EG18032A - Gas get steering device and missible comprising such a device - Google Patents

Gas get steering device and missible comprising such a device

Info

Publication number
EG18032A
EG18032A EG216/82A EG21682A EG18032A EG 18032 A EG18032 A EG 18032A EG 216/82 A EG216/82 A EG 216/82A EG 21682 A EG21682 A EG 21682A EG 18032 A EG18032 A EG 18032A
Authority
EG
Egypt
Prior art keywords
gas
missible
steering
steering device
rotary element
Prior art date
Application number
EG216/82A
Other languages
English (en)
Original Assignee
Thomson Brandt
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 Thomson Brandt filed Critical Thomson Brandt
Application granted granted Critical
Publication of EG18032A publication Critical patent/EG18032A/xx

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C15/00Attitude, flight direction, or altitude control by jet reaction
    • B64C15/14Attitude, flight direction, or altitude control by jet reaction the jets being other than main propulsion jets
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42AMMUNITION; BLASTING
    • F42BEXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B10/00Means 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
    • F42B10/60Steering arrangements
    • F42B10/66Steering by varying intensity or direction of thrust
    • F42B10/663Steering 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)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Chemical & Material Sciences (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Exhaust Gas After Treatment (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Air Bags (AREA)
  • Nozzles (AREA)
  • Percussion Or Vibration Massage (AREA)
  • Jet Pumps And Other Pumps (AREA)
EG216/82A 1981-04-21 1982-04-18 Gas get steering device and missible comprising such a device EG18032A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8107915A FR2504085A1 (fr) 1981-04-21 1981-04-21 Dispositif de pilotage par jets de gaz et projectile comprenant un tel dispositif

Publications (1)

Publication Number Publication Date
EG18032A true EG18032A (en) 1991-08-30

Family

ID=9257616

Family Applications (1)

Application Number Title Priority Date Filing Date
EG216/82A EG18032A (en) 1981-04-21 1982-04-18 Gas get steering device and missible comprising such a device

Country Status (9)

Country Link
US (1) US4463921A (xx)
EP (1) EP0063979B1 (xx)
JP (1) JPS57182598A (xx)
AT (1) ATE27691T1 (xx)
CA (1) CA1218344A (xx)
DE (1) DE3276528D1 (xx)
EG (1) EG18032A (xx)
FR (1) FR2504085A1 (xx)
IL (1) IL65530A (xx)

Families Citing this family (44)

* 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
DE3317583C2 (de) * 1983-05-13 1986-01-23 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung mit einer von einer Treibmittelquelle versorgten Düsenanordnung
GB8318729D0 (en) * 1983-07-11 1983-08-10 Secr Defence Fuselage sideforce control
DE3332415A1 (de) * 1983-09-08 1985-03-28 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Steuerbares stroemungsumlenksystem
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
DE3519892A1 (de) * 1985-06-04 1986-12-04 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Brems- und freigabeeinrichtung fuer einen drehduesenkoerper
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
DE3702240C1 (en) * 1987-01-27 1988-07-21 Messerschmitt Boelkow Blohm Actuating device for a rotating-nozzle arrangement for controlling missiles
US5024395A (en) * 1987-01-27 1991-06-18 Messerschmitt Bolkow-Blohm Gmbh Stepping mechanism for rotary motions
FR2620812B1 (fr) * 1987-09-18 1992-04-17 Thomson Brandt Armements Dispositif de commutation de jets de gaz lateraux destine au pilotage d'engins
FR2634548B1 (xx) * 1988-07-22 1993-09-03 Thomson Brandt Armements
US5070761A (en) * 1990-08-07 1991-12-10 The United States Of America As Represented By The Secretary Of The Navy Venting apparatus for controlling missile underwater trajectory
US5082209A (en) * 1991-03-01 1992-01-21 United Technologies Corporation Thrust reverser assembly
US5209432A (en) * 1992-07-02 1993-05-11 United Technologies Corporation Aircraft reverser port door
US5456429A (en) * 1993-08-02 1995-10-10 Loral Corp. Thrust maneuver system
US5505408A (en) * 1993-10-19 1996-04-09 Versatron Corporation Differential yoke-aerofin thrust vector control system
US6460801B1 (en) * 1993-11-18 2002-10-08 Lockheed Martin Corp. Precision guidance system for aircraft launched bombs
US5816042A (en) * 1996-12-27 1998-10-06 United Technologies Corporation Flow diverter system for multiple streams for gas turbine engines
DE19735279C1 (de) * 1997-08-14 1999-03-11 Bayern Chemie Gmbh Flugchemie Querschub-Steueranordnung für Flugkörper mit Feststoff-Heißgasgenerator
US6289669B1 (en) * 1999-02-25 2001-09-18 LKF Lenkflugkörpersysteme GmbH Lateral-thrust control arrangement for missiles with solid-fuel hot-gas generator
US6494140B1 (en) 1999-04-22 2002-12-17 Lockheed Martin Corporation Modular rocket boosted penetrating warhead
US6276277B1 (en) 1999-04-22 2001-08-21 Lockheed Martin Corporation Rocket-boosted guided hard target penetrator
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
US7851732B2 (en) * 2006-03-07 2010-12-14 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US8084725B1 (en) * 2008-05-01 2011-12-27 Raytheon Company Methods and apparatus for fast action impulse thruster
US8076623B2 (en) * 2009-03-17 2011-12-13 Raytheon Company Projectile control device
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
KR101362304B1 (ko) 2012-09-19 2014-02-13 엘아이지넥스원 주식회사 단계별 정밀 추진이 가능한 측 추력 장치
US9068808B2 (en) * 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
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
JP6738370B2 (ja) * 2018-05-10 2020-08-12 株式会社Subaru 航空機

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE568066C (de) * 1930-08-02 1933-01-13 Elek Sche App M B H Ges Steuerung fuer Raketen- und aehnliche Geschosse
US2726510A (en) * 1952-03-26 1955-12-13 Daniel And Florence Guggenhcim Flight-control apparatus involving steering combustion chambers
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
DE1232030B (de) * 1961-05-18 1967-01-05 Dornier Gmbh Steuerduesenkopf fuer die Strahlsteuerung von Luftfahrzeugen
US3273825A (en) * 1961-10-30 1966-09-20 Emerson Electric Co Guidance systems
US3245620A (en) * 1961-12-13 1966-04-12 Gen Motors Corp Missile steering control
US3302890A (en) * 1964-07-10 1967-02-07 Atlantic Res Corp Rocket nozzle
GB1073075A (en) * 1964-12-30 1967-06-21 Carter Day Company Distributor valve for controlling the distribution of a solids-gas mixture
US3927693A (en) * 1974-10-11 1975-12-23 Minnesota Mining & Mfg High-pressure valve
US4011720A (en) * 1975-05-13 1977-03-15 Thiokol Corporation Gas generator or rocket motor with selective discrete time vs. output profiles
FR2386802A1 (fr) * 1977-04-08 1978-11-03 Thomson Brandt Dispositif de pilotage pour projectile du genre missile, et projectile equipe de ce dispositif

Also Published As

Publication number Publication date
JPS57182598A (en) 1982-11-10
DE3276528D1 (en) 1987-07-16
EP0063979A1 (fr) 1982-11-03
IL65530A (en) 1986-08-31
FR2504085A1 (fr) 1982-10-22
ATE27691T1 (de) 1987-06-15
EP0063979B1 (fr) 1987-06-10
FR2504085B1 (xx) 1984-05-18
CA1218344A (en) 1987-02-24
US4463921A (en) 1984-08-07

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