Emergency track departure device and emergency orbit departure method

摘要

An emergency orbit departure device 10 provided on an artificial satellite 100 that flies on orbit around the earthA propulsion device 27 for generating a thrust for releasing the satellite 100 from the orbitThe receiver 31 receives a repetitive signal repeatedly transmitted from the transmitter 21 of the satellite bus 3 at a distance in the artificial satelliteDuring the configuration timeIf the receiver 31 does not receive the repeat signal,OrWhen the receiver 31 receives the orbit departure command from the transmitter 21 or the outside of the artificial satelliteThe detector 33 outputs a detection signal to that effect.In response to the detection signalAn operating device 35 for operating the propulsion device 27It is provided separately from the power supply device 15 of the satellite busReceiving unitDetector 33A power supply 37 for supplying power to the operating device 35 is provided.