Orbit space transportation and recovery system
An 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.
1. A method of operating a nuclear powered vehicle in orbit comprising the steps of:
providing said nuclear powered vehicle in orbit with a radiation shield ( 20 ) for protecting a detachable payload ( 15 );
providing said nuclear powered vehicle with a grasping means ( 14 ) extending outwardly therefrom at one end for docking and interacting with a plurality of other satellites; said grasping means ( 14 ) being configured for multiple use and for interacting with a plurality of different objects; said grasping means ( 14 ) including a plurality of segments;
configuring said plurality of segments to partially surround one of said plurality of different objects and to engage and to grasp said object without the need for any preconfigured docking interface on said object; and
providing controlled kinetic energy; said controlled kinetic energy for interacting with a plurality of other satellites.
2. A method as recited in claim 1 , in which said controlled kinetic energy is used to move a satellite.