公开(公告)号：WO2015138592A3

公开(公告)日：2015-11-26

申请号：PCT/US2015019936

申请日：2015-03-11

申请人： LOCKHEED CORP

发明人： BIBIGHAUS BRIAN P ,  SCIULLI DOMINIC ANTHONY ,  GOODZEIT NEIL E ,  MILIEN JOHNNY

IPC分类号： B64G1/26

CPC分类号： B64G1/26 ,  B64G1/222 ,  B64G1/405

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.

摘要翻译： 根据本发明的一些方面，航天器包括第一和第二多个推进器。 多个推进器通过构造成在收起位置和展开位置之间移动第一多个推进器的吊杆附接到航天器本体。 第一多个推进器的展开位置比第一多个推进器的收起位置更远。 第二多个推进器的展开位置比第二多个推进器的收起位置更靠南。 第一组多个推进器包括在东西方向彼此分离的第一推进器和第二推进器。 第二组推进器包括在东西方向彼此分离的第三推进器和第四推进器。