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.
AUSWURFEINHEIT FÜR EINEN SATELLITEN
EJECTION UNIT FOR A SATELLITE
BLOC DE LANCEMENT POUR UN SATELLITE
30.01.2019
Patent
Elektronische Ressource
Deutsch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Europäisches Patentamt | 2021
|Europäisches Patentamt | 2021
|