发明名称 THRUSTER ARRANGEMENT FOR GEOSYNCHRONOUS ORBIT SPACECRAFT
摘要 According to some aspects of the subject disclosure, a spacecraft comprises first and second pluralities of thrusters. The pluralities of thrusters are attached to a spacecraft body by booms configured to move the first plurality of thrusters between stowed and deployed positions. The deployed position of the first plurality of thrusters is farther north than is the stowed position of the first plurality of thrusters. The deployed position of the second plurality of thrusters is farther south than is the stowed position of the second plurality of thrusters. The first plurality of thrusters comprises a first thruster and a second thruster separated from each other in an east-west direction. The second plurality of thrusters comprises a third thruster and a fourth thruster separated from each other in the east-west direction.
申请公布号 WO2015138592(A2) 申请公布日期 2015.09.17
申请号 WO2015US19936 申请日期 2015.03.11
申请人 LOCKHEED MARTIN CORPORATION 发明人 BIBIGHAUS, BRIAN P.;SCIULLI, DOMINIC ANTHONY;GOODZEIT, NEIL E.;MILIEN, JOHNNY
分类号 B64G1/26 主分类号 B64G1/26
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