An ejection method (100) for ejecting at least one payload such as a satellite. The ejection method includes a step (108) of ejecting the payload from a spacecraft that is driven by a continuous propulsion force when the satellite is ejected.
PROCÉDÉ D'ÉJECTION D'UNE CHARGE UTILE DEPUIS UN VÉHICULE SPATIAL ANIME D'UNE FORCE DE PROPULSION CONTINUE
METHOD FOR EJECTING A PAYLOAD FROM A SPACECRAFT DRIVEN BY A CONTINUOUS PROPULSION FORCE
VERFAHREN ZUM AUSSTOSSEN EINER NUTZLAST VON EINEM MIT KONTINUIERLICHER ANTRIEBSKRAFT ANGETRIEBENEN RAUMFAHRZEUG
2021-12-08
Patent
Electronic Resource
French
| IPC: | B64G Raumfahrt , COSMONAUTICS |
| European Patent Office | 2019
| European Patent Office | 2020
SYSTEME DE CALIBRATION DEPUIS LE SOL D'UNE CHARGE UTILE D'UN SATELLITE
| European Patent Office | 2020
| European Patent Office | 2015