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.


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    Titel :

    Requirements report for SSTO vertical take-off/horizontal landing vehicle


    Beteiligte:

    Erscheinungsdatum :

    1994-07-29


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch







    An Assessment of Take-Off and Landing Modes for Reusable SSTO Launchers

    Lacaze, H. / Boyeldieu, E. / Wagner, A. et al. | British Library Conference Proceedings | 1994


    VERTICAL TAKE OFF AND LANDING VEHICLE

    ROSS EDWIN ANTON / JOORE HANS / STEKELENBURG MICHAEL ALWIN WILLIAM et al. | Europäisches Patentamt | 2020

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