An atmospheric re-entry vehicle includes a main body defining a forward end of the vehicle, a base defining an aft end of the vehicle, and a heat shield at the base. The heat shield includes a heat shield outer surface. The main body and the heat shield are configured such that a centerline of the heat shield is offset relative to a centerline of the main body. At least a portion of the heat shield outer surface is at least substantially axisymmetric relative to the centerline of the heat shield.


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    Titel :

    ANNULAR AEROSPIKE NOZZLE WITH WIDELY-SPACED THRUST CHAMBERS, ENGINE INCLUDING THE ANNULAR AEROSPIKE NOZZLE, AND VEHICLE INCLUDING THE ENGINE


    Weitere Titelangaben:

    RINGFÖRMIGE LUFTDÜSENANORDNUNG MIT WEIT BEABSTANDETEN SCHUBKAMMERN, MOTOR MIT DER RINGFÖRMIGEN LUFTDÜSENANORDNUNG UND FAHRZEUG MIT DEM MOTOR
    TUYÈRE ANNULAIRE DE TYPE AEROSPIKE POURVUE DE CHAMBRES PROPULSIVES LARGEMENT ESPACÉES, MOTEUR COMPRENANT LA TUYÈRE ANNULAIRE DE TYPE AEROSPIKE, ET VÉHICULE COMPRENANT LEDIT MOTEUR


    Beteiligte:
    MCCULLOUGH THOMAS RYAN (Autor:in) / FELDMAN THOMAS (Autor:in) / LAPSA ANDREW (Autor:in) / SANDER ZACHARY (Autor:in)

    Erscheinungsdatum :

    05.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS



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