The invention relates to an ejection unit for at least one satellite, in particular a picosatellite, comprising a frame that defines an inner space for receiving the satellite; and a retention device for holding the satellite in the inner space, the retention device being configured such that the satellite is releasable from the retention device.
Ejection unit for a satellite
2020-02-25
Patent
Electronic Resource
English
IPC: | B64G Raumfahrt , COSMONAUTICS |
Multipurpose Satellite Ejection System
NTIS | 1987
|NTRS | 1965
|A multipurpose satellite ejection system
NTRS | 1987
|