A dual structure aerospace vehicle is described which has an aeroshell structure and an internally disposed separable and reusable integral tank/thrust structure. The tank/thrust structure is inuslated for cryogenic fuels and the cavity within aeroshell is insulated from the tank/thrust structure. An internal support ring within the cavity serves as an attachment for lugs on the tank/thrust structure via double hinges. The aft end of tank/thrust structure is provided with rocket engines and exit nozzles with a trunnion supporting the tank/thrust structure within the aeroshell.
Aerospace vehicle
1985-12-10
Sonstige
Keine Angabe
Englisch
NTIS | 1984
|SAE Technical Papers | 2019
SAE Technical Papers | 2010
SAE Technical Papers | 2003