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특허 상세정보

Multi-use launch system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/14   
미국특허분류(USC) 244/158R ; 244/172 ; 244/2
출원번호 US-0349840 (1989-05-09)
발명자 / 주소
인용정보 피인용 횟수 : 28  인용 특허 : 0
초록

A multi-use launch system comprises a plurality of different modules releasably securable together into a plurality of different possible launch configurations. The modules include an at least partially expendable, unmanned first stage unit which is capable of single-stage-to-orbit operations on its own carrying internal or external payloads, or as part of a multi-stage-to-orbit system for higher payload capacity launches. The first stage unit is demountably securable to other first stage units, unpowered cargo-carrying units, and/or manned space vehicle...

대표
청구항

A multi-use launch system, comprising: a plurality of generally cylindrical modules selectably securable together in a variety of different possible launch configurations, the modules including: an at least partially expendable, unmanned first stage unit including primary propulsion means for boosting payloads up to a predetermined mass to a predetermined altitude and velocity, the primary propulsion means comprising means for selectively boosting the first stage unit alone from Earth into Earth orbit as a single-stage-to-orbit vehicle in one possible la...

이 특허를 인용한 특허 피인용횟수: 28

  1. Carpenter, Jon J.; Cronick, Jeffrey J.; Green, Jennifer L.; Lindley, Brian R.; Wechsler, James K.. Autonomous orbit transfer vehicle. USP2003056568639.
  2. Don A. Hart ; David W. Geyer. Configurable space launch system. USP2002036360994.
  3. 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. USP2003126666409.
  4. 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. USP2003056557803.
  5. Keith Edward L. ; Bauer Thomas P.. Economical launch vehicle. USP1998095799902.
  6. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2015028950703.
  7. Bayliss, Andrew J.; Paterson, John T.; Retz, Kevin. Independent power generation in aircraft. USP2014028657227.
  8. Thomas C. Taylor. Inflatable habitation volumes in space. USP2002086439508.
  9. McKinney,Bevin C.; Hudson,Gary C.. Integrated abort rocket and orbital propulsion system. USP2009027484692.
  10. Harry George Campbell ; Ronald Earle Hovden ; Glenn Woodrow Law. Janus reusable spacecraft system. USP2002096446905.
  11. Morris, Dennis E.; Little, Alfred. Launch abort and orbital maneuver system. USP2014058727283.
  12. Breit, Joseph Sherman; Witting, Michael Neil; Laib, Trevor; Rankin, Richard L.; Trela, John Anthony; Gates, Markland T.; Mansouri, Ali Reza. Localized utility power system for aircraft. USP2012078232670.
  13. 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 . USP2004036712319.
  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 . USP2004086769651.
  15. Lottes, Daniel. Motor vehicle with an electronic receptacle unit comprising a plurality of separate receptacle spaces configured to receive a plurality of function modules of a portable communications device. USP2018059975498.
  16. Aldrin, Buzz. Multi-crew modules for space flight. USP2004126827313.
  17. Criswell, David R.; Petersen, Jori L.. Power generating and distribution system and method. USP2013128596581.
  18. Sidney P. Glasser ; Charles J. Sosa. Propellant cross-feed system and method. USP2002126488237.
  19. Coraboeuf, Yohann; Dutheil, Jean-Philippe. Propulsion unit for reusable launch vehicle. USP2018059981757.
  20. Casillas, Eduardo D.; Shaeffer, Charlie W.; Joyner, Claude R.; Parsley, Randy C.. Reusable space access launch vehicle system. USP2004046726154.
  21. Kirshman, David James; Fricker, Darren Alec; LeBar, James Francis. Rocket engine ignition flame reduction system. USP2014058720181.
  22. Helou, Jr., Elie. Space shuttle orbiter and return system. USP2017039586700.
  23. Hall,Allison Earl. Space transportation system. USP2006077080809.
  24. Drymon Thomas S.. Utilizing high altitude long endurance unmanned airborne vehicle technology for airborne space lift range support. USP2001016176451.
  25. Karimi, Kamiar J.; Liu, Shengyi; Liffring, Mark E.; Helton, Steven B.; Fu, Sheau-Wei (Johnny). Vehicle electrical power management and distribution. USP2014058738268.
  26. Flanagan, Adam L.. Water rocket toys, assemblies, components, and methods. USP2016079393499.
  27. Nejad, Shah A.; Ihly, Rafael A.; Wangsvick, Chad. Wireless communication system and method for wireless signal communication in flight vehicles. USP2013048422951.
  28. Penn, Jay P.. X33 aeroshell and bell nozzle rocket engine launch vehicle. USP2004026685141.