An ejection unit for a satellite comprises a housing (10) closed by a door (12-18) in which housing a guiding structure for the satellite is provided. The guiding structure comprises angle bars (50-56) and a clamping device for clamping the satellite in place by means of a clamping mechanism.
EJECTION UNIT
2024-09-26
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
NTRS | 1965
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