U.S. patents available from 1976 to present.
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In orbit space transportation and recovery system

Patent 7070151 Issued on July 4, 2006. Estimated Expiration Date: Icon_subject January 9, 2024. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

3825211

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Inventor: Minovitch

Soft ride method for changing the altitude or position of a spacecraft in orbit
Patent #: 4943014
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Method for remotely powering a device such as a lunar rover
Patent #: 5260639
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More ...

Inventors

Assignee

Application

No. 10755200 filed on 01/09/2004

US 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 details

Examiners

Primary: Swiatek, Robert P.

Attorney, Agent or Firm

Foreign Patent References

  • 2 040 445 RU 07/01/1995

International Classes

B64G 1/10
B64G 1/40
B64G 1/64
B64G 1/54

Abstract

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.

Other References

  • EL Genk A Critical Review of Space Nuclear Power and Propulsion.
  • Barnett Nuclear Electric Propulsion.
  • JPL SP-100 Technical Summary Report—vol. 1—Executive Summary.
  • Olin Small Upper Stage.
  • Topaz II Proves to be a Gem for International Tech Transfer.
  • Litchford Prospects for Nuclear Electric Propulsion.
  • Collins Small Orbit Transfer Vehicle.
  • Hord CRC Handbook of Space Technology: Status and Projections.
  • Cohen The Grand Challenge: A New Plasma Thruster.
  • General Electric and NASA—Leaders in Space Technology.
  • TRW—A Low Cost Premium Performance OMV.
  • Lenard Insterstellar Rendezvous . . . .
  • Lenard Recent Progress . . . .
  • Godfroy Realistic Development . . . .
  • Lenard Technology Needs . . . .
  • Lipinski A Gas-Cooled Reactor . . . .
  • Lipinski Small Fission Power Systems for NEP.
  • Lipinski Small Fission Power Systems for Mars.
  • Lipinski NEP for a Kuiper Belt Object . . . .
  • Lipinski Fission-Based Electric Propulsion . . . .
  • Lenard Power System Requirements.
  • Lipinski A Fission-Powered Interstellar Precursor Mission.
  • Lenard Fission Electric Propulsion with MagSail . . . .
  • Lenard Technical Aspects . . . (Abstract Only—Paper Never Published).
  • Ortiz A Cost Analysis . . . .
  • Earley Reusable Space Tug Concepts.
  • Martin Nuclear Electric Propulsion of Spacecraft.
  • Jaffe Nuclear-Electric Reuseable . . . .
  • Lenard Nuclear Electric Propulsion for Enhanced Mars Sample Return Missions.
  • Schall Laser Radiation for Cleaning Space Debris . . . .
  • El-Genk Space Nuclear Power Systems.
  • Bruno Building Roadmaps . . . .
  • Deininger Arcjet Propulsion.
  • Shepherd Performance Criteria.
  • Loeb A Nuclear-Electric Propulsion Module for Advance Solar System Exploration . . . .
  • Barnett Nuclear Electric Propulasion.
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