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특허 상세정보

Two-stage earth-to-orbit transport with translating oblique wings for booster recovery

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-010/00   
미국특허분류(USC) 244/328 ; 244/46 ; 244/49 ; 244/172
출원번호 US-0433804 (1989-11-09)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 21  인용 특허 : 4
초록

A two-stage earth-to-orbit transport includes an orbiter vehicle and a pair of boosters, each having a depolyable oblique wing located along a longitudinal axis of the booster. The wing is deployed in an oblique disposition in supersonic and hypersonic speeds, and disposed at 90°for subsonic speeds encountered during entry. The oblique wing is driven axially and rotated by means of a turret mounted on rails.

대표
청구항

A two-stage earth-to-orbit transport comprising: an orbiter vehicle; a pair of boosters disposed at diametrically opposite sides of the orbiter, each having a deployable wing located on top of each booster along a longitudinal axis of each booster during launch and being movable into an oblique disposition after separation of the boosters from the orbiter vehicle; means for pivotally and slidably coupling each wing to each corresponding booster, the pivotal and slidable coupling means comprising for each booster a longitudinal track coupled to and center...

이 특허를 인용한 특허 피인용횟수: 21

  1. Morgan, Robert W; Normoyle, James P; Wuest, Kurt J; Drake, David. Air vehicle with control surfaces and vectored thrust. USP2015099121680.
  2. Cazals, Olivier; Druot, Thierry. Aircraft with a wing movable along the longitudinal axis of the fuselage. USP2013018360357.
  3. Carpenter, Jon J.; Cronick, Jeffrey J.; Green, Jennifer L.; Lindley, Brian R.; Wechsler, James K.. Autonomous orbit transfer vehicle. USP2003056568639.
  4. Pflug, William; Tillotson, Brian J.. Bilaterally asymmetric design for minimizing wave drag. USP2016129522727.
  5. Williams, Sr., Lawrence Ellis. Centripetal aerodynamic platform spacecraft. USP20190410246200.
  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. USP2003126666409.
  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. USP2003056557803.
  8. Cochran David B. ; Limerick Charles D.. Delivering liquid propellant in a reusable booster stage. USP2000096113032.
  9. Smith, Thomas R.; Bowcutt, Kevin G.. First and second stage aircraft coupled in tandem. USP2015028955791.
  10. Darbyshire, Ian T.. Flight control system for an aircraft. USP2004026685137.
  11. Luther, David I.. In-line staged horizontal takeoff and landing space plane. USP2013098528853.
  12. Hand, Michael Leslie. Multi-stage space launch systems with reusable thrust augmentation and associated methods. USP2016109457918.
  13. Hand, Michael Leslie. Multi-stage space launch systems with reusable thrust augmentation and associated methods. USP2017069676498.
  14. Mueller George E. ; Pohl Henry O.. Recoverable booster stage and recovery method. USP2000126158693.
  15. 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.
  16. Hall,Allison Earl. Space transportation system. USP2006077080809.
  17. Marshall ; Jr. Preston F. (Manassas VA) Chaskin Mel (Clifton VA). Space vehicle and method. USP1997105678784.
  18. Chen, Zhuo. Spacecraft and aerospace plane having scissors wings. USP2004066745979.
  19. Pflug, William; Tillotson, Brian J.. System and method for minimizing wave drag through bilaterally asymmetric design. USP2015038979018.
  20. Tyree, Anthony K.. System and method for navigating an object. USP2013088502126.
  21. Lane Jeffery G. ; French James R.. Vehicle rotation and control mechanism. USP1999025873549.