A satellite assembly (402) is disclosed, including a satellite (413, 415) and a shroud (200). The satellite (413, 415) is stowed in a launch vehicle (124, Fig. 1) and the shroud (200) includes a frame (210) supporting a flexible thermal blanket (212) enclosing the satellite (413, 415).
SATELLITE THERMAL ENCLOSURE
THERMISCHES SATELLITENGEHÄUSE
ENCEINTE THERMIQUE POUR SATELLITE
22.06.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |