METHOD FOR EJECTING A PAYLOAD FROM A SPACECRAFT DRIVEN BY A CONTINUOUS PROPULSION FORCE

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.

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Bibliographische Detailangaben
Hauptverfasser: CHAVY, Siegfrid, SANNINO, Jean-Michel, QUINQUIS, Isabelle
Format: Patent
Sprache:eng ; fre ; ger
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Zusammenfassung: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.