The invention relates to a propulsion unit for a reusable launch vehicle including a rocket engine (4) supported by a cradle (2). According to the invention, said cradle (2) comprises at least three attachment elements (9) for assembling said unit on the structure of said vehicle to which said unit is to be connected; said at least three attachment elements defining a plane (12) for removing said unit, and in which said unit includes one or more fluid and/or electric links of said engine (4), each one of said links comprising a free end (11) to be assembled with a corresponding circuit for supplying the vehicle, to which said unit is to be connected, the tip of at least some of said free ends (11) being contained in said removal plane (12).


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    Titel :

    Propulsion unit for reusable launch vehicle


    Beteiligte:

    Erscheinungsdatum :

    24.02.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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    Reusable Launch Vehicle (RLV) Propulsion Technology

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    X-33-Reusable Launch Vehicle Propulsion Technology

    Smith, D. / AIAA | British Library Conference Proceedings | 1996