Theses and Dissertations
Now showing items 1-1 of 1
Design considerations for the ORION satellite: structure, propulsion and attitude control subsystems for a small, general purpose spacecraft
(Monterey, California. Naval Postgraduate School, 1988-03)
A general purpose satellite (ORION) has been designed which will launch from the Space Shuttle using a NASA Get-Away-Special (GAS) canister. The design is based on the use of a new extended GAS canister and a low profile ...