This project, undertaken through the Advanced Space Design Program, developed a 'Conceptual Design of a Two Stage To Orbit Spacecraft (TSTO).' The design developed utilizes a combination of air breathing and rocket propulsion systems and is fully reusable, with horizontal takeoff and landing capability. The orbiter is carried in an aerodynamically designed bay in the aft section of the booster vehicle to the staging altitude. This TSTO Spacecraft design meets the requirements of replacing the aging Space Shuttle system with a more easily maintained vehicle with more flexible mission capability.
Conceptual design of a two stage to orbit spacecraft
1993-03-04
Report
Keine Angabe
Englisch
Conceptual Design of a Two Stage to Orbit Spacecraft
NTIS | 1993
|Orbit Design of Spacecraft on Elliptical Orbit
Springer Verlag | 2018
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