Patent References 3825211 Transfer vehicle for use in conjunction with a reusable space shuttle Spacecraft for use in conjunction with a reusable space shuttle Apparatus and method of capturing an orbiting spacecraft Orbital maneuvering vehicle end effectors Satellite retrieval apparatus Self-refueling space propulsion system and operating method Soft ride method for changing the altitude or position of a spacecraft in orbit Method for remotely powering a device such as a lunar rover Space transfer vehicle InventorsAssigneeApplicationNo. 10755200 filed on 01/09/2004US Classes:244/171.1, With propulsion244/172.4, Rendezvous or docking244/171.7, With shield or other protective means (e.g., meteorite shield, insulation, radiation/plasma shield)244/172.2With fuel system detailsExaminersPrimary: Swiatek, Robert P.Attorney, Agent or FirmForeign Patent References
International ClassesB64G 1/10B64G 1/40 B64G 1/64 B64G 1/54 AbstractAn In Orbit Transportation & Recovery System (IOSTAR™) (10) One preferred embodiment of the present invention comprises a space tug powered by a nuclear reactor (19). The IOSTAR™ 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™ (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.Other References
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