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특허 상세정보

Overlapping stage burn for multistage launch vehicles

특허상세정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/40   
미국특허분류(USC) 102/377 ; 244/172 ; 60/225 ; 60/250
출원번호 US-0254601 (1988-10-07)
발명자 / 주소
  • Daniels Mark H. (Houston TX) Funk Jack (Houston TX) Evans Wyendell B. (Friendswood TX) Varner Christopher C. (Houston TX)
출원인 / 주소
  • Space Services, Incorporated (Houston TX 02)
인용정보 피인용 횟수 : 30  인용 특허 : 7
초록

The invention relates to a multistage launch vehicle and method of multistage launch vehicle operation in which at least one subsequent motor stage is ignited following lift-off in partially overlapping relationship with its immediately preceding motor stage prior to shut-down and staging of the preceding motor stage in order to effect positive thrust control over the launch vehicle throughout shut-down and staging of the preceding motor stage. Preferably, each of the motors comprising the subsequently fired motor stage is provided with a thrust profile ...

대표
청구항

A launch vehicle comprising first and second sequentially ignitible rocket motor stages, wherein each of said rocket motors stages is comprised of at least one solid rocket motor and means is provided for igniting the second stage rocket motor subsequent to vehicle lift-off while the launch vehicle is within the earth\s atmosphere in partially overlapping relationship with the first stage rocket motor prior to termination of first stage motor operation.

이 특허를 인용한 특허 (30)

  1. Featherstone, Mark, Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods.
  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. Tangirala, Venkat Eswarlu; Janssen, Jonathan Sebastian; Dean, Anthony John, Compact, low pressure-drop shock-driven combustor and rocket booster, pulse detonation based supersonic propulsion system employing the same.
  5. Featherstone, Mark, Control surfaces for use with high speed vehicles, and associated systems and methods.
  6. Featherstone, Mark; Boelitz, Frederick W.; Ramsey, Roger E.; Biggs, David M., Control surfaces for use with high speed vehicles, and associated systems and methods.
  7. Shiau, Chin; Facciano, Andrew, Digital interface unit (DIU) and method for controlling stages of a multi-stage missle.
  8. Keith Edward L. ; Bauer Thomas P., Economical launch vehicle.
  9. Castiel David ; Draim John ; Brosius Jay ; Schor Matthew, Elliptical orbit satellite, system, and deployment with controllable coverage characteristics.
  10. Shing Peter Kau, Employing booster trajectory in a payload inertial measurement unit.
  11. Lee A. Barker, Low earth orbit satellite constellation stationkeeping algorithm with absolute altitude control.
  12. 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 .
  13. 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 .
  14. 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 .
  15. Sisk David S., Mass producible launch system.
  16. Trudeau Howard D. ; Sutphin David L. ; Damon Donald E. ; Bedegrew Ernest R. ; Cabrera Filamon T. ; Pereyda Douglas B. ; MacDonald Robert J. ; Hada Daniel H. ; Havens Frank C. ; Tomasek Allan R. ; Tay, Method and system for rapidly assembling a launch vehicle.
  17. Hand, Michael Leslie, Multi-stage space launch systems with reusable thrust augmentation and associated methods.
  18. Hand, Michael Leslie, Multi-stage space launch systems with reusable thrust augmentation and associated methods.
  19. Chan Allan L. ; Connors James J. ; Epstein Kenneth W. ; Heath Robert M. ; Ogden Gene Spencer ; Prewitt Michael B. ; Wong Michael ; Szeto Edward W. ; Kennon David P. ; Vogel Michael J. ; Hsu Larry Y. , Orbital assist module and interstage.
  20. Chan Allan L. ; Heath Robert M. ; Mettler Steven D. ; Pham Chau N. ; Pereyda Douglas B. ; MacDonald Robert J. ; Epstein Kenneth W. ; Kennon David P., Payload housing and assembly joint for a launch vehicle.
  21. Facciano, Andrew B.; Ebel, James A.; Alkema, Michael; Travis, Robert D.; Saxton, Mike J., Projectile and method that include speed adjusting guidance and propulsion systems.
  22. Brewster Robert J. (2107 Cox Rd. Cocoa FL 32926), Range safety tracking and data processing system.
  23. Casillas, Eduardo D.; Shaeffer, Charlie W.; Joyner, Claude R.; Parsley, Randy C., Reusable space access launch vehicle system.
  24. Kirshman, David James; Fricker, Darren Alec; LeBar, James Francis, Rocket engine ignition flame reduction system.
  25. Vuillamy, Didier; Gazave, Robert, Rocket engine nozzle system.
  26. Lee, Gerald A.; Krene, Michael C., Rocket turbopump valves and associated systems and methods.
  27. Mbamalu, Othniel, Space vehicle system.
  28. Knight,Andrew F., Super-staged and continuously staged rocket.
  29. Ellinthorpe James William, System for upending/reclining launch vehicles.
  30. Drymon Thomas S., Utilizing high altitude long endurance unmanned airborne vehicle technology for airborne space lift range support.