01:01:09.660 --> 01:01:12.030 align:middle line:84%
is because of the angular
dependence of sputtering,

01:01:12.030 --> 01:01:16.080 align:middle line:84%
sputtering occurs preferentially
on a slope surface rather than

01:01:16.080 --> 01:01:18.840 align:middle line:84%
a surface that's either
vertical or horizontal.

01:01:18.840 --> 01:01:21.600 align:middle line:84%
Because, remember, that
sputtering rate sort of

01:01:21.600 --> 01:01:23.230 align:middle line:90%
peaked at around 60 degrees.

01:01:23.230 --> 01:01:25.020 align:middle line:84%
So if you have a
sloped surface, you

01:01:25.020 --> 01:01:26.400 align:middle line:90%
get preferential sputtering.

01:01:26.400 --> 01:01:29.610 align:middle line:84%
So you can actually use
these high density plasma

01:01:29.610 --> 01:01:32.030 align:middle line:90%
systems to do planarization.

01:01:32.030 --> 01:01:34.530 align:middle line:84%
Now, all along I've been talking
about conformal deposition.

01:01:34.530 --> 01:01:36.600 align:middle line:84%
You may not want to get
conformal deposition.

01:01:36.600 --> 01:01:38.010 align:middle line:90%
You may want planarized.

01:01:38.010 --> 01:01:40.380 align:middle line:84%
So what do I mean by a
planarized deposition?

01:01:40.380 --> 01:01:42.090 align:middle line:90%
Well, if you start out--

01:01:42.090 --> 01:01:45.820 align:middle line:84%
let's say your surface
topography looks like this.

01:01:45.820 --> 01:01:47.280 align:middle line:84%
You have a metal
line or something

01:01:47.280 --> 01:01:49.110 align:middle line:84%
and you want to
cover it with oxide,

01:01:49.110 --> 01:01:52.830 align:middle line:84%
but you want it to be
planar when you're done.

01:01:52.830 --> 01:01:55.320 align:middle line:84%
You'd like the surface to look
like that after deposition,

01:01:55.320 --> 01:01:56.250 align:middle line:90%
completely flat.

01:01:56.250 --> 01:01:58.740 align:middle line:84%
That's just the
opposite of conformal.

01:01:58.740 --> 01:02:02.570 align:middle line:84%
If it were conformal, right,
it would have looked like this.

01:02:02.570 --> 01:02:05.190 align:middle line:84%
It would reproduce
that big hump.

01:02:05.190 --> 01:02:08.250 align:middle line:84%
But if you're trying to do
planarization during deposition

01:02:08.250 --> 01:02:10.740 align:middle line:84%
without using CMP,
you'd love a process

01:02:10.740 --> 01:02:12.480 align:middle line:90%
that would deposit like this.

01:02:12.480 --> 01:02:13.780 align:middle line:90%
Well, how can you do that?

01:02:13.780 --> 01:02:16.350 align:middle line:84%
Well, there are some
processes that are self

01:02:16.350 --> 01:02:19.670 align:middle line:90%
planarizing during deposition.

01:02:19.670 --> 01:02:21.920 align:middle line:84%
And here's an here's an
example of such a process.

01:02:21.920 --> 01:02:24.200 align:middle line:84%
You need these
ionized techniques,

01:02:24.200 --> 01:02:26.600 align:middle line:84%
which in addition to
depositing, are doing

01:02:26.600 --> 01:02:28.740 align:middle line:90%
sputtering preferentially.

01:02:28.740 --> 01:02:33.320 align:middle line:84%
So here's an example on slide
31 of two SPEEDIE simulations.

01:02:33.320 --> 01:02:37.850 align:middle line:84%
On the left, I have low pressure
CVD, regular low pressure CVD.

01:02:37.850 --> 01:02:39.590 align:middle line:84%
So I have a line
like this and I'm

01:02:39.590 --> 01:02:41.420 align:middle line:90%
trying to cover it with oxide.

01:02:41.420 --> 01:02:43.415 align:middle line:84%
And you see you
started out with a bump

01:02:43.415 --> 01:02:44.540 align:middle line:90%
and you end up with a bump.

01:02:44.540 --> 01:02:45.623 align:middle line:90%
There is no planarization.

01:02:45.623 --> 01:02:47.970 align:middle line:90%
It's perfectly conforming.

01:02:47.970 --> 01:02:53.020 align:middle line:84%
In b, we've simulated this high
density plasma CVD deposition,

01:02:53.020 --> 01:02:55.140 align:middle line:90%
and it has a directed ion flux.

01:02:55.140 --> 01:02:59.620 align:middle line:84%
And the key is it has this angle
dependent sputtering, which

01:02:59.620 --> 01:03:02.560 align:middle line:84%
you end up with a little
bump but much more planarized

01:03:02.560 --> 01:03:04.030 align:middle line:90%
topography after deposition.

01:03:04.030 --> 01:03:06.880 align:middle line:84%
So if you had to do CMP
to planarize, on this one

01:03:06.880 --> 01:03:08.650 align:middle line:90%
you'd have to CMP quite a bit.

01:03:08.650 --> 01:03:11.920 align:middle line:84%
On this one, you'd probably have
to CMP only a little bit, just

01:03:11.920 --> 01:03:12.970 align:middle line:90%
a small amount.

01:03:12.970 --> 01:03:15.160 align:middle line:84%
And that's very
desirable because CMP

01:03:15.160 --> 01:03:16.705 align:middle line:90%
is a tricky process.

01:03:16.705 --> 01:03:19.550 align:middle line:84%
It introduces non-uniformity
and it's fairly expensive.

01:03:19.550 --> 01:03:22.330 align:middle line:84%
So if you can do self
planarizing deposition

01:03:22.330 --> 01:03:25.480 align:middle line:84%
with these fancy ionized
deposition systems,

01:03:25.480 --> 01:03:28.300 align:middle line:90%
you're much better off.

01:03:28.300 --> 01:03:30.710 align:middle line:84%
And I'll actually show
some real examples of that.

01:03:30.710 --> 01:03:34.000 align:middle line:84%
So besides depositing
over a line,

01:03:34.000 --> 01:03:36.670 align:middle line:84%
you can also use this
high density plasma CVD.

01:03:36.670 --> 01:03:39.250 align:middle line:84%
It's very good at
filling open spaces

01:03:39.250 --> 01:03:41.720 align:middle line:90%
and reducing void formation.

01:03:41.720 --> 01:03:44.740 align:middle line:84%
So here's an example here,
again, a SPEEDIE simulation

01:03:44.740 --> 01:03:45.650 align:middle line:90%
on the left.

01:03:45.650 --> 01:03:48.290 align:middle line:84%
I had a trench with a
relatively high aspect ratio.

01:03:48.290 --> 01:03:51.970 align:middle line:90%
This was that 1.25 aspect ratio.

01:03:51.970 --> 01:03:56.170 align:middle line:84%
By LPCVD, you see it pinches
off and you end up with a void.

01:03:56.170 --> 01:03:59.260 align:middle line:84%
And in order to do this, we
used a sticking coefficient

01:03:59.260 --> 01:04:02.920 align:middle line:84%
of 0.2 and an isotropic
arrival angle.

01:04:02.920 --> 01:04:04.570 align:middle line:90%
On the one on the left--

01:04:04.570 --> 01:04:06.790 align:middle line:84%
on the right, I'm sorry--
is high density plasma

01:04:06.790 --> 01:04:09.070 align:middle line:90%
deposition in the trench.

01:04:09.070 --> 01:04:12.310 align:middle line:90%
And you get much better filling.

01:04:12.310 --> 01:04:14.690 align:middle line:90%
You don't see the void.

01:04:14.690 --> 01:04:15.810 align:middle line:90%
Well, why does it do this?

01:04:15.810 --> 01:04:18.020 align:middle line:84%
Well, high density plasma
gives you better filling

01:04:18.020 --> 01:04:20.103 align:middle line:84%
because you combine this
highly directed ion flux.

01:04:20.103 --> 01:04:22.687 align:middle line:84%
So a lot of the ions are coming
straight down, and that helps.

01:04:22.687 --> 01:04:24.170 align:middle line:90%
They get into the trench.

01:04:24.170 --> 01:04:26.895 align:middle line:84%
So they're towards the
surface with this angle

01:04:26.895 --> 01:04:27.770 align:middle line:90%
dependent sputtering.

01:04:27.770 --> 01:04:29.300 align:middle line:84%
So the angular
dependent sputtering

01:04:29.300 --> 01:04:31.610 align:middle line:84%
tends to etch off any
of these overhangs.

01:04:31.610 --> 01:04:33.530 align:middle line:84%
As they form they
get etched off by

01:04:33.530 --> 01:04:35.130 align:middle line:90%
the sputtering preferentially.

01:04:35.130 --> 01:04:37.377 align:middle line:84%
So overhangs that develop
get sputtered away,

01:04:37.377 --> 01:04:39.710 align:middle line:84%
and you end up being able to
fill the trench pretty well

01:04:39.710 --> 01:04:41.542 align:middle line:90%
without a void.

01:04:41.542 --> 01:04:43.250 align:middle line:84%
Often, you do not want
voids in the film.

01:04:43.250 --> 01:04:44.975 align:middle line:84%
You don't want air
spaces in your chips.

01:04:44.975 --> 01:04:47.225 align:middle line:84%
So this is a way to do it
is that high density plasma.

01:04:47.225 --> 01:04:50.770 align:middle line:90%


01:04:50.770 --> 01:04:54.630 align:middle line:84%
Here's an example on slide
33 just to show you--

01:04:54.630 --> 01:04:58.650 align:middle line:84%
instead of just showing SPEEDIE
simulations, actual data.

01:04:58.650 --> 01:05:02.610 align:middle line:84%
These are scanning
electron micrograph images

01:05:02.610 --> 01:05:05.040 align:middle line:90%
of HDP oxide deposition.

01:05:05.040 --> 01:05:08.760 align:middle line:84%
And on the left, this was
a metal line you can see.

01:05:08.760 --> 01:05:11.860 align:middle line:84%
And we we're trying to
deposit oxide over that.

01:05:11.860 --> 01:05:13.380 align:middle line:84%
And again, if it
had been conformal,

01:05:13.380 --> 01:05:15.270 align:middle line:84%
you'd have a big
hump in your oxide.

01:05:15.270 --> 01:05:18.703 align:middle line:84%
But with high density plasma
CVD, which is not conformal,

01:05:18.703 --> 01:05:20.370 align:middle line:84%
all you end up with
pretty planar oxide.

01:05:20.370 --> 01:05:22.260 align:middle line:84%
You still have a little
bit of a bump there,

01:05:22.260 --> 01:05:24.870 align:middle line:84%
a very small little
bump, that you

01:05:24.870 --> 01:05:27.003 align:middle line:90%
would have to planarize away.

01:05:27.003 --> 01:05:28.920 align:middle line:84%
But the amount of CMP
you'd have to do on that

01:05:28.920 --> 01:05:31.930 align:middle line:90%
would be very minimal.

01:05:31.930 --> 01:05:35.410 align:middle line:84%
And again, so that's the case
of depositing over a line.

01:05:35.410 --> 01:05:37.390 align:middle line:84%
If you're depositing
oxide in a trench,

01:05:37.390 --> 01:05:39.400 align:middle line:84%
so here's an
example of a trench.

01:05:39.400 --> 01:05:42.040 align:middle line:84%
You have two metal lines, one
on the right, one on the left.

01:05:42.040 --> 01:05:44.290 align:middle line:84%
They're separated by
half a micron or so.

01:05:44.290 --> 01:05:46.390 align:middle line:84%
You want to completely
fill this without voids.

01:05:46.390 --> 01:05:50.200 align:middle line:84%
You can see you've
gotten excellent filling.

01:05:50.200 --> 01:05:53.230 align:middle line:84%
You did get some of
these strange, you know,

01:05:53.230 --> 01:05:57.590 align:middle line:84%
topographies because
of the ion effects.

01:05:57.590 --> 01:05:59.320 align:middle line:84%
But that would have
to be CMPed off.

01:05:59.320 --> 01:06:02.770 align:middle line:84%
But the key is you were able
to fill a very small space

01:06:02.770 --> 01:06:04.777 align:middle line:90%
without inducing voids.

01:06:04.777 --> 01:06:06.610 align:middle line:84%
And that would be a
problem if you're trying

01:06:06.610 --> 01:06:09.460 align:middle line:90%
to use, say, an LPCVD system.

01:06:09.460 --> 01:06:12.900 align:middle line:84%
So you can imagine looking
at these topographies,

01:06:12.900 --> 01:06:16.500 align:middle line:84%
simulating, and then
going back in SPEEDIE

01:06:16.500 --> 01:06:18.420 align:middle line:84%
and varying your
models to try to get

01:06:18.420 --> 01:06:22.890 align:middle line:84%
something that looks like what
you actually got from SCM.

01:06:22.890 --> 01:06:24.420 align:middle line:84%
And that's what
exactly what people

01:06:24.420 --> 01:06:25.650 align:middle line:90%
do in topography simulation.

01:06:25.650 --> 01:06:27.150 align:middle line:84%
Again, it's not
first principles.

01:06:27.150 --> 01:06:30.030 align:middle line:84%
You vary all these
different parameters.

01:06:30.030 --> 01:06:33.040 align:middle line:84%
The sputtering yield is a
function of angle, the n value,

01:06:33.040 --> 01:06:35.040 align:middle line:84%
which is the cosine theta
to the n distribution,

01:06:35.040 --> 01:06:36.082 align:middle line:90%
the sticking coefficient.

01:06:36.082 --> 01:06:38.910 align:middle line:84%
You vary all those until you
get something in your simulation

01:06:38.910 --> 01:06:42.780 align:middle line:84%
that looks somewhat close to
what you actually deposited.

01:06:42.780 --> 01:06:46.680 align:middle line:90%


01:06:46.680 --> 01:06:49.080 align:middle line:84%
Slide 34 shows the
case-- we haven't

01:06:49.080 --> 01:06:51.720 align:middle line:84%
had much chance to talk
about it, but this whole idea

01:06:51.720 --> 01:06:54.180 align:middle line:90%
of surface diffusion.

01:06:54.180 --> 01:06:56.880 align:middle line:84%
And this becomes
important only when

01:06:56.880 --> 01:07:00.840 align:middle line:84%
you're usually doing
high temperature PVD, say

01:07:00.840 --> 01:07:01.590 align:middle line:90%
for aluminum.

01:07:01.590 --> 01:07:05.250 align:middle line:84%
That's a practical example
that people sometimes do.

01:07:05.250 --> 01:07:08.070 align:middle line:84%
Again, all of these
issues tend to arise

01:07:08.070 --> 01:07:11.080 align:middle line:84%
when you have high aspect
ratios on the wafer.

01:07:11.080 --> 01:07:16.290 align:middle line:84%
So you have a very high
aspect ratio trench like this

01:07:16.290 --> 01:07:19.590 align:middle line:84%
and you're trying to
fill that with aluminum.

01:07:19.590 --> 01:07:25.200 align:middle line:84%
And so on A on the left is
a high aspect ratio trench

01:07:25.200 --> 01:07:26.310 align:middle line:90%
using PVD.

01:07:26.310 --> 01:07:30.690 align:middle line:84%
So we have a sticking
coefficient of 1, n equals 4.

01:07:30.690 --> 01:07:32.880 align:middle line:84%
So this could be a
sputtered situation.

01:07:32.880 --> 01:07:34.560 align:middle line:90%
And you have very poor filling.

01:07:34.560 --> 01:07:37.500 align:middle line:84%
In fact, you don't have much at
all aluminum on the side walls

01:07:37.500 --> 01:07:41.820 align:middle line:84%
if you weren't able to fill
the trench well at all.

01:07:41.820 --> 01:07:47.860 align:middle line:84%
In B, this is again, now this
is way of high temperature

01:07:47.860 --> 01:07:50.080 align:middle line:84%
PVD where we've raised
the surface of the wafer

01:07:50.080 --> 01:07:54.250 align:middle line:84%
up to about 400 degrees,
much better filling, not

01:07:54.250 --> 01:07:56.030 align:middle line:90%
completely, but much better.

01:07:56.030 --> 01:07:59.080 align:middle line:84%
And finally, if you do to a
deposition temperature of 550,

01:07:59.080 --> 01:08:00.190 align:middle line:90%
and you can't go to hot.

01:08:00.190 --> 01:08:02.117 align:middle line:90%
Aluminum melts at six something.

01:08:02.117 --> 01:08:02.950 align:middle line:90%
You'd be in trouble.

01:08:02.950 --> 01:08:05.405 align:middle line:84%
But at 550, you get a
lot of surface diffusion.

01:08:05.405 --> 01:08:07.780 align:middle line:84%
And you get a lot of reflow
of the aluminum, essentially,

01:08:07.780 --> 01:08:10.810 align:middle line:84%
and you completely filled
the trench, so much better

01:08:10.810 --> 01:08:12.410 align:middle line:90%
much smoother topography.

01:08:12.410 --> 01:08:13.570 align:middle line:90%
So that's an example.

01:08:13.570 --> 01:08:15.340 align:middle line:84%
When you get to very
high aspect ratios,

01:08:15.340 --> 01:08:18.710 align:middle line:84%
you cannot rely just
simply on sputtering.

01:08:18.710 --> 01:08:20.950 align:middle line:84%
And so you need to add
something to the system.

01:08:20.950 --> 01:08:23.920 align:middle line:84%
You add the surface
diffusion component

01:08:23.920 --> 01:08:25.330 align:middle line:84%
by raising the
wafer temperature.

01:08:25.330 --> 01:08:27.100 align:middle line:84%
So then you need
a special system

01:08:27.100 --> 01:08:28.779 align:middle line:84%
where the sputtering
system is designed

01:08:28.779 --> 01:08:32.740 align:middle line:84%
so it can heat the wafer up to
reasonably high temperatures

01:08:32.740 --> 01:08:34.855 align:middle line:84%
at which the species
will surface diffuse.

01:08:34.855 --> 01:08:39.720 align:middle line:90%


01:08:39.720 --> 01:08:43.080 align:middle line:84%
OK, so on slide 35 I
just want to summarize.

01:08:43.080 --> 01:08:47.790 align:middle line:84%
As I mentioned, this is the
last lecture on chapter 9.

01:08:47.790 --> 01:08:50.760 align:middle line:84%
We talked about important
issues for thin film deposition.

01:08:50.760 --> 01:08:52.660 align:middle line:84%
We said there are two
different properties,

01:08:52.660 --> 01:08:54.785 align:middle line:84%
the physical properties
and the chemical properties

01:08:54.785 --> 01:08:55.950 align:middle line:90%
of the film.

01:08:55.950 --> 01:08:59.220 align:middle line:84%
The coverage of
topography, for example,

01:08:59.220 --> 01:09:01.859 align:middle line:84%
this conformal deposition
and step coverage we said

01:09:01.859 --> 01:09:03.395 align:middle line:90%
were very important.

01:09:03.395 --> 01:09:04.770 align:middle line:84%
There are two main
techniques you

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need to keep in mind, chemical
vapor and physical vapor

01:09:07.140 --> 01:09:09.890 align:middle line:90%
deposition.

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If you have simple
models, the dep rate

01:09:12.439 --> 01:09:15.410 align:middle line:84%
is limited by either the
surface reaction rate--

01:09:15.410 --> 01:09:16.910 align:middle line:84%
that's usually at
low temperatures--

01:09:16.910 --> 01:09:20.300 align:middle line:84%
or the mass transfer through
the gas phase boundary layer.

01:09:20.300 --> 01:09:21.800 align:middle line:84%
That's usually at
high temperatures.

01:09:21.800 --> 01:09:25.069 align:middle line:90%


01:09:25.069 --> 01:09:27.830 align:middle line:84%
But you do have to take into
account shadowing and surface

01:09:27.830 --> 01:09:32.029 align:middle line:84%
features to model
the actual coverage.

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For PVD, these processes,
again, their names--

01:09:34.310 --> 01:09:37.290 align:middle line:84%
it's very physical
rather than chemical.

01:09:37.290 --> 01:09:40.500 align:middle line:84%
The arrival angle distribution
at the wafer surface

01:09:40.500 --> 01:09:44.130 align:middle line:84%
is important, that cosine
theta to the n term.

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In a lot of these
techniques, the species

01:09:45.960 --> 01:09:48.930 align:middle line:84%
arrive more vertical
to the wafer surface,

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and the sticking coefficient
tends to be one for PVD.

01:09:52.319 --> 01:09:55.290 align:middle line:84%
So PVD has a lot
of shadowing issues

01:09:55.290 --> 01:09:59.090 align:middle line:90%
that you need to keep in mind.

01:09:59.090 --> 01:10:03.890 align:middle line:84%
We model this by having a
sticking coefficient s sub c.

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And if you have a low
sticking coefficient,

01:10:08.120 --> 01:10:11.870 align:middle line:84%
say much less than 0.01 or
something like that or 0.001,

01:10:11.870 --> 01:10:14.450 align:middle line:84%
and you have an isotropic
arrival distribution,

01:10:14.450 --> 01:10:17.580 align:middle line:84%
you'll get much better
filling of holes.

01:10:17.580 --> 01:10:19.000 align:middle line:90%
But there are new techniques.

01:10:19.000 --> 01:10:21.420 align:middle line:84%
But this only works to a
certain extent this filling.

01:10:21.420 --> 01:10:26.550 align:middle line:84%
So the latest techniques use
these high density plasma

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and these ionized
sputtering techniques,

01:10:29.220 --> 01:10:32.490 align:middle line:84%
which have simultaneously
sputtering going on

01:10:32.490 --> 01:10:34.290 align:middle line:90%
at the same time as deposition.

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And this can be used to get good
gap filling and planarization.

01:10:37.860 --> 01:10:42.070 align:middle line:84%
So these are the most modern
techniques people use today.

01:10:42.070 --> 01:10:43.510 align:middle line:84%
There's a lot of
things we didn't

01:10:43.510 --> 01:10:46.450 align:middle line:84%
get to talk about in
chapter 9 in this course.

01:10:46.450 --> 01:10:49.450 align:middle line:84%
6774 is about front
end processing,

01:10:49.450 --> 01:10:52.835 align:middle line:84%
but we give the lion's share of
the time to oxidation diffusion

01:10:52.835 --> 01:10:53.710 align:middle line:90%
and ion implantation.

01:10:53.710 --> 01:10:55.930 align:middle line:84%
Most of the lectures
are on that.

01:10:55.930 --> 01:10:58.810 align:middle line:84%
If you really want to know
a lot more, if your thesis

01:10:58.810 --> 01:11:01.540 align:middle line:84%
research is going to be on
thin films, for example,

01:11:01.540 --> 01:11:02.890 align:middle line:90%
we didn't cover a lot of things.

01:11:02.890 --> 01:11:05.740 align:middle line:84%
We didn't talk at all about the
grain structure, the density,

01:11:05.740 --> 01:11:06.883 align:middle line:90%
the stress in the film.

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None of these things did
we have time to cover

01:11:08.800 --> 01:11:11.440 align:middle line:84%
and how to model
these properties.

01:11:11.440 --> 01:11:14.213 align:middle line:84%
There are courses that are more
thin film oriented courses,

01:11:14.213 --> 01:11:15.880 align:middle line:84%
like in the material
science department.

01:11:15.880 --> 01:11:18.400 align:middle line:84%
And if you really want
to know about thin films

01:11:18.400 --> 01:11:20.650 align:middle line:84%
beyond what's in
chapter 9, I would

01:11:20.650 --> 01:11:23.020 align:middle line:84%
recommend you look towards
some of those classes.

01:11:23.020 --> 01:11:24.940 align:middle line:84%
But I just wanted
to make it clear

01:11:24.940 --> 01:11:28.300 align:middle line:84%
that this is sort of the
minimum amount of information

01:11:28.300 --> 01:11:30.190 align:middle line:84%
you need to know for
front end processing

01:11:30.190 --> 01:11:33.850 align:middle line:84%
as far as thin film
dep and epi goes.

01:11:33.850 --> 01:11:36.550 align:middle line:84%
OK, I think that's
about all I have

01:11:36.550 --> 01:11:39.580 align:middle line:90%
in this for today's lecture.

01:11:39.580 --> 01:11:42.250 align:middle line:84%
As I mentioned at the beginning,
if you came in late, hopefully

01:11:42.250 --> 01:11:46.240 align:middle line:84%
you're working on
homework number 5.

01:11:46.240 --> 01:11:47.200 align:middle line:90%
It's due Thursday.

01:11:47.200 --> 01:11:49.510 align:middle line:90%
And I did bring the clipboard.

01:11:49.510 --> 01:11:52.623 align:middle line:84%
My assistant has
typed up her version

01:11:52.623 --> 01:11:54.790 align:middle line:84%
of what she thinks you're
going to be either talking

01:11:54.790 --> 01:11:55.690 align:middle line:90%
about or writing up.

01:11:55.690 --> 01:11:56.273 align:middle line:90%
You can check.

01:11:56.273 --> 01:11:57.650 align:middle line:90%
That I've approved all of them.

01:11:57.650 --> 01:11:59.108 align:middle line:84%
There's only one
person who doesn't

01:11:59.108 --> 01:12:00.233 align:middle line:90%
have anything listed there.

01:12:00.233 --> 01:12:01.941 align:middle line:84%
And if you're giving
an oral report, what

01:12:01.941 --> 01:12:03.970 align:middle line:84%
I'm going to do this
week is start scheduling

01:12:03.970 --> 01:12:07.210 align:middle line:84%
for the last week of classes
so you know which day you

01:12:07.210 --> 01:12:09.420 align:middle line:90%
have to give your oral report.

01:12:09.420 --> 01:12:10.980 align:middle line:84%
OK, good, well,
I'll look forward

01:12:10.980 --> 01:12:13.400 align:middle line:90%
to seeing you on Thursday then.

01:12:13.400 --> 01:12:14.000 align:middle line:90%