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Delivering liquid propellant in a reusable booster stage

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64G-001/22
출원번호 US-0030645 (1998-02-25)
발명자 / 주소
  • Cochran David B.
  • Limerick Charles D.
출원인 / 주소
  • Kistler Aerospace Corporation
대리인 / 주소
    Baker Botts L.L.P.
인용정보 피인용 횟수 : 20  인용 특허 : 35

초록

A system is provided for delivering liquid propellant in a booster stage of a launch vehicle. The system includes an arrangement of tanks and valves to direct a first supply of liquid propellant during ascent of the booster stage and a second supply during descent of the booster stage. In disclosed

대표청구항

[ What is claimed is:] [1.] A system for delivering liquid propellant in a booster stage of a launch vehicle, the system comprising:a first tank operable to hold liquid propellant;a second tank connected in series with the first tank so that the liquid propellant flows from the first tank through th

이 특허에 인용된 특허 (35)

  1. Girard Alain (Cagnes Sur Mer FRX), Adaptable system for storing liquid under pressure and spacecraft propellant storage applications thereof.
  2. Rosen Harold A. (Santa Monica CA) Wittmann Alois (Palos Verdes CA), Apparatus and method for transporting a spacecraft and a fluid propellant from the earth to a substantially low gravity.
  3. Soeffker ; deceased Eduard (late of Berlin DEX) Soeffker ; heir by Klaus (Berlin DEX) Pattison ; nee Soeffker ; heir by Susanne (Achim DEX) Soeffker ; heir by Bettina (Achim DEX), Apparatus for storing propellant in a satellite.
  4. Martin James A. (Gloucester VA), Earth-to-orbit vehicle providing a reusable orbital stage.
  5. Bruhn Hansdieter (Bremen DEX), Fuel tank for aggressive liquid fuels.
  6. Palmer William R. (Melbourne FL), High altitude launch platform payload launching apparatus and method.
  7. Palmer William R. (Melbourne FL), High altitude launch platform payload launching apparatus and method.
  8. Palmer William R. (Melbourne FL), High altitude launch platform payload launching apparatus and method.
  9. Hardy Richard (Seattle WA) Hardy Jonathan (Seattle WA) Kornell Thomas J. (Federal Way WA) Tallquist Kenneth M. (Bellevue WA), Horizontal-takeoff transatmospheric launch system.
  10. Heye Donald R. (San Diego CA), In-line pressure balanced universal expansion joint.
  11. Martin James A. (Gloucester VA), Integrated launch and emergency vehicle system.
  12. Leonard Byron P. (13700 Tahiti Way Marina Del Rey CA 90292), Launch vehicle with interstage propellant manifolding.
  13. Adachi Kazuhide (No. 3393-7 Banchi Sunagawa ; Tachikawa ; Tokyo JA), Liquid fuel multistage rocket.
  14. Grove R. K. (Los Altos CA) King Ronald W. (San Francisco CA) L\Heureux Julie M. (Santa Clara CA), Liquid management apparatus for spacecraft.
  15. Perdu Michel (Frejus FRX), Liquid propellant supply device for spacecraft adapted to predict the end of its service life.
  16. Saccoccia Giorgio (Lisse NLX) Paganucci Fabrizio (Grosseto ITX) Scortecci Fabrizio (Rapolano Terme ITX), Method for re-orbiting a dual-mode propulsion geostationary spacecraft.
  17. Kistler Walter Paul (Redmond WA), Methods and apparatus for reusable launch platform and reusable spacecraft.
  18. Coffinberry George A. (West Chester OH), Multiple-propellant air vehicle and propulsion system.
  19. Coffinberry George A. (West Chester OH), Multiple-propellant air vehicle and propulsion system.
  20. Coffinberry George A. (West Chester OH), Multiple-propellant air vehicle and propulsion system.
  21. Lau Monica M. (Okeana OH) Coffinberry George A. (West Chester OH), Multiple-propellant air vehicle and propulsion system.
  22. Lau Monica M. (Okeana OH) Coffinberry George A. (West Chester OH), Multiple-propellant air vehicle and propulsion system.
  23. Leonard Byron P. (13700 Tahiti Way Marina Del Rey CA 90292), Multistage launch vehicle employing interstage propellant transfer and redundant staging.
  24. Koppel Christophe (St. Denis FRX), Optimized system for feeding a reignitable rocket engine.
  25. Schweickert Thomas F. (Collinsville IL) Orton George F. (St. Louis MO), Propellant tank resupply system.
  26. Foust Robert R. (Palm Beach FL), Rocket engine with redundant capabilities.
  27. Rider Todd (501 W. “A”St. North Little Rock AR 72116), Rocket staging system.
  28. Hamant James E. (Tempe AZ) McBride John R. (Phoenix AZ) Cubbage David H. (Chandler AZ), Satellite fueling system and method therefor.
  29. Kelly Michael S. (Redlands CA), Space launch vehicles configured as gliders and towed to launch altitude by conventional aircraft.
  30. Carmouche William J. (353 Stanford Ave. Baton Rouge LA 70808), Spaceship to harness radiations in interstellar flights.
  31. Gindre Philippe (Leiderdorp NLX) Hhnel Peter (Oegstgeest NLX) Helmke Hartmut (Leiden NLX), System for determining the depletion of propellant tanks onboard a spacecraft.
  32. Pulkowski Joseph A. (Ringoes NJ) Davies Keith (Robbinsville NJ) Young Marc B. (Plainsboro NJ) Lichtin Daniel A. (West Windsor NJ), Thermal fuel transfer and tank isolation to reduce unusable fuel.
  33. Marshall, William R., Three stage rocket vehicle with parallel staging.
  34. Stiennon Patrick J. G. (Madison WI), Two stage launch vehicle and launch trajectory method.
  35. MacConochie Ian O. (Yorktown VA) Briener Charles A. (Hampton VA), Two-stage earth-to-orbit transport with translating oblique wings for booster recovery.

이 특허를 인용한 특허 (20)

  1. Lopez, Alfredo; Grayson, Gary David; Addison, Stephen Michael, Antivortex device and method of assembling thereof.
  2. Grayson, Gary David; Addison, Stephen Michael, Antivortex device for multi-outlet liquid reservoir.
  3. Ford,Donald B., Asymmetrical low-profile bulkhead.
  4. Carpenter, Jon J.; Cronick, Jeffrey J.; Green, Jennifer L.; Lindley, Brian R.; Wechsler, James K., Autonomous orbit transfer vehicle.
  5. Watts, Keith Peter, Counterweight based rocket launch platform.
  6. Carpenter, Jon J.; Cronick, Jeffrey J.; Green, Jennifer L.; Lindley, Brian R.; Wechsler, James K.; Smith, Thomas R., Crewed on-orbit, returnable, and reusable space vehicle.
  7. Carpenter, Jon J.; Cronick, Jeffrey J.; Green, Jennifer L.; Lindley, Brian R.; Wechsler, James K.; Smith, Thomas R., Crewed on-orbit, returnable, and reusable space vehicle.
  8. Zeender, Peter; Wurst, Joseph Patrick, Cryogenic propellant depletion system for a launch vehicle.
  9. Henderson, John B.; Goodzeit, Neil E., Enhanced high-efficiency spacecraft propulsion system.
  10. Andrew E. Turner, Expendable launch vehicle.
  11. Robert B. Spencer ; Thomas D. Megna ; James R. Greenwood ; Daniel J. Laintz, Fly back booster.
  12. Mueller, George E.; Kohrs, Richard H.; Cochran, David B.; Cuzzupoli, Joseph W.; Limerick, Charles D.; Bailey, Richard A.; Johnson, Thomas G.; Knowles, Steven C., Logistics module system and method.
  13. Geneste, Jean-Francois; Poussin, Jean-Francois, Method of launching into operational orbit an artificial satellite and associated propulsion device.
  14. Johnson, Michael David; Hall, Baron, Modular spacecraft.
  15. Mango, Frank S., Propellant management system and method for multiple booster rockets.
  16. Mango,Frank S., Propellant management system and method for multiple booster rockets.
  17. Mazanek, Daniel D.; Mankins, John C., Reusable module for the storage, transportation, and supply of multiple propellants in a space environment.
  18. Casillas, Eduardo D.; Shaeffer, Charlie W.; Joyner, Claude R.; Parsley, Randy C., Reusable space access launch vehicle system.
  19. Bahn, Patrick R. E., Rocket stage and method of improving an existing rocket stage.
  20. Smith, Gregory H.; Martinez, Julio C.; Teran, Fernando C.; Reyes, Romy Andrade; Pauley, B. Wayne; Watkins, Randall W., Valve controller for pressure stabilization.
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