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Two stage launch vehicle and launch trajectory method 원문보기

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • B64C-037/02
  • B64D-005/00
  • B64F-001/04
  • B64G-001/40
출원번호 US-0283739 (1994-08-01)
발명자 / 주소
  • Stiennon Patrick J. G. (Madison WI)
출원인 / 주소
  • Gates
  • William Henry (Redmond WA 04)
인용정보 피인용 횟수 : 38  인용 특허 : 0

초록

A method of launching a two stage vehicle and a trajectory for use with a two stage vehicle which allows recovery of both stages at the launch site. This is accomplished by launching the first stage completely vertically so that on burnout the first stage is positioned directly above the recovery si

대표청구항

A method of launching payloads to earth orbit employing a two stage liquid fueled launch vehicle comprising the steps of: a) placing a payload on an upper stage having a velocity capability of between 24,000 ft/sec and 27,000 ft/sec when carrying the payload; b) placing the upper stage on a lower ro

이 특허를 인용한 특허 (38)

  1. Mueller, George E.; Cochran, David B.; Kohrs, Richard H., Active satellite dispenser for reusable launch vehicle.
  2. Featherstone, Mark, Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods.
  3. Featherstone, Mark, Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods.
  4. Featherstone, Mark, Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods.
  5. William James Clark ; Robert John Wetherall, Common bulkhead cryogenic propellant tank.
  6. Boelitz, Frederick W., Compensating for wind prior to engaging airborne propulsion devices.
  7. Featherstone, Mark, Control surfaces for use with high speed vehicles, and associated systems and methods.
  8. Featherstone, Mark; Boelitz, Frederick W.; Ramsey, Roger E.; Biggs, David M., Control surfaces for use with high speed vehicles, and associated systems and methods.
  9. Watts, Keith Peter, Counterweight based rocket launch platform.
  10. Cochran David B. ; Limerick Charles D., Delivering liquid propellant in a reusable booster stage.
  11. Luther, David I., In-line staged vehicle.
  12. McKinney,Bevin C.; Hudson,Gary C., Integrated abort rocket and orbital propulsion system.
  13. Auger, Valery; Balemboy, Christophe; Laine, Robert Andre; Perkinson, Marie-Claire, Landing device for a space probe, and landing method for a probe provided with such a device.
  14. Morris, Dennis E.; Little, Alfred, Launch abort and orbital maneuver system.
  15. Boelitz, Frederick W.; Featherstone, Mark; Gil, Christopher M.; Ramsey, Roger E.; Biggs, David M., Launch vehicles with fixed and deployable deceleration surfaces, and/or shaped fuel tanks, and associated systems and methods.
  16. Featherstone, Mark; Sanders, John Michael; Ramsey, Roger E.; Wetzel, Eric David, Launch vehicles with ring-shaped external elements, and associated systems and methods.
  17. Cochran David B., Liquid oxygen downcomer.
  18. Kiselev, Anatoly Ivanovich; Medvedev, Alexandr Alexeevich; Karrask, Vladimir Konstantinovich; Dermichev, Gennady Dmitrievich; Radugin, Igor Sergeevich; Petrokovsky, Sergei Alexandrovich; Ivanovich, E, METHOD FOR PLACING PAYLOAD IN ORBIT BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LIQUID ROCKET ENGINE SYSTEM (LRES), MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE .
  19. Kiselev, Anatoly Ivanovich; Medvedev, Alexandr Alexeevich; Karrask, Vladimir Konstantinovich; Dermichev, Gennady Dmitrievich; Radugin, Igor Sergeevich; Petrokovsky, Sergei Alexandrovich; Motorny, Evg, METHOD FOR PLACING PAYLOAD IN ORBIT BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LIQUID ROCKET ENGINE SYSTEM (LRES), MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE .
  20. Kiselev, Anatoly Ivanovich; Medvedev, Alexandr Alexeevich; Karrask, Vladimir Konstantinovich; Dermichev, Gennady Dmitrievich; Radugin, Igor Sergeevich; Petrokovsky, Sergei Alexandrovich; Motorny, Evg, METHOD FOR PLACING PAYLOAD IN ORBIT BY MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE LIQUID ROCKET ENGINE SYSTEM (LRES), MULTIFUNCTIONAL LAUNCH VEHICLE OF COMBINED SCHEME WITH CRUISE .
  21. Robert H. Ballard ; Maxwell W. Hunter, II ; Richard N. Jurmain ; Charles P. Kelley, Method of controlling acceleration of a spacecraft reentering the atmosphere to accommodate adventure travelers.
  22. Scott Harry ; Wurst Stephen G., Payload carry and launch system.
  23. Mueller George E. ; Cochran David B., Payload module.
  24. Boelitz, Frederick W.; Hilstad, Mark O., Predicting and correcting trajectories.
  25. Wainfan, Barnaby S.; James, Warren W.; Sokol, Daniel H., Process for recovering a spacecraft first stage.
  26. Mango, Frank S., Propellant management system and method for multiple booster rockets.
  27. Coraboeuf, Yohann; Dutheil, Jean-Philippe, Propulsion unit for reusable launch vehicle.
  28. Mueller George E. ; Pohl Henry O., Recoverable booster stage and recovery method.
  29. Hoover, Randall L., Releasable forward section of an underwater vehicle.
  30. Lee, Gerald A.; Krene, Michael C., Rocket turbopump valves and associated systems and methods.
  31. Bezos, Jeffrey P.; Lai, Gary; Findlay, Sean R., Sea landing of space launch vehicles and associated systems and methods.
  32. Bailey Richard A. ; Cohen Aaron ; Myers Dale D., System and method for controlling a re-entry vehicle.
  33. Smith, Norman Louis, System and method for return and landing of launch vehicle booster stage.
  34. Mueller,George E.; Lai,Gary; Taylor,Thomas C., System for use of external secondary payloads.
  35. Grayson, Gary D.; Hand, Michael L.; Cady, Edwin C., Thermally coupled liquid oxygen and liquid methane storage vessel.
  36. Mueller George E. ; Kistler Walter P. ; Johnson Thomas G. ; Pohl Henry O. ; McLain Chris ; Hill Allan S. ; Andrews Jason E. ; Taylor Thomas C. ; Cohen Aaron ; Myers Dale ; Bruckner Adam P. ; Knowles , Two-stage reusable earth-to-orbit aerospace vehicle and transport system.
  37. Drymon Thomas S., Utilizing high altitude long endurance unmanned airborne vehicle technology for airborne space lift range support.
  38. Penn, Jay P., X33 aeroshell and bell nozzle rocket engine launch vehicle.
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