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Solid-propellant-powered maneuvering system for spacecraft

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) B64G-001/26    F42B-015/033   
미국특허분류(USC) 244/169 ; 244/171 ; 244/170 ; 244/172
출원번호 US-0660361 (1991-02-15)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 33  인용 특허 : 0
초록

An improvement to a variable-pressure solid-propellant-powered maneuvering system for spacecraft, enabling the system to operate for longer than one propellant burn time. At least two solid propellant gas generators are connected via a manifold to a plurality of nozzle valve clusters; at least one of the gas generators is connected to the manifold via a sequence valve which isolates that generator from the manifold until such time as it is desired to put that generator into operation.

대표
청구항
▼

In combination with a solid-propellant-powered maneuvering system for spacecraft having (1) a first gas generator set for providing a hot gas output said first set consisting of at least one gas generator each generator containing solid propellant and having an ignition means responsive to an ignition command, the burn rate of said propellant being directly related to the pressure of said gas output so that the rate of said gas output is directly related to the pressure of said gas output, (2) at least three nozzle valve clusters disposed to be mounted o...

이 특허를 인용한 특허 피인용횟수: 33

  1. Hultman, John A.. Adjustable range munition. USP2013128618455.
  2. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  3. Fenske Allen J. ; Gelderloos Hendrik C.. Dual fault tolerant actuator control system. USP1998075781398.
  4. Olden, Thomas A.; Wrigglesworth, Walter. Flight vehicles including electrically-interconnective support structures and methods for the manufacture thereof. USP2014098826640.
  5. Bergmann, Edward; London, Brian; Dineen, Andrew. Guidance control system for projectiles. USP2012098269156.
  6. Facciano, Andrew B; Alkema, Michael S; Leal, Michael A; Chasman, Daniel; Moore, Robert T. Integral injection thrust vector control with booster attitude control system. USP2015089115964.
  7. Rodden, John J.; Turner, Andrew E.. Method and system for synchronized forward and Aft thrust vector control. USP2004026695251.
  8. Facciano, Andrew B.; Moore, Robert T.; Hlavacek, Gregg J.; Do, Michael D.. Methods and apparatus for transferring a fluid. USP2011087989744.
  9. Sharpin, David; Kolanek, Jim; Cvetnic, Mark A.; Hutchings, Mike; Tennison, James; Nelson, Kent Carl; Hunsberger, Harold Kregg; Baseghi, Behshad. Methods and apparatuses for active protection from aerial threats. USP2015109170070.
  10. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for aerial interception of aerial threats. USP2017019551552.
  11. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP20190310228689.
  12. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP2016119501055.
  13. Cover, Cary Lee; Stroud, Sean Scott; Piovoso, Michael Joseph; Kelly, Timothy James. Methods of controlling thrust in a rocket motor. USP2013098539751.
  14. Olden, Thomas A.; Cavalleri, Robert J.. Modular divert and attitude control system. USP2012088242422.
  15. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016109469419.
  16. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2017079696726.
  17. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016069365300.
  18. Olden, Thomas A.; Cavalleri, Robert J.. Pellet-loaded multiple impulse rocket motor. USP2014038667776.
  19. Starken, George M.. Post boost control power assembly. USP2011017875838.
  20. Dryer, Richard L.. Projectile control device. USP2011128076623.
  21. Preston, Kenneth G.; Leal, Michael A.; Wilson, Rondell J.; Hussey, Richard C.. Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control. USP2014058735788.
  22. Cover, Cary Lee; Stroud, Sean Scott; Piovoso, Michael Joseph; Kelly, Timothy James. Propulsion thrust control system and method. USP2010057716912.
  23. Facciano, Andrew B.; Graves, William G.; Barker, Michael A.; Alkema, Michael S.; Larson, Jeffrey S.. Rocket cluster divert and attitude control system. USP2016069377279.
  24. Stroud, Sean S.; Piovoso, Michael J.. Rockets, methods of rocket control and methods of rocket evaluation utilizing pressure compensation. USP2017069677504.
  25. Onojima, Noboru; Tezuka, Hitoshi; Osada, Akira; Yamaguchi, Ichiro. Side thruster of flying object. USP2003016502384.
  26. Woessner, George T.; Abel, Stephen G.; Peck, Ronald A.; Baker, Mark H.; Christensen, Donald J.. Solid propellant burn rate, propellant gas flow rate, and propellant gas pressure pulse generation control system and method. USP2011027886519.
  27. Baker, Mark H.; Abel, Steve; Woessner, George. Solid propellant gas control system and method. USP2013098528316.
  28. Rohrbaugh,Eric M.; White,Jeffrey M.. Steerable, intermittently operable rocket propulsion system. USP2007107281367.
  29. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M. System and method for attitude control of a flight vehicle using pitch-over thrusters. USP2010127851732.
  30. Brinkerhoff, Robert S.; Mahnken, Michael J.; Loehr, Richard D.; Cook, James M.. System and method for attitude control of a flight vehicle using pitch-over thrusters and application to an active protection system. USP2011087989743.
  31. Olden, Thomas A.; Wrigglesworth, Walter. Systems and methods for composite structures with embedded interconnects. USP2014088809689.
  32. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.
  33. Abel, Stephen G.; Christensen, Donald J.. Two stage gas pilot valve controlling gas flow to a reaction jet nozzle. USP2003076598385.

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