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특허 상세정보

Reusable booster for the first stage of a launcher

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/62   
미국특허분류(USC) 244/160; 244/162
출원번호 US-0869273 (2001-08-08)
우선권정보 RU-0122487 (1999-10-26)
국제출원번호 PCT/RU00/00407 (2000-10-13)
§371/§102 date 20010808 (20010808)
국제공개번호 WO01/30653 (2001-05-03)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Burns, Doane, Swecker & Mathis, L.L.P.
인용정보 피인용 횟수 : 23  인용 특허 : 5
초록

A booster comprises a body including tanks for an oxidizer and fuel, a nose compartment with a dome, a between-tank section and an afterbody, a rocket engine installation, an all-moving wing with a unit for turning it and fixing in a position along the axis of the booster during the ascension step and in a position turned by 90.degree. during the return flight, horizontal and vertical fin assemblies, a triple-point support landing gear, aerodynamic control organs and units for jointing to the second stage of the launch vehicle. The booster is provided wi...

대표
청구항

1. A reusable booster of the first stage of a launch vehicle, comprising a body including tanks for oxidizer and fuel, a nose compartment with a dome, a between-tank section and an afterbody, a rocket engine installation, a straight all-moving wing with a unit for turning it and fixing in a position along the axis of the booster during the ascension step and in a position turned by 90.degree. during return flight, horizontal and vertical fin assemblies, a triple-point support landing gear consisting of two main supports mounted on the booster body, and a...

이 특허를 인용한 특허 피인용횟수: 23

  1. Morgan, Robert W; Normoyle, James P; Wuest, Kurt J; Drake, David. Air vehicle with control surfaces and vectored thrust. USP2015099121680.
  2. Featherstone, Mark. Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods. USP2014118894016.
  3. Featherstone, Mark. Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods. USP2014118878111.
  4. Featherstone, Mark. Bidirectional control surfaces for use with high speed vehicles, and associated systems and methods. USP2014118876059.
  5. Williams, Sr., Lawrence Ellis. Centripetal aerodynamic platform spacecraft. USP20190410246200.
  6. Featherstone, Mark. Control surfaces for use with high speed vehicles, and associated systems and methods. USP2015038991767.
  7. Featherstone, Mark; Boelitz, Frederick W.; Ramsey, Roger E.; Biggs, David M.. Control surfaces for use with high speed vehicles, and associated systems and methods. USP2017029580191.
  8. Osdon, Tal. Fin deployment system. USP2018069989338.
  9. 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.
  10. Featherstone, Mark; Sanders, John Michael; Ramsey, Roger E.; Wetzel, Eric David. Launch vehicles with ring-shaped external elements, and associated systems and methods. USP2016119487308.
  11. Hand, Michael Leslie. Multi-stage space launch systems with reusable thrust augmentation and associated methods. USP2016109457918.
  12. Hand, Michael Leslie. Multi-stage space launch systems with reusable thrust augmentation and associated methods. USP2017069676498.
  13. Ball, James M.; Kutzmann, Aaron J.; Deamer, David A.. Multiple stage tractor propulsion vehicle. USP2015089114892.
  14. Ball, James M.; Kutzmann, Aaron J.; Deamer, David A.. Multiple stage tractor propulsion vehicle. USP2016089403605.
  15. Ustinov, Eugene Alexis. Non-powered, aero-assisted pre-stage for ballistic rockets and aero-assisted flight vehicles. USP2012058168929.
  16. Troy, John R.. Payload delivery vehicle and method. USP2010077753315.
  17. Wainfan, Barnaby S.; James, Warren W.; Sokol, Daniel H.. Process for recovering a spacecraft first stage. USP2010117834859.
  18. Coraboeuf, Yohann; Dutheil, Jean-Philippe. Propulsion unit for reusable launch vehicle. USP2018059981757.
  19. Barnes, Kenneth H.; Butler, William M.; Hagseth, Paul E.. Reusable flyback rocket booster and method for recovering same. USP2003096616092.
  20. Prampolini, Marco; Gogdet, Olivier. Reusable module for launcher. USP2015119174749.
  21. Bezos, Jeffrey P.; Lai, Gary; Findlay, Sean R.. Sea landing of space launch vehicles and associated systems and methods. USP2014038678321.
  22. Prampolini, Marco. Simplified reusable module for launcher. USP2014098844876.
  23. Smith, Norman Louis. System and method for return and landing of launch vehicle booster stage. USP2004116817580.