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 US2004031885(A1) 申请公布日期 2004.02.19
申请号 US20020298138 申请日期 2002.11.15
申请人 D'AUSILIO ROBERT F.;LENARD ROGER X.;SOUTHARD BARI M. 发明人 D'AUSILIO ROBERT F.;LENARD ROGER X.;SOUTHARD BARI M.
分类号 B64G1/10;B64G1/22;B64G1/40;B64G1/42;B64G1/50;B64G1/64;B64G1/66;(IPC1-7):B64G1/62 主分类号 B64G1/10
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