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 deliver 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 of inclination. This document will be updated on a timely basis as informatIon becomes available throughout the project.
Requirements report for SSTO vertical take-off/horizontal landing vehicle
1994-07-29
Report
Keine Angabe
Englisch
An Assessment of Take-Off and Landing Modes for Reusable SSTO Launchers
British Library Conference Proceedings | 1994
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