This document describes the detailed design requirements and design criteria to support Structures/TPS Technology development for SSTO winged vehicle configurations that use vertical take-off and horizontal landing and delivers 25,000 lb payloads to a 220 nm circular orbit at an inclination of 51.6 degrees or 40,000 lb payloads to a 150 nm circular orbit at a 28.5 degree inclination.
Requirements report for SSTO vertical take-off and horizontal landing vehicle
1994-11-04
Report
No indication
English
An Assessment of Take-Off and Landing Modes for Reusable SSTO Launchers
British Library Conference Proceedings | 1994
|Online Contents | 1995
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