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특허 상세정보

Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F42B-015/01    F41G-007/22    F42B-010/60    F42B-015/00    F41G-007/00    F42B-010/00   
미국특허분류(USC) 244/003.22; 244/003.1; 244/003.15; 244/003.16; 244/003.19; 244/003.21
출원번호 US-0030307 (2011-02-18)
등록번호 US-8735788 (2014-05-27)
발명자 / 주소
출원인 / 주소
대리인 / 주소
    Schwegman, Lundberg & Woessner, P.A.
인용정보 피인용 횟수 : 14  인용 특허 : 35
초록

Embodiments of a propulsion and maneuvering system that may be suitable for use during a terminal phase in an interceptor are generally described herein. The propulsion and maneuvering system may include one or more axial thrusters to provide thrust along axial thrust lines that run through a center-of-gravity of the interceptor and a plurality of divert thrusters to provide thrust in radial directions. The combination of divert and axial thrusters may allow the interceptor to respond to a maneuvering target and may allow the interceptor to increase its ...

대표
청구항

1. A propulsion and maneuvering system for use during a terminal phase of an interceptor, the system comprising: one or more axial thrusters to provide thrust along axial thrust lines that run through a center-of-gravity of the interceptor;a plurality of divert thrusters to provide thrust in radial directions; anda common propellant distribution manifold for distributing pressurized fuel to both the axial thrusters and the divert thrusters. 2. The propulsion and maneuvering system of claim 1 wherein the propulsion and maneuvering system includes two axia...

이 특허에 인용된 특허 (35)

  1. Hibma Richard A. ; Hilscher Richard W. ; Miralles Carlos T. ; Ward Jerry D. ; Wright Blaine G.. Apparatus for defending a vehicle against an approaching threat. USP2001056231003.
  2. East ; George F. ; Hallum ; Charles E.. Combined warm gas fin and reaction control servo. USP1978044085909.
  3. Metz Pierre (Paris FRX). Control device using gas jets for a guided missile. USP1984114482107.
  4. Douglass, Randle; Jacquin, H. George; Chewey, Paul M.; Galvan, Paul A.; Naragon, Richard S.. Dual pressure solid propellant control system. USP1985114550888.
  5. Ryan William F. (Phoenix AZ). Fluidic thruster control and method. USP1983114413795.
  6. Metz Pierre (Paris FRX). Gas jet steering device and method missile comprising such a device. USP1984084463921.
  7. Metz Pierre (Paris FRX). Guided projectile. USP1993085238204.
  8. Minick, Alan B.; Hobart, Stephen Alan; Widman, Frederick; Kokan, Timothy S.; Massey, Frederic H.. Guided projectile. USP2011027891298.
  9. Bagley Cloy J. (Fountain Valley CA). Lateral thruster for missiles. USP1990114967982.
  10. Leonard Byron P. (13700 Tahiti Way Marina Del Rey CA 90292). Launch vehicle with interstage propellant manifolding. USP1992085141181.
  11. Gundel, Bernd; Graf, Hans-Rainer; Hammer, Helmut; Thurner, Günther. Method and device for varying a flight path of a projectile by intentional tumbling of the projectile. USP2010067741588.
  12. Flament Patrick,FRX ; Perdu Michel,FRX ; Portier Jean,FRX ; Brunet Pierre,FRX. Method for controlling the pitch attitude of a satellite by means of solar radiation pressure. USP1998125850992.
  13. Krishnaswamy, Kailash; Bugajski, Dan. Methods and systems for controlling multi-body vehicles with fuel slosh. USP2009087580778.
  14. Whitehead John C. (Davis CA) Swink Don G. (Woodinville WA). Miniaturized pressurization system. USP1991065026259.
  15. Pinson George T. (Huntsville AL). Missile control surface actuator system. USP1987044659036.
  16. Mavroudakis,Peter J.; Boka,Jeffrey B.; Patel,Naresh R.. Missile identification and tracking system and method. USP2006047026980.
  17. Nathanson Harvey C. (Pittsburgh PA) Underwood Thomas E. (Edgewater MD). Multi-mode missile seeker system. USP1991105061930.
  18. Morris Joseph W. (Rancho Cordova CA) Carlson Russell W. (Folsom CA) Peterson Kevin L. (Sacramento CA) Reich Edward M. (Orangevale CA). Multiple pintle nozzle propulsion control system. USP1995105456425.
  19. Keigler John Edward (Princeton NJ) Muhlfelder Ludwig (Livingston NJ) Cenker Robert Joseph (Princeton NJ). Orientation system for a spin stabilized spacecraft. USP1976083977633.
  20. Pinson George T. (Huntsville AL). Pressure gas supply for a missile and the like. USP1987084684080.
  21. Metz Pierre (Paris FRX). Process for piloting and guiding projectiles in the terminal phase and a projectile comprising means for implementing th. USP1983104408735.
  22. Bar Klaus (Lauf DEX) Lehrieder Gunther (Rothenbach DEX). Projectile with correctable trajectory. USP1991105054712.
  23. Schweickert Thomas F. (Collinsville IL) Orton George F. (St. Louis MO). Propellant tank resupply system. USP1986094609169.
  24. Cover, Cary Lee; Stroud, Sean Scott; Piovoso, Michael Joseph; Kelly, Timothy James. Propulsion thrust control system and method. USP2010057716912.
  25. Machell Anthony (Stevenage GB2) Foulsham Peter G. (Stevenage GB2). Reaction control system. USP1990094955558.
  26. Davies Guy E. (Hampshire GB2). Reaction jet control system. USP1989084856734.
  27. Howell, W. Max. SSICM guidance and control concept. USP1985094542870.
  28. Campbell John G. (Northridge CA) Ruttle Daniel W. (Panorama City CA). Safe propulsion system for missile divert thrusters and attitude control thrusters and method for use of same. USP1996075533331.
  29. Sackheim Robert L. (Palos Verdes CA) Hook Dale L. (Rancho Palos Verdes CA) Joseph Gary W. (Torrance CA). Satellite propulsion and power system. USP1995055417049.
  30. Goddard Charles W. (San Jose CA) Lucas John T. (Los Altos CA) Galvan Paul A. (San Jose CA). Solid-propellant-powered maneuvering system for spacecraft. USP1991115062593.
  31. Sackheim Robert L. ; Bassichis James S. ; Hook Dale L.. Spacecraft attitude and velocity control thruster system. USP2000106135393.
  32. Rohrbaugh,Eric M.; White,Jeffrey M.. Steerable, intermittently operable rocket propulsion system. USP2007107281367.
  33. Bittle,David A.; Jimmerson,Gary T.; Cothran,Julian L.. Trajectory correction kit. USP2008087416154.
  34. Shankar Uday J. (Plainsboro NJ) Raman Kidambi V. (East Windsor NJ). Unified spacecraft attitude control system. USP1992085140525.
  35. Smith Gregory H. ; Clark Roland D.. Universal driver circuit for actuating both valves and ordnances. USP2001076267326.

이 특허를 인용한 특허 피인용횟수: 14

  1. Morgan, Robert W; Borg, Eric J; Leal, Michael A; Nicholl, Adam D. Air vehicle with bilateral steering thrusters. USP2015069068808.
  2. 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.
  3. Kaltenbach, Alexandre. Method and device for electric satellite propulsion. USP2017059650159.
  4. 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.
  5. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for aerial interception of aerial threats. USP2017019551552.
  6. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP20190310228689.
  7. Kolanek, James; Baseghi, Behshad; Sharpin, David; Visco, Anthony; Shieh, Falin. Methods and apparatuses for engagement management of aerial threats. USP2016119501055.
  8. Wood, James Richard. Missile, chemical plasm steering system, and method. USP20181010113844.
  9. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016019242745.
  10. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016109469419.
  11. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2017079696726.
  12. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016049302790.
  13. Fujita, Toshiharu; Hayakawa, Nobuaki. Orbit attitude control device, and method of controlling orbit attitude. USP2016069365300.
  14. Facciano, Andrew B.; Alkema, Michael S.; Moore, Robert T.. Rocket propelled payload with divert control system within nose cone. USP2015049018572.

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