IT1024554B - Dispositivo di guida di un proiettile sulla traiettoria desiderata - Google Patents

Dispositivo di guida di un proiettile sulla traiettoria desiderata

Info

Publication number
IT1024554B
IT1024554B IT69853/74A IT6985374A IT1024554B IT 1024554 B IT1024554 B IT 1024554B IT 69853/74 A IT69853/74 A IT 69853/74A IT 6985374 A IT6985374 A IT 6985374A IT 1024554 B IT1024554 B IT 1024554B
Authority
IT
Italy
Prior art keywords
bullet
guiding device
desired trajectory
trajectory
guiding
Prior art date
Application number
IT69853/74A
Other languages
English (en)
Inventor
Tubeuf Jean
Original Assignee
Europ Propulsion
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 Europ Propulsion filed Critical Europ Propulsion
Application granted granted Critical
Publication of IT1024554B publication Critical patent/IT1024554B/it

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/80Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/88Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
IT69853/74A 1973-09-21 1974-09-20 Dispositivo di guida di un proiettile sulla traiettoria desiderata IT1024554B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7334005A FR2244978B1 (it) 1973-09-21 1973-09-21

Publications (1)

Publication Number Publication Date
IT1024554B true IT1024554B (it) 1978-07-20

Family

ID=9125404

Family Applications (1)

Application Number Title Priority Date Filing Date
IT69853/74A IT1024554B (it) 1973-09-21 1974-09-20 Dispositivo di guida di un proiettile sulla traiettoria desiderata

Country Status (5)

Country Link
US (1) US3977629A (it)
JP (1) JPS5060000A (it)
DE (1) DE2444920C2 (it)
FR (1) FR2244978B1 (it)
IT (1) IT1024554B (it)

Families Citing this family (39)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2674621B1 (fr) * 1977-07-29 1994-08-26 Thomson Brandt Projectile guide .
DE2813032C1 (de) * 1978-03-25 1991-02-21 Messerschmitt Boelkow Blohm Gleitgeschoss
DE2846372C2 (de) * 1978-10-25 1985-11-21 Rheinmetall GmbH, 4000 Düsseldorf Geschoß mit radialgerichteten Steuerdüsen zur Endphasenlenkung
DE3231528C1 (de) * 1982-08-25 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Steuersystem fuer eine fluegellose Lenkmunition
US4537371A (en) * 1982-08-30 1985-08-27 Ltv Aerospace And Defense Company Small caliber guided projectile
US4522357A (en) * 1983-01-19 1985-06-11 Ford Aerospace & Communications Corp. Ram air steering system for a guided missile
JPS60501366A (ja) * 1983-01-20 1985-08-22 ローラル・エアロスペイス・コーポレイション 誘導ミサイルのためのラム空気燃焼式操舵装置
DE3442974C1 (de) * 1984-11-24 1986-03-13 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zum Stabilisieren und Vermindern der Pendelung eines mit UEberschallgeschwindigkeit fliegenden Flugkoerpers
US4685639A (en) * 1985-12-23 1987-08-11 Ford Aerospace & Communications Corp. Pneumatically actuated ram air steering system for a guided missile
DE3804930A1 (de) * 1988-02-17 1989-08-31 Deutsch Franz Forsch Inst Flugkoerper
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
JPH0524501U (ja) * 1991-09-11 1993-03-30 富士ロビン株式会社 掘削土砂袋詰め機
US5788178A (en) * 1995-06-08 1998-08-04 Barrett, Jr.; Rolin F. Guided bullet
AUPQ776300A0 (en) * 2000-05-25 2000-08-10 Metal Storm Limited Missile control
US6467722B1 (en) * 2002-01-31 2002-10-22 The United States Of America As Represented By The Secretary Of The Army Magnetostrictive missile guidance system
US7143983B2 (en) * 2002-08-28 2006-12-05 Lockheed Martin Corporation Passive jet spoiler for yaw control of an aircraft
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
IL167721A (en) * 2005-03-29 2008-06-05 Israel Aerospace Ind Ltd Steering system and method for guided flying apparatus
US7851732B2 (en) * 2006-03-07 2010-12-14 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US9052174B2 (en) * 2007-08-31 2015-06-09 Ra Brands, L.L.C. Tipped projectiles
US8084725B1 (en) * 2008-05-01 2011-12-27 Raytheon Company Methods and apparatus for fast action impulse thruster
US7781709B1 (en) 2008-05-05 2010-08-24 Sandia Corporation Small caliber guided projectile
US7823510B1 (en) 2008-05-14 2010-11-02 Pratt & Whitney Rocketdyne, Inc. Extended range projectile
US7891298B2 (en) * 2008-05-14 2011-02-22 Pratt & Whitney Rocketdyne, Inc. Guided projectile
US8319162B2 (en) 2008-12-08 2012-11-27 Raytheon Company Steerable spin-stabilized projectile and method
US8076623B2 (en) * 2009-03-17 2011-12-13 Raytheon Company Projectile control device
US9108711B2 (en) 2009-03-23 2015-08-18 Southern Methodist University Generation of a pulsed jet by jet vectoring through a nozzle with multiple outlets
US8618455B2 (en) * 2009-06-05 2013-12-31 Safariland, Llc Adjustable range munition
US8975565B2 (en) * 2012-07-17 2015-03-10 Raytheon Company Integrated propulsion and attitude control system from a common pressure vessel for an interceptor
IL226044B (en) 2013-04-29 2018-10-31 Israel Aerospace Ind Ltd Steering system and method
IL242320B (en) 2015-10-28 2022-02-01 Israel Aerospace Ind Ltd Projectile, and system and method for steering a projectile
US10315754B2 (en) 2016-06-10 2019-06-11 Coflow Jet, LLC Fluid systems that include a co-flow jet
US10106246B2 (en) 2016-06-10 2018-10-23 Coflow Jet, LLC Fluid systems that include a co-flow jet
US10615547B2 (en) 2016-09-08 2020-04-07 Raytheon Company Electrical device with shunt, and receptacle
US10662898B2 (en) 2016-09-08 2020-05-26 Raytheon Company Integrated thruster
US10683076B2 (en) 2017-10-31 2020-06-16 Coflow Jet, LLC Fluid systems that include a co-flow jet
US11293293B2 (en) 2018-01-22 2022-04-05 Coflow Jet, LLC Turbomachines that include a casing treatment
US11111025B2 (en) 2018-06-22 2021-09-07 Coflow Jet, LLC Fluid systems that prevent the formation of ice
WO2021016321A1 (en) 2019-07-23 2021-01-28 Gecheng Zha Fluid systems and methods that address flow separation

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3246863A (en) * 1962-10-25 1966-04-19 Honeywell Inc Control apparatus
US3208383A (en) * 1963-07-18 1965-09-28 Roland W Larson Ramjet vent
US3278140A (en) * 1964-02-13 1966-10-11 Kenneth C Evans Pure fluid amplifier and pure fluid amplifier attitude control system for missiles
US3325121A (en) * 1964-07-30 1967-06-13 Honeywell Inc Airborne vehicle with vortex valve controlled by linear accelerometer to compensate for variations in aerodynamic drag
US3502285A (en) * 1968-04-19 1970-03-24 Us Army Missile system with pure fluid guidance and control
US3726496A (en) * 1971-08-04 1973-04-10 Us Army Tridirectional actuator
US3740003A (en) * 1972-03-13 1973-06-19 Us Army Secondary injection/jet reaction control
FR2190661B3 (it) * 1972-06-26 1976-06-18 Cargo Airships Ltd

Also Published As

Publication number Publication date
DE2444920A1 (de) 1975-04-17
FR2244978A1 (it) 1975-04-18
US3977629A (en) 1976-08-31
JPS5060000A (it) 1975-05-23
DE2444920C2 (de) 1983-12-15
FR2244978B1 (it) 1976-10-01

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