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특허 상세정보

Launch vehicles with ring-shaped external elements, and associated systems and methods

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/00    B64G-001/14    F42B-010/02    F42B-010/64    B64G-001/22    B64G-001/62    B64G-001/64    B64G-001/40    B64G-001/12   
출원번호 US-0833985 (2013-03-15)
등록번호 US-9487308 (2016-11-08)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Perkins Coie LLP
인용정보 피인용 횟수 : 0  인용 특허 : 33
초록

Launch vehicles with ring-shaped external elements, and associated systems and methods. A representative aerospace system includes a launch vehicle having a first end and a second end generally opposite the first end, with the launch vehicle being elongated along a vehicle axis extending between the first and second ends, and having an external, outwardly facing surface. The system can further include an annular element carried by the launch vehicle, the annular element having an external, inwardly-facing surface radially spaced apart from, and extending...

대표
청구항

1. An aerospace system, comprising: a launch vehicle having a first end and a second end generally opposite the first end, the launch vehicle being elongated along a vehicle axis extending between the first end and the second end and having an external, outwardly facing surface;an annular element fixedly attached to the launch vehicle, the annular element having an external, inwardly facing surface radially spaced apart from, and extending at least partially circumferentially around, the vehicle axis, the annular element having a first edge surface facin...

이 특허에 인용된 특허 (33)

  1. Rupert, John G.; Siewart, Jeff. 2-D projectile trajectory corrector. USP2003126666402.
  2. Gertsch Paul R. (San Diego CA). Aerodynamic braking system for recovering a space vehicle. USP1990014896847.
  3. Blevio, Sr.,Henry L.. Aerodynamically stable, high-lift, vertical takeoff aircraft. USP2007067226017.
  4. Wainfan Barnaby (Long Beach CA). Airplane with variable-incidence wing. USP1992025086993.
  5. Featherstone, Mark. Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods. USP2014118894016.
  6. Smith John R. (Kettering OH). Combined cycle ramjet engine. USP1984044441312.
  7. Boelitz, Frederick W.. Compensating for wind prior to engaging airborne propulsion devices. USP2013048424808.
  8. Frank Stephen J,GBX ; Hawkins David,GBX. Drag-producing aerodynamic device. USP1999025871173.
  9. Robert B. Spencer ; Thomas D. Megna ; James R. Greenwood ; Daniel J. Laintz. Fly back booster. USP2002096450452.
  10. 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. USP2013048408497.
  11. Kim Kyusik (5026 Rhoads Ave. Santa Barbara CA 93111). Liquid fuel prevaporization and back burning induction jet oval thrust transition tail pipe. USP1985024500052.
  12. Baker Brian C. ; Banks Johnny Edward. Method and apparatus for non-propulsive fin control in an air or sea vehicle using planar actuation. USP2001066247666.
  13. Kristensen Per Herbert,NOX ; S.o slashed.rhaug Lars Martin,NOX ; Lien Bj.o slashed.rn R.,NOX ; Johannessen Einar,NOX. Method for rocket launching. USP1999085932830.
  14. Kindem Bj.o slashed.rn,NOX ; Kristensen Per Herbert,NOX ; Lien Bj.o slashed.rn Reidar,NOX. Method for transferring a horizontally arranged rocket from a vessel to a floating structure located at sea. USP2000026024006.
  15. Kistler Walter Paul (Redmond WA). Methods and apparatus for reusable launch platform and reusable spacecraft. USP1997095667167.
  16. Demidov German V. (ul.Frunze ; d.9. ; kv.173 Kazan RUX 420033 ) Osipov Eduard S. (ul.M.Gorkogo ; d.6 ; kv.22 Kazan RUX 420015 ). Multipurpose airborne vehicle. USP1997015595358.
  17. Scott Harry ; Wurst Stephen G.. Payload carry and launch system. USP2001026193187.
  18. Armstrong, Paula J.; Wittkopp, Scott H.. Power transmission for a vehicle. USP2005086929576.
  19. Mueller George E. ; Pohl Henry O.. Recoverable booster stage and recovery method. USP2000126158693.
  20. Kendall Robert T. (Palos Verdes Estates CA) Kendall ; Jr. Robert T. (Grants Pass OR). Recovery system. USP1989054832288.
  21. Anatoly Ivanovich Kiselev RU; Alexandr Alexeevich Medvedev RU; Jury Nikolaevich Trufanov RU; Igor Sergeevich Radugin RU; Jury Leonidovich Kuznetsov RU; Alexandr Alexandrovich Pankevich RU; Genn. Reusable booster for the first stage of a launcher. USP2002096454216.
  22. Janeke,Charl E.. Reversible space plane. USP2008037344111.
  23. Alway, Peter Curtis; Alway, Robert Matthew. Rocket with backwards gliding recovery. USP2005086926576.
  24. Klestadt Ralph H. (Sherman Oaks CA). Rotationally mounted flexible band wing. USP1995055417393.
  25. Bezos, Jeffrey P.; Lai, Gary; Findlay, Sean R.. Sea landing of space launch vehicles and associated systems and methods. USP2014038678321.
  26. Meston Vyacheslav A. (Altufievskoe Shosse ; d.86 ; kv. 275 Moscow RUX 127349). Spacecraft with a crew escape system. USP1996065526999.
  27. Facciano Andrew B. (Oro Valley AZ) Eisentraut Rudolph A. (Tucson AZ) Haight Stephen D. (Tucson AZ) Lamberton Ryan D. (Tucson AZ) Smith John D. (Tucson AZ). Stage separation mechanism for space vehicles. USP1994065318255.
  28. Bailey Richard A. ; Cohen Aaron ; Myers Dale D.. System and method for controlling a re-entry vehicle. USP2000066076771.
  29. Fernandez, Ian M.; Venkatapathy, Ethiraj; Hamm, Kenneth R.. Transformable and reconfigurable entry, descent and landing systems and methods. USP2014058733706.
  30. Stiennon Patrick J. G. (Madison WI). Two stage launch vehicle and launch trajectory method. USP1996105568901.
  31. 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. USP1999075927653.
  32. Ebbert Marvin D. (San Diego CA) Gustin Russell G. (Jamul CA) Horbett Edward G. (San Diego CA) Edwards Jack J. (El Cajon CA) Adcock Clifton L. (San Diego CA). Unmanned vertical take-off and landing, horizontal cruise, air vehicle. USP1994035295643.
  33. Lane Jeffery G. ; French James R.. Vehicle rotation and control mechanism. USP1999025873549.