CPC B64G 1/428 (2013.01) [B64G 1/002 (2013.01); B64G 1/66 (2013.01)] | 14 Claims |
1. A spacecraft launch system, comprising:
a launch vehicle; and
at least one spacecraft removably attached to the launch vehicle, wherein the at least one spacecraft includes one or more power-consuming devices in an inactive state, wherein the one or more power-consuming devices of the at least one spacecraft are activated to an active state based on signals received by the at least one spacecraft after lift-off from Earth but prior to release from the launch vehicle.
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