AE4870 Spacecraft Design and Integration I

Principles of spacecraft design considerations, spacecraft configurations, design of spacecraft subsystems, interdependency of designs of spacecraft subsystems, launch vehicles, mass power estimation, and trade-offs between performance, cost, and reliability. The emphasis is on military geosynchronous communications satellites. The course includes an individual design project.

Prerequisite

AE2820, AE3804, AE3851 or by consent of instructor

Lecture Hours

4

Lab Hours

0

Quarter Offered

  • Spring