Systems and methods for a fully reusable upper stage for a multi-stage launch vehicle are provided. The reusable upper stage uses an aerospike engine for main propulsion and for vertical landing. A heat shield can include a plurality of scarfed nozzles embedded radially around a semi-spherical surface of the heat shield, wherein inboard surfaces of the plurality of scarfed nozzles collectively define an aerospike contour. The heat shield can be actively cooled to dissipate heat encountered during reentry of the upper stage.
REUSABLE UPPER STAGE ROCKET WITH AEROSPIKE ENGINE
2023-07-06
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
OPTIMIZED DUAL-EXPANDER AEROSPIKE NOZZLE UPPER STAGE ROCKET ENGINE
British Library Conference Proceedings | 2011
|Parametric Study of Dual-Expander Aerospike Nozzle Upper-Stage Rocket Engine
British Library Conference Proceedings | 2011
|Parametric Study of Dual-Expander Aerospike Nozzle Upper-Stage Rocket Engine
Online Contents | 2011
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