FR2545879B1 - Systeme de tuyeres de poussee - Google Patents

Systeme de tuyeres de poussee

Info

Publication number
FR2545879B1
FR2545879B1 FR8407229A FR8407229A FR2545879B1 FR 2545879 B1 FR2545879 B1 FR 2545879B1 FR 8407229 A FR8407229 A FR 8407229A FR 8407229 A FR8407229 A FR 8407229A FR 2545879 B1 FR2545879 B1 FR 2545879B1
Authority
FR
France
Prior art keywords
nozzle system
push nozzle
push
nozzle
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
FR8407229A
Other languages
English (en)
Other versions
FR2545879A1 (fr
Inventor
Walter Kranz
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2545879A1 publication Critical patent/FR2545879A1/fr
Application granted granted Critical
Publication of FR2545879B1 publication Critical patent/FR2545879B1/fr
Expired legal-status Critical Current

Links

Classifications

    • 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

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR8407229A 1983-05-13 1984-05-10 Systeme de tuyeres de poussee Expired FR2545879B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3317583A DE3317583C2 (de) 1983-05-13 1983-05-13 Vorrichtung mit einer von einer Treibmittelquelle versorgten Düsenanordnung

Publications (2)

Publication Number Publication Date
FR2545879A1 FR2545879A1 (fr) 1984-11-16
FR2545879B1 true FR2545879B1 (fr) 1989-01-20

Family

ID=6198975

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8407229A Expired FR2545879B1 (fr) 1983-05-13 1984-05-10 Systeme de tuyeres de poussee

Country Status (4)

Country Link
US (1) US4589594A (fr)
EP (1) EP0128337B1 (fr)
DE (1) DE3317583C2 (fr)
FR (1) FR2545879B1 (fr)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3332415A1 (de) * 1983-09-08 1985-03-28 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Steuerbares stroemungsumlenksystem
GB8417706D0 (en) * 1984-07-11 1994-01-26 British Aerospace Spin rate variation of spinning bodies
DE3429798C1 (de) * 1984-08-13 1985-12-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Vorrichtung zur Korrektur der Flugbahn eines Geschosses
DE3442975C2 (de) * 1984-11-24 1986-11-06 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Einrichtung zur Kurzzeitsteuerung eines Flugkörpers mit Hilfe von Querkraft-Schuberzeugern
DE3518904C1 (de) * 1985-05-25 1986-06-26 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Reversiermotor
DE3519892C2 (de) * 1985-06-04 1987-04-23 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Brems- und Freigabevorrichtung für einen Drehdüsenkörper zur Lenkung eines Flugkörpers
DE3537079C1 (en) * 1985-10-18 1987-02-19 Messerschmitt Boelkow Blohm Quick-acting fluid control valve esp. for supersonic aircraft - has piston actuated by gas to deflect retaining balls
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
DE3645077C2 (de) * 1986-02-27 1996-06-27 Daimler Benz Aerospace Ag Vorrichtung zum Steuern von Flugkörpern
GB8618510D0 (en) * 1986-07-29 1986-12-17 Imi Kynuch Ltd Guidance apparatus for projectiles
US5024395A (en) * 1987-01-27 1991-06-18 Messerschmitt Bolkow-Blohm Gmbh Stepping mechanism for rotary motions
DE3702240C1 (en) * 1987-01-27 1988-07-21 Messerschmitt Boelkow Blohm Actuating device for a rotating-nozzle arrangement for controlling missiles
DE3708312A1 (de) * 1987-03-14 1988-09-22 Messerschmitt Boelkow Blohm Vorrichtung zum steuern eines flugkoerpers
DE3742836C1 (de) * 1987-12-17 1989-07-13 Messerschmitt Boelkow Blohm Flugkoerper mit verstellbaren Steuerorganen
DE3818615C1 (en) * 1988-06-01 1989-12-14 Messerschmitt-Boelkow-Blohm Gmbh, 8012 Ottobrunn, De Device for controlling missiles
FR2634548B1 (fr) * 1988-07-22 1993-09-03 Thomson Brandt Armements
DE3838100A1 (de) * 1988-11-10 1990-05-17 Messerschmitt Boelkow Blohm Fluidverteiler
US5129604A (en) * 1989-07-17 1992-07-14 General Dynamics Corporation, Pomona Div. Lateral thrust assembly for missiles
DE4107054C2 (de) * 1991-03-06 1995-01-12 Rheinmetall Gmbh Flugbahnkorrektureinrichtung für Munition
DE4408085C2 (de) * 1994-03-10 1999-08-12 Rheinmetall W & M Gmbh Vorrichtung zur Lenkung eines nicht um seine Längsachse rotierenden Flugkörpers
US5631830A (en) 1995-02-03 1997-05-20 Loral Vought Systems Corporation Dual-control scheme for improved missle maneuverability
US5590850A (en) * 1995-06-05 1997-01-07 Hughes Missile Systems Company Blended missile autopilot
US6308911B1 (en) 1998-10-30 2001-10-30 Lockheed Martin Corp. Method and apparatus for rapidly turning a vehicle in a fluid medium
US6494140B1 (en) 1999-04-22 2002-12-17 Lockheed Martin Corporation Modular rocket boosted penetrating warhead
US8186145B2 (en) * 2008-02-26 2012-05-29 Aerojet-General Corporation Rocket nozzles for unconventional vehicles
US8362408B2 (en) * 2009-10-22 2013-01-29 Honeywell International Inc. Steerable projectile charging system
US9018572B2 (en) * 2012-11-06 2015-04-28 Raytheon Company Rocket propelled payload with divert control system within nose cone
RU2579294C1 (ru) * 2015-06-16 2016-04-10 Акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель с дефлектором на срезе сопла
RU2657400C1 (ru) * 2017-07-10 2018-06-13 Акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель с насадком из углерод-углеродного композиционного материала (уукм)
IL271483A (en) * 2019-12-16 2021-06-30 Shilat Optronics Ltd A guided weapon system with low accuracy at night
CN113654412B (zh) * 2021-09-13 2024-08-02 北京理工大学 一种电机驱动的脉冲推力姿控装置
US20240076034A1 (en) * 2022-09-02 2024-03-07 Raytheon Technologies Corporation Aerial vehicle fluid control system with multi-way flow regulator

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3125297A (en) * 1964-03-17 Rotary spray head
US4193567A (en) * 1962-07-17 1980-03-18 Novatronics, Inc. Guidance devices
US3749334A (en) * 1966-04-04 1973-07-31 Us Army Attitude compensating missile system
US3614027A (en) * 1969-07-08 1971-10-19 Us Army Pneumatic resolver for missile control
FR2386802A1 (fr) * 1977-04-08 1978-11-03 Thomson Brandt Dispositif de pilotage pour projectile du genre missile, et projectile equipe de ce dispositif
DE2809281C2 (de) * 1978-03-03 1984-01-05 Emile Jean Versailles Stauff Steuervorrichtung für ein Geschoß mit Eigendrehung
GB2094240B (en) * 1981-03-10 1984-08-01 Secr Defence Attitude control systems for rocket powered vehicles
FR2504252B1 (fr) * 1981-04-21 1987-03-06 Thomson Brandt Projectile guide
FR2504085A1 (fr) * 1981-04-21 1982-10-22 Thomson Brandt Dispositif de pilotage par jets de gaz et projectile comprenant un tel dispositif
FR2508414B1 (fr) * 1981-06-30 1985-06-07 Thomson Brandt Dispositif de pilotage par jets de gaz pour engin guide

Also Published As

Publication number Publication date
US4589594A (en) 1986-05-20
EP0128337A2 (fr) 1984-12-19
DE3317583A1 (de) 1984-11-29
EP0128337B1 (fr) 1988-01-07
FR2545879A1 (fr) 1984-11-16
DE3317583C2 (de) 1986-01-23
EP0128337A3 (en) 1985-09-18

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