A space vehicle includes: an aerospike nozzle formed on an aft end of the vehicle; a truncated spike including an outer edge and a surface formed on a rear portion of the truncated spike; and an annular ring outlet formed at the aft end of the vehicle between the outer edge of the truncated spike and an inner edge of the aft end of the space vehicle.
Reusable vertical take-off and landing space launch vehicle
2020-09-15
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Dynamic analysis for vertical soft landing of reusable launch vehicle with landing strut flexibility
SAGE Publications | 2019
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