发明名称 In orbit space transportation & recovery system
摘要 An In Orbit Transportation & Recovery System (IOSTAR(TM)) ( 10 ) is disclosed. One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor ( 19 ). The IOSTAR(TM) includes a collapsible boom ( 11 ) connected at one end to a propellant tank ( 13 ) which stores fuel for an electric propulsion system ( 12 ). This end of the boom ( 11 ) is equipped with docking hardware ( 14 ) that is able to grasp and hold a satellite ( 15 ) and as a means to refill the tank ( 13 ). Radiator panels ( 16 ) mounted on the boom ( 11 ) dissipate heat from the reactor ( 19 ). A radiation shield ( 20 ) is situated next to the reactor ( 19 ) to protect the satellite payload ( 15 ) at the far end of the boom ( 11 ). The IOSTAR(TM) ( 10 ) will be capable of accomplishing rendezvous and docking maneuvers which will enable it to move spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.
申请公布号 US2005151022(A1) 申请公布日期 2005.07.14
申请号 US20040755200 申请日期 2004.01.09
申请人 D'AUSILIO ROBERT F.;LENARD ROGER X.;UPHOFF CHAUNCEY W.;WILLIAMS FRANKLIN H.JR. 发明人 D'AUSILIO ROBERT F.;LENARD ROGER X.;UPHOFF CHAUNCEY W.;WILLIAMS FRANKLIN H.JR.
分类号 B64C27/22;B64G1/00;B64G1/40;B64G1/42;B64G1/50;B64G1/64;F03H1/00;(IPC1-7):B64C27/22 主分类号 B64C27/22
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