Method of launching into operational orbit an artificial satellite and associated propulsion device
AssigneeAstrium GmbH
InventorsJean-Francois Geneste, Jean-Francois Poussin
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AssigneeAstrium GmbH
InventorsJean-Francois Geneste, Jean-Francois Poussin
Estimating the term…
A method is disclosed for placing a satellite in an operational orbit. The satellite is equipped with its own satellite propulsion system as well as a detachable separate propulsion device. The satellite and separate propulsion device are launched into a transfer orbit by means of a space launcher. The separate propulsion device is controlled by a satellite. The satellite is transferred from the transfer orbit to an intermediate orbit by means of the separate propulsion device. The separate propulsion device is separated from the satellite in the intermediate orbit. The satellite then enters and operational orbit from the intermediate orbit by means of its own satellite propulsion system. The intermediate orbit is disposed between the transfer and operational orbits, and is in relatively close proximity to the operational orbit but is far enough away from the operational orbit to prevent possible interferences.
A method of launching a satellite into an operational orbit from a transfer orbit obtained by means of a space launcher, the satellite comprising a satellite propulsion system, compatible with launchers available on market which are not capable of direct launching into operational orbit, the method comprising:
Propulsion device, for the implementation of a method of launching a satellite into operational orbit from a transfer orbit obtained by means of a space launcher, the satellite comprising a satellite propulsion system, the method being compatible with launchers available on market which are not capable of direct launching into operational orbit, the method comprising at least the following stages:
Dependencies are inferred from the claim text.