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특허 상세정보

Aerospike for attachment to space vehicle system

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/64    B64G-001/52    B64C-001/38   
미국특허분류(USC) 244/161 ; 244/1N ; 244/130 ; 244/163
출원번호 US-0636292 (1984-07-31)
발명자 / 주소
인용정보 피인용 횟수 : 28  인용 특허 : 1
초록

An aerospike is adapted to be attached to the front nose of an aerodynamically asymmetric space vehicle system, such as the external tank and orbiter of the space shuttle. The aerospike basically comprises a tapered elongated portion having a first end which is adapted to be attached to the nose of the space vehicle, and a second free end terminating in a substantially rounded disc-like tip member. Use of the spike reduces aerodynamic heating and drag during ascent of the space vehicle into its orbital position, provides an attachment point for tether op...

대표
청구항

An aerospike adapted to be attached to a nose of an aerodynamically asymmetrical space vehicle system, said aerospike comprising an elongated portion having a first end adapted to be attached to said nose and a second end distant from said nose, said aerospike further comprising a disc-shaped tip member with a substantially curved front surface which is integrally formed with said second end of said elongated portion, said elongated portion being rigid and comprising means for attaching said vehicle system to another object in space, said system further ...

이 특허를 인용한 특허 피인용횟수: 28

  1. Schoonmaker, Michael J.; Sowers, George. Aerodynamic fairing. USP2003046554228.
  2. Tidman Derek A. (Falls Church VA). Apparatus and method for facilitating supersonic motion of bodies through the atmosphere. USP1990044917335.
  3. Sackheim, Robert L.; Hutt, John J.; Anderson, William E.; Dressler, Gordon A.. Axisymmetric, throttleable non-gimballed rocket engine. USP2005116964154.
  4. Taylor Thomas C.. Centrifugal gravity habitation torus constructed of salvaged orbital debris. USP2001036206328.
  5. Grip, Robert Erik; Brown, John Joseph. Expandable nose cone. USP2015099132908.
  6. Schulein, Erich. Flying object for transonic or supersonic velocities. USP2014028657237.
  7. Lugg, Richard H.. Hypersonic aircraft. USP20190310232937.
  8. Conners, Timothy R.; Henne, Preston A.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2016119482155.
  9. Conners, Timothy R.; Howe, Donald C.; Henne, Preston A.. Isentropic compression inlet for supersonic aircraft. USP2012128333076.
  10. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012128327645.
  11. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Isentropic compression inlet for supersonic aircraft. USP2012108286434.
  12. Conners, Timothy R.. Low shock strength inlet. USP2013038393158.
  13. Conners, Timothy R.. Low shock strength inlet. USP2015059027583.
  14. Conners, Timothy R.. Low shock strength propulsion system. USP2014068739514.
  15. Conners, Timothy R.. Low shock strength propulsion system. USP2014078783039.
  16. Dunn Bruce P.,CAX. Method and apparatus for pressurized feeding of liquid propellants to a rocket engine. USP1999105961074.
  17. Runne, Kay; Srulijes, Julio. Method and apparatus for reducing pressure and temperature on the front of a missile at ultrasonic speed. USP2003066581870.
  18. Teter, Roger D.; Dunn, Steven A.; Meyer, J. William. Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy. USP2010057721997.
  19. Teter,Roger D.; Dunn,Steven A.; Meyer,J. William. Method and system for providing cruciform steered, bent biconic and plasma suppression for maximum accuracy. USP2007097267303.
  20. Kobayashi,Hiroaki; Tanatsugu,Nobuhiro; Sato,Tetsuya; Hongo,Motoyuki; Maru,Yusuke. Method for reducing resistance of flying object using expandable nose cone. USP2006107118072.
  21. Arata,Allen A.. Movable nose cap and control strut assembly for supersonic aircraft. USP2007107278609.
  22. Johnson,Michael D.; Baker,James D.; Eichstadt,Frank T.; Bain,Michael E.. Multipurpose modular spacecraft. USP2007057219859.
  23. Mbamalu, Othniel. Space vehicle system. USP20180710023329.
  24. Henne, Preston A.; Conners, Timothy R.; Howe, Donald C.. Supersonic aircraft jet engine installation. USP2016059334801.
  25. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2004036698684.
  26. Henne, Preston A.; Howe, Donald C.; Wolz, Robert R.; Hancock, Jr., Jimmy L.. Supersonic aircraft with spike for controlling and reducing sonic boom. USP2014078789789.
  27. Meyer,J. W.. System and method for reducing plasma induced communication disruption utilizing electrophilic injectant and sharp reentry vehicle nose shaping. USP2007077237752.
  28. Mueller,George E.; Lai,Gary; Taylor,Thomas C.. System for use of external secondary payloads. USP2008047354020.