A reusable orbital vehicle (14) for a space transport system (10) comprises a fuselage (22) the shape of which widens in a direction extending from the front end (24) of the reusable orbital vehicle to a rear end (26) of said fuselage (22) and inside which there is defined a housing (32), and a crew-evacuation vehicle (34) housed in said housing (32) and oriented in such a way as to be extracted from the housing (32) in a direction (D1) directed from said rear end (26) of the fuselage (22) toward said front end (24) of the reusable orbital vehicle (14).
VEHICULE ORBITAL REUTILISABLE COMPRENANT UN VEHICULE D'EVACUATION D'EQUIPAGE A EXTRACTION VERS L'AVANT
REUSABLE ORBITAL VEHICLE COMPRISING A CREW-EVACUATION VEHICLE EXTRACTED FROM THE FRONT
WIEDERVERWENDBARES ORBITALFAHRZEUG MIT EINEM AUS DER VORDERSEITE EXTRAHIERTEN BESATZUNGSEVAKUIERUNGSFAHRZEUG
2025-05-21
Patent
Electronic Resource
French
IPC: | B64G Raumfahrt , COSMONAUTICS |
European Patent Office | 2024
|European Patent Office | 2024
|European Patent Office | 2024
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