16.851 | Fall 2003 | Graduate

Satellite Engineering

Assignments

ps4_cg_solution.pdf

Description:

Problem set and solution. Problem statement: The power and communications subsystems aboard a spacecraft interact with one another as a function of the spacecraft?s orbit to achieve a set of requirements. Determine the optimal combination of orbit size and inclination, solar array and battery sizes, communication subsystem power usage and antenna size, given a specified ground station.

Resource Type:
Assignments
pdf
ps4_cg_solution.pdf

Course Info

As Taught In
Fall 2003
Level
Learning Resource Types
Lecture Notes
Projects with Examples
Design Assignments with Examples
Programming Assignments with Examples