Nps Alternate Techsat Satellite, Design Project for Ae-4871

By: Nasa, National Aeronautics and Space Adm

This project was completed as part of AE-4871, Advanced Spacecraft Design. The intent of the course is to provide experience in the design of all the major components in a spacecraft system. Team members were given responsibility for the design of one of the six primary subsystems: power, structures, propulsion, attitude control, telemetry, tracking and control (TT&C), and thermal control. In addition, a single member worked on configuration control, launch vehicle integration, and a spacecraft test plan. Given an eleven week time constraint, a preliminary design of each subsystem was completed. Where possible, possible component selections were also made. Assistance for this project came principally from the Naval Research Laboratory's Spacecraft Technology Branch. Specific information on components was solicited from representatives in industry. The design project centers on a general purpose satellite bus that is currently being sought by the Strategic Defense Initiative. Unspecified Center SATELLITE DESIGN; SPACECRAFT PROPULSION; UNIVERSITY PROGRAM; ORBITAL MECHANICS; PROPULSION SYSTEM CONFIGURATIONS; SATELLITE ATTITUDE CONTROL; SPACECRAFT POWER SUPPLIES; SPACECRAFT TRACKING; TELEMETRY; TEMPERATURE CONTROL

• Format: Paperback
• Language: English
• ISBN: 1731240309
• ISBN13: 9781731240309
• Release Date: November 2018
• Publisher: Independently Published
• Length: 120 Pages
• Weight: 0.65 lbs.
• Dimensions: 0.3" x 8.5" x 11.0"