Pre-deployment battery power conservation for spacecraft
Embodiments of the present disclosure are directed to techniques for transitioning a spacecraft from a power-saving state to a power-consuming state at a time after launch of the spacecraft on a launch vehicle. Because the spacecraft can detect conditions for transitioning to the power-consuming state, commands received via an umbilical connection to the launch vehicle, or detecting the presence or absence of such a connection, is unnecessary, thereby removing several technical barriers to eliminating such umbilical connections altogether.
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.
2. The spacecraft of claim 1 , wherein the one or more power-consuming devices include a flight computer.
3. The spacecraft of claim 1 , wherein the one or more power-consuming devices are activated the one or more power-consuming devices are activated receiving at least one signal from at least one sensor of the spacecraft.
4. The spacecraft of claim 3 , wherein the at least one sensor includes at least one of a vacuum detection device, a contact switch, a vibration sensor, a wireless communication sensor, an optical sensor, and a spacecraft-to-spacecraft connectivity sensor.
5. The spacecraft of claim 3 , wherein the at least one sensor includes a plurality of sensors.
6. The spacecraft of claim 5 , wherein activating the one or more power-consuming systems based on signals received from a plurality of sensors includes activating the one or more power-consuming devices in response to detecting that a majority of the signals received from the sensors indicate an activation condition.
7. A method of launching a spacecraft into orbit, the method comprising:
loading the spacecraft with one or more power-consuming devices of the spacecraft in an inactive state onto a launch vehicle;
launching the launch vehicle;
detecting a condition for activating the power-consuming devices;
activating the one or more power-consuming devices after lift-off from Earth but prior to release from the launch vehicle; and
releasing the spacecraft from the launch vehicle.
8. The method of claim 7 , wherein activating the power-consuming devices includes activating a flight computer.
9. The method of claim 7 , wherein detecting a condition for activating the power-consuming devices includes receiving at least one signal from the at least one sensor of the spacecraft.
10. The method of claim 9 , wherein the at least one sensor includes at least one of a vacuum detection device, a contact switch, a vibration sensor, a wireless communication sensor, an optical sensor, and a spacecraft-to-spacecraft connectivity sensor.
11. The method of claim 9 , wherein receiving at least one signal from the at least one sensor of the spacecraft includes receiving a plurality of signals from a plurality of sensors.
12. The method of claim 7 , wherein determining whether the at least one signal indicates an activation condition includes determining whether a majority of the plurality of signals indicate an activation condition.
13. A spacecraft, comprising:
one or more power-consuming systems configured to be inactive prior to the spacecraft being deployed from a launch vehicle; and
one or more sensors that:
detect an activation condition associated with the spacecraft being deployed from the launch vehicle;
output activation signals indicating detection of the activation condition; and
a monitoring device configured to direct the one or more power-consuming systems to become active in response to receiving the activation signals from the one or more sensors.
14. A method for activating one or more power-consuming systems of a spacecraft, wherein the one or more power-consuming systems are configured to be inactive prior to the spacecraft being deployed from a launch vehicle, the method comprising:
receiving, by a monitoring device of the spacecraft, at least one signal from at least one sensor of the spacecraft;
determining, by the monitoring device, whether the at least one signal indicates the at least one sensor detected an activation condition associated with the spacecraft being deployed from the launch vehicle; and
in response to determining that the at least one signal indicates the at least one sensor detected the activation condition, directing, by the monitoring device, the one or more power-consuming systems to become active.