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.
ANNULAR AEROSPIKE NOZZLE WITH WIDELY-SPACED THRUST CHAMBERS, ENGINE INCLUDING THE ANNULAR AEROSPIKE NOZZLE, AND VEHICLE INCLUDING THE ENGINE
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
2025-03-05
Patent
Electronic Resource
English
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