DE3261284D1 - Guided missile directional control using gas jets - Google Patents

Guided missile directional control using gas jets

Info

Publication number
DE3261284D1
DE3261284D1 DE8282401089T DE3261284T DE3261284D1 DE 3261284 D1 DE3261284 D1 DE 3261284D1 DE 8282401089 T DE8282401089 T DE 8282401089T DE 3261284 T DE3261284 T DE 3261284T DE 3261284 D1 DE3261284 D1 DE 3261284D1
Authority
DE
Germany
Prior art keywords
guided missile
gas jets
directional control
nozzles
gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
DE8282401089T
Other languages
English (en)
Inventor
Pierre Metz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
BRANDT ARMEMENTS
Original Assignee
BRANDT ARMEMENTS
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by BRANDT ARMEMENTS filed Critical BRANDT ARMEMENTS
Application granted granted Critical
Publication of DE3261284D1 publication Critical patent/DE3261284D1/de
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
    • F42B10/60—Steering arrangements
    • F42B10/66—Steering by varying intensity or direction of thrust
    • F42B10/663—Steering by varying intensity or direction of thrust using a plurality of transversally acting auxiliary nozzles, which are opened or closed by valves

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Fluid Mechanics (AREA)
  • Mechanical Engineering (AREA)
  • Combustion & Propulsion (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Furnace Charging Or Discharging (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Spray Control Apparatus (AREA)
  • Medicines That Contain Protein Lipid Enzymes And Other Medicines (AREA)
  • Platform Screen Doors And Railroad Systems (AREA)
  • Sampling And Sample Adjustment (AREA)
DE8282401089T 1981-06-30 1982-06-15 Guided missile directional control using gas jets Expired DE3261284D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8112835A FR2508414B1 (fr) 1981-06-30 1981-06-30 Dispositif de pilotage par jets de gaz pour engin guide

Publications (1)

Publication Number Publication Date
DE3261284D1 true DE3261284D1 (en) 1985-01-03

Family

ID=9260019

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8282401089T Expired DE3261284D1 (en) 1981-06-30 1982-06-15 Guided missile directional control using gas jets

Country Status (9)

Country Link
US (1) US4482107A (de)
EP (1) EP0068972B1 (de)
JP (1) JPS5831298A (de)
AT (1) ATE10396T1 (de)
CA (1) CA1206763A (de)
DE (1) DE3261284D1 (de)
EG (1) EG17912A (de)
FR (1) FR2508414B1 (de)
IL (1) IL66150A (de)

Families Citing this family (46)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2536720A1 (fr) * 1982-11-29 1984-06-01 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux et missile comportant un tel systeme
US4573648A (en) * 1983-01-20 1986-03-04 Ford Aerospace And Communications Corp. Ram air combustion steering system for a guided missile
DE3317583C2 (de) * 1983-05-13 1986-01-23 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung mit einer von einer Treibmittelquelle versorgten Düsenanordnung
DE3332415A1 (de) * 1983-09-08 1985-03-28 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Steuerbares stroemungsumlenksystem
DE3340037A1 (de) * 1983-11-05 1985-05-23 Diehl GmbH & Co, 8500 Nürnberg Stellsystem fuer gelenkte, mit ueberschallgeschwindigkeit fliegende flugkoerper
JPS60136657A (ja) * 1983-12-24 1985-07-20 Toyota Motor Corp ベルト式無段変速機用油圧装置
GB2156290B (en) * 1984-03-27 1988-06-02 British Aerospace Rockets and rocket motors
DE3429798C1 (de) * 1984-08-13 1985-12-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur Korrektur der Flugbahn eines Geschosses
DE3518904C1 (de) * 1985-05-25 1986-06-26 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Reversiermotor
FR2588372B1 (fr) * 1985-10-08 1989-07-13 Thomson Brandt Armements Dispositif de pilotage pour projectile guide au moyen de tuyeres laterales
US4951901A (en) * 1985-11-22 1990-08-28 Ship Systems, Inc. Spin-stabilized projectile with pulse receiver and method of use
US4685639A (en) * 1985-12-23 1987-08-11 Ford Aerospace & Communications Corp. Pneumatically actuated ram air steering system for a guided missile
GB8604912D0 (en) * 1986-02-27 2007-04-04 Short Brothers Plc Flight control of missiles
GB8618510D0 (en) * 1986-07-29 1986-12-17 Imi Kynuch Ltd Guidance apparatus for projectiles
FR2686687B1 (fr) * 1987-04-22 1994-05-13 Thomson Brandt Armements Procede et dispositif de pilotage d'un projectile selon ses trois axes de roulis tangage et lacet.
DE3801795C1 (de) * 1988-01-22 1989-08-17 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De
FR2634548B1 (de) * 1988-07-22 1993-09-03 Thomson Brandt Armements
DE4408085C2 (de) * 1994-03-10 1999-08-12 Rheinmetall W & M Gmbh Vorrichtung zur Lenkung eines nicht um seine Längsachse rotierenden Flugkörpers
US5711348A (en) * 1996-08-14 1998-01-27 Moog Inc. Hot gas control valve
US5816042A (en) * 1996-12-27 1998-10-06 United Technologies Corporation Flow diverter system for multiple streams for gas turbine engines
IL130681A (en) * 1997-01-02 2003-05-29 Tibor G Horwath Reticle for use in a guidance seeker for a spinning projectile
AUPQ776300A0 (en) * 2000-05-25 2000-08-10 Metal Storm Limited Missile control
US6752351B2 (en) * 2002-11-04 2004-06-22 The United States Of America As Represented By The Secretary Of The Navy Low mass flow reaction jet
JP2004306762A (ja) * 2003-04-07 2004-11-04 Mitsubishi Heavy Ind Ltd 三軸姿勢制御用推進装置及びその装置を備えた飛行物体
US7416154B2 (en) * 2005-09-16 2008-08-26 The United States Of America As Represented By The Secretary Of The Army Trajectory correction kit
US7856806B1 (en) * 2006-11-06 2010-12-28 Raytheon Company Propulsion system with canted multinozzle grid
US8084725B1 (en) * 2008-05-01 2011-12-27 Raytheon Company Methods and apparatus for fast action impulse thruster
US8338768B2 (en) 2008-10-15 2012-12-25 Honeywell International Inc. Actuation assembly
US20100275576A1 (en) * 2009-05-04 2010-11-04 Technion - Research & Development Foundation Ltd. System and method for maneuvering rockets
US8618455B2 (en) * 2009-06-05 2013-12-31 Safariland, Llc Adjustable range munition
US8362408B2 (en) * 2009-10-22 2013-01-29 Honeywell International Inc. Steerable projectile charging system
US20110204177A1 (en) * 2010-02-25 2011-08-25 Pacific Scientific Energetic Materials Company Projectile diverter release and method of diverting a projectile
FR2967766B1 (fr) * 2010-11-24 2012-12-28 Mbda France Systeme pour piloter autour de ses axes de rotation un mobile mu par reaction, en particulier un missile
US8735788B2 (en) * 2011-02-18 2014-05-27 Raytheon Company Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
US9501055B2 (en) 2012-03-02 2016-11-22 Orbital Atk, Inc. Methods and apparatuses for engagement management of aerial threats
US11313650B2 (en) 2012-03-02 2022-04-26 Northrop Grumman Systems Corporation Methods and apparatuses for aerial interception of aerial threats
US11947349B2 (en) 2012-03-02 2024-04-02 Northrop Grumman Systems Corporation Methods and apparatuses for engagement management of aerial threats
US9170070B2 (en) 2012-03-02 2015-10-27 Orbital Atk, Inc. Methods and apparatuses for active protection from aerial threats
US9551552B2 (en) 2012-03-02 2017-01-24 Orbital Atk, Inc. Methods and apparatuses for aerial interception of aerial threats
US9068808B2 (en) * 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
US9115964B2 (en) * 2013-12-27 2015-08-25 Raytheon Company Integral injection thrust vector control with booster attitude control system
US9377279B2 (en) * 2014-04-22 2016-06-28 Raytheon Company Rocket cluster divert and attitude control system
US10662898B2 (en) 2016-09-08 2020-05-26 Raytheon Company Integrated thruster
US10615547B2 (en) 2016-09-08 2020-04-07 Raytheon Company Electrical device with shunt, and receptacle
US10578413B1 (en) * 2017-06-23 2020-03-03 Douglas Burke Bullet projectile with internal electro-mechanical action producing combustion for warfare
JP6738370B2 (ja) * 2018-05-10 2020-08-12 株式会社Ｓｕｂａｒｕ 航空機

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB865785A (en) * 1958-05-24 1961-04-19 Schlepperwerk Nordhausen Veb Improvements in or relating to control devices for hydraulic equipment
US3110228A (en) * 1961-02-08 1963-11-12 Thompson Ramo Wooldridge Inc Oscillatory actuator system
FR1293654A (fr) * 1961-04-07 1962-05-18 Snecma Dispositif de distribution de fluide applicable notamment à la gouverne par jet desavions à décollage vertical
US3273825A (en) * 1961-10-30 1966-09-20 Emerson Electric Co Guidance systems
US3190584A (en) * 1962-08-02 1965-06-22 Snecma Fluid distribution device especially applicable to control by jet of v.t.o.l. aircraft
US3302890A (en) * 1964-07-10 1967-02-07 Atlantic Res Corp Rocket nozzle
US3304721A (en) * 1964-09-08 1967-02-21 George U Oppel Aircraft thrust vector control assembly
US4265405A (en) * 1978-10-09 1981-05-05 Tosio Takagi Sprinkler nozzle
US4384690A (en) * 1981-03-06 1983-05-24 The United States Of America As Represented By The Secretary Of The Navy Thrust vector control for large deflection angles

Also Published As

Publication number Publication date
EP0068972A1 (de) 1983-01-05
ATE10396T1 (de) 1984-12-15
US4482107A (en) 1984-11-13
JPS5831298A (ja) 1983-02-23
FR2508414B1 (fr) 1985-06-07
EP0068972B1 (de) 1984-11-21
CA1206763A (en) 1986-07-02
IL66150A (en) 1988-10-31
EG17912A (en) 1991-08-30
FR2508414A1 (fr) 1982-12-31

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Legal Events

Date Code Title Description
8339 Ceased/non-payment of the annual fee