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Title: US5813217: Ion beam thrust method
[ Derwent Title ]


Country: US United States of America

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10 pages

 
Inventor: Beall, James C.; Tucson, AZ 85735

Assignee: None

Published / Filed: 1998-09-29 / 1996-04-05

Application Number: US1996000627360

IPC Code: Advanced: B64G 1/40; F03H 1/00; B64G 1/10;
Core: B64G 1/22; B64G 1/00; more...
IPC-7: B64G 1/00; H05H 1/00;

ECLA Code: B64G1/40D; B64G1/40Z; F03H1/00;

U.S. Class: Current: 060/202; 060/203.1; 244/169; 244/171.1;
Original: 060/202; 244/172; 244/169; 060/203.1;

Field of Search: 060/202,203.1,200.1,204,228 244/158,169,172 315/111.81

Priority Number:
1996-04-05  US1996000627360

Abstract: A method for providing thrust to a space borne vehicle uses an ion beam current to deliver a continuous stream of mass to the vehicle. The mass stream is decelerated thereby transferring its momentum to the vehicle as thrust. The vehicle reaccelerates the mass stream projecting it back to it origin, and thus receives further thrust in reaction to the departing mass stream. The mass stream may be set up between two particle beam accelerators so that thrust is realized by both accelerators, or the beam may be merely received continuously by one accelerator. In both cases the thrust may be used for deep space acceleration to high velocities by a vehicle not carrying fuel or propellant and not near any natural energy source.

Attorney, Agent or Firm: Gene Scott-Patent Law & Venture Group ;

Primary / Asst. Examiners: Thorpe, Timothy; Kim, Ted

Maintenance Status: E1 Expired  Check current status

INPADOC Legal Status: Show legal status actions

Family: None

First Claim:
Show all 4 claims
What is claimed is:     1. An ion propulsion method for a first independent space borne PBA, and a second independent space borne PBA, the first and second PBA being on a common line of sight, the method comprising the steps of:
  • a) generating a first collimated, linear ion beam with the first PBA;
  • b) directing the first ion beam at the second PBA;
  • d) capturing the first ion beam with the second PBA;
  • e) generating a second ion beam at the second PBA;
  • f) directing the second ion beam at the first PBA;
  • g) capturing the second ion beam with the first PBA;
  • h) repeating steps (a) through (g) intermittently or continuously;
  • wherein the first and second ion beams move in parallel, spaced apart paths;
  • whereby momentum transfer between the first ion beam and the second PBA and the second ion beam and the first PBA is converted to thrust on the first and second PBA driving said first and second PBA apart or slowing the mutual approach of said first and second PBA.


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Forward References: Show 2 U.S. patent(s) that reference this one

       
U.S. References: Go to Result Set: All U.S. references   |  Forward references (2)   |   Backward references (13)   |   Citation Link

Buy
PDF
Patent  Pub.Date  Inventor Assignee   Title
Buy PDF- 5pp US3367114  1968-02 Webb   CONSTRUCTION AND METHOD OF ARRANGING A PLURALITY OF ION ENGINES TO FORM A CLUSTER
Buy PDF- 5pp US3535880  1970-10 Work et al.   ION BEAM DEFLECTION SYSTEM
Buy PDF- 5pp US3537266  1970-11 Mahadevan et al.   ION ENGINE THRUST MULTIPLIER
Buy PDF- 3pp US3552125  1971-01 Banks et al.   ION BEAM DEFLECTOR
Buy PDF- 9pp US3891160  1975-06 Minovitch   Microwave powered reusable orbiting space tug
Buy PDF- 7pp US4028579  1977-06 King  Hughes Aircraft Company High current density ion source
Buy PDF- 8pp US4209703  1980-06 Delcroix et al.   Source for plasma of large transverse section and constituting an ion accelerator
Buy PDF- 7pp US4899084  1990-02 Post  The United States of America as represented by the United States Department of Energy Particle accelerator employing transient space charge potentials
Buy PDF- 5pp US5007348  1991-04 Pinson  The Boeing Company Spherical projectile for electromagnetic acceleration
Buy PDF- 7pp US5146742  1992-09 Iida et al.  NEC Corporation Ion thruster for interplanetary space mission
Buy PDF- 13pp US5305974  1994-04 Willis   Spaceship propulsion by momentum transfer
Buy PDF- 7pp US5369953  1994-12 Brophy  The United States of America as represented by the Administrator of the National Aeronautics and Space Administration Three-grid accelerator system for an ion propulsion engine
Buy PDF- 18pp US5489312  1996-02 Willis  BASF Aktiengesellschaft Cyan mixtures for dye transfer
       
Foreign References:
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PDF
Publication Date IPC Code Assignee   Title
Buy PDF- 26pp WO9007450 1990-07  B64G 1/22 FORWARD, Robert, L. STATITE APPARATUS AND METHOD OF USE 


Other Abstract Info: DERABS G1998-541232 DERABS G1998-541232

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