In orbit space transportation and recovery system

Aeronautics and astronautics – Spacecraft – With propulsion

Reexamination Certificate

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C244S171700

Reexamination Certificate

active

07461818

ABSTRACT:
A preferred In Orbit Transportation & Recovery System (IOSTAR™)(10) includes 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 fully deployed spacecraft between a low Earth parking orbit and positions in higher orbits or to other locations in our Solar System.

REFERENCES:
patent: 3465986 (1969-09-01), Milly
patent: 5734736 (1998-03-01), Palmer et al.
patent: 5806802 (1998-09-01), Scott
patent: 5883394 (1999-03-01), Mussman
patent: 6254035 (2001-07-01), Howard et al.
patent: 7070151 (2006-07-01), D'Ausilio et al.
Martin, A. R., “Nuclear Electric Propulsion of Spacecraft,” Journal of the British Interplanetary Society, Dec. 1995, vol. 48, No. 12, pp. 517-524.
Jet Propulsion Laboratory, “SP-100 Technical Summary Report: vol. I—Executive Summary,” Sep. 1994.

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