FR2113856B1 - - Google Patents

Info

Publication number
FR2113856B1
FR2113856B1 FR717139412A FR7139412A FR2113856B1 FR 2113856 B1 FR2113856 B1 FR 2113856B1 FR 717139412 A FR717139412 A FR 717139412A FR 7139412 A FR7139412 A FR 7139412A FR 2113856 B1 FR2113856 B1 FR 2113856B1
Authority
FR
France
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
FR717139412A
Other languages
French (fr)
Other versions
FR2113856A1 (OSRAM
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 FR2113856A1 publication Critical patent/FR2113856A1/fr
Application granted granted Critical
Publication of FR2113856B1 publication Critical patent/FR2113856B1/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
FR717139412A 1970-11-10 1971-11-03 Expired FR2113856B1 (OSRAM)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19702055088 DE2055088A1 (de) 1970-11-10 1970-11-10 Einrichtung zum Erzeugen von Steuermomenten bei raketengetriebenen Flugkörpern

Publications (2)

Publication Number Publication Date
FR2113856A1 FR2113856A1 (OSRAM) 1972-06-30
FR2113856B1 true FR2113856B1 (OSRAM) 1974-06-21

Family

ID=5787590

Family Applications (1)

Application Number Title Priority Date Filing Date
FR717139412A Expired FR2113856B1 (OSRAM) 1970-11-10 1971-11-03

Country Status (4)

Country Link
US (1) US3802190A (OSRAM)
DE (1) DE2055088A1 (OSRAM)
FR (1) FR2113856B1 (OSRAM)
GB (1) GB1359864A (OSRAM)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5411845B2 (OSRAM) * 1974-10-07 1979-05-18
US4091665A (en) * 1977-02-11 1978-05-30 Nasa Multi-purpose wind tunnel reaction control model block
US4202517A (en) * 1977-07-20 1980-05-13 The United States Of America As Represented By The Secretary Of The Navy Fluidic interface means
GB2251834B (en) * 1983-02-22 1992-12-16 George Alexander Tarrant Guided missiles
US4630790A (en) * 1984-11-19 1986-12-23 Ford Aerospace & Communications Corporation Velocity and attitude control for exoatmospheric projectile
US4711414A (en) * 1986-03-31 1987-12-08 The Boeing Company Projectile with integrated propulsion system
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.
US5028014A (en) * 1988-11-15 1991-07-02 Anderson Jr Carl W Radial bleed total thrust control apparatus and method for a rocket propelled missile
US5158246A (en) * 1988-11-15 1992-10-27 Anderson Jr Carl W Radial bleed total thrust control apparatus and method for a rocket propelled missile
US5129604A (en) * 1989-07-17 1992-07-14 General Dynamics Corporation, Pomona Div. Lateral thrust assembly for missiles
US5664742A (en) * 1989-07-31 1997-09-09 The United States Of America As Represented By The Secretary Of The Navy Plume avoidance maneuvers
FR2656382B1 (fr) * 1989-12-21 1994-07-08 Europ Propulsion Moteur a propulsion combinee a haute adaptabilite pour aeronef ou avion spatial.
DE4210113C1 (de) * 1992-03-27 1998-11-05 Athanassios Dr Ing Zacharias Verfahren zum Leiten eines Flugkörpers und Flugkörper
US5294079A (en) * 1992-04-01 1994-03-15 Trw Inc. Space transfer vehicle
RU2126904C1 (ru) * 1997-03-28 1999-02-27 Кехваянц Валерий Григорьевич Силовая установка летательного аппарата вертикального или укороченного взлета и посадки
AU2252800A (en) * 1998-08-11 2000-04-10 Nekton Technologies, Inc. Devices and methods for orienting and steering in three-dimensional space
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
US7416154B2 (en) * 2005-09-16 2008-08-26 The United States Of America As Represented By The Secretary Of The Army Trajectory correction kit
FR2924763B1 (fr) * 2007-12-06 2014-04-25 Snecma Systeme de tuyeres de moteur-fusee
US7989744B2 (en) * 2008-02-01 2011-08-02 Raytheon Company Methods and apparatus for transferring a fluid
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
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
US9501055B2 (en) 2012-03-02 2016-11-22 Orbital Atk, Inc. 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
US8975565B2 (en) * 2012-07-17 2015-03-10 Raytheon Company Integrated propulsion and attitude control system from a common pressure vessel for an interceptor
US9068808B2 (en) * 2013-01-17 2015-06-30 Raytheon Company Air vehicle with bilateral steering thrusters
GB2519155B (en) * 2013-10-11 2016-10-12 Reaction Engines Ltd Engine
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
US9927217B1 (en) * 2014-09-05 2018-03-27 Valley Tech Systems, Inc. Attitude control system
US11143143B1 (en) 2018-05-11 2021-10-12 Valley Tech Systems, Inc. Extinguishable divert system
CN112197655A (zh) * 2020-09-25 2021-01-08 中国航天空气动力技术研究院 一种旋转导弹的滚转控制方法及控制装置
CN114184093A (zh) * 2021-11-30 2022-03-15 北京天兵科技有限公司 一种液体火箭单推力rcs布局及姿态控制方法

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968454A (en) * 1951-10-29 1961-01-17 Martin Co Rocket control system
US3524319A (en) * 1955-05-03 1970-08-18 Bolkow Gmbh Rocket engine with cooling walls of combustion chamber with oxygensupplying liquid
US2974594A (en) * 1958-08-14 1961-03-14 Boehm Josef Space vehicle attitude control system
US3099960A (en) * 1960-08-19 1963-08-06 George J Bryan Method of thrust vector control
US3135291A (en) * 1961-06-14 1964-06-02 United Aircraft Corp Bistable fluid valve
US3168807A (en) * 1961-08-08 1965-02-09 United Aircraft Corp Nuclear rocket flow control
US3231223A (en) * 1962-11-16 1966-01-25 Thiokol Chemical Corp Flight attitude control system
US3330483A (en) * 1964-10-26 1967-07-11 United Aircraft Corp Bistable valve control

Also Published As

Publication number Publication date
US3802190A (en) 1974-04-09
DE2055088A1 (de) 1972-05-18
GB1359864A (en) 1974-07-10
FR2113856A1 (OSRAM) 1972-06-30

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