DE102017102160A1 - Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird - Google Patents

Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird Download PDF

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Publication number
DE102017102160A1
DE102017102160A1 DE102017102160.4A DE102017102160A DE102017102160A1 DE 102017102160 A1 DE102017102160 A1 DE 102017102160A1 DE 102017102160 A DE102017102160 A DE 102017102160A DE 102017102160 A1 DE102017102160 A1 DE 102017102160A1
Authority
DE
Germany
Prior art keywords
fuel
combustion chamber
gas
control
thrust
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.)
Ceased
Application number
DE102017102160.4A
Other languages
German (de)
English (en)
Inventor
Jürgen Ramsel
Pedro Caldas-Pinto
Helmut Niedermaier
Tobias Meyer
Albert Thumann
Karl Wieland Naumann
Susanne Risse
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.)
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Original Assignee
Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
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 Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH filed Critical Bayern Chemie Gesellschaft fuer Flugchemische Antriebe mbH
Publication of DE102017102160A1 publication Critical patent/DE102017102160A1/de
Ceased legal-status Critical Current

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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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/401—Liquid propellant rocket engines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/402—Propellant tanks; Feeding propellants
    • B64G1/4021—Tank construction; Details thereof
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B23/00—Compositions characterised by non-explosive or non-thermic constituents
    • C06B23/001—Fillers, gelling and thickening agents (e.g. fibres), absorbents for nitroglycerine
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B31/00—Compositions containing an inorganic nitrogen-oxygen salt
    • C06B31/28—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate
    • C06B31/32—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate with a nitrated organic compound
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06B—EXPLOSIVES OR THERMIC COMPOSITIONS; MANUFACTURE THEREOF; USE OF SINGLE SUBSTANCES AS EXPLOSIVES
    • C06B31/00—Compositions containing an inorganic nitrogen-oxygen salt
    • C06B31/28—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate
    • C06B31/32—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate with a nitrated organic compound
    • C06B31/38—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate with a nitrated organic compound the nitrated compound being an aromatic
    • C06B31/40—Compositions containing an inorganic nitrogen-oxygen salt the salt being ammonium nitrate with a nitrated organic compound the nitrated compound being an aromatic with an organic non-explosive or an organic non-thermic component
    • C—CHEMISTRY; METALLURGY
    • C06—EXPLOSIVES; MATCHES
    • C06D—MEANS FOR GENERATING SMOKE OR MIST; GAS-ATTACK COMPOSITIONS; GENERATION OF GAS FOR BLASTING OR PROPULSION (CHEMICAL PART)
    • C06D5/00—Generation of pressure gas, e.g. for blasting cartridges, starting cartridges, rockets
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/425—Propellants
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/52—Injectors
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/68—Decomposition chambers
    • 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
    • F02K9/70—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using semi- solid or pulverulent propellants
    • 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
    • F02K9/72—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid and solid propellants, i.e. hybrid rocket-engine plants
    • 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
    • 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
    • F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section
    • 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
    • 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
    • F02K9/94—Re-ignitable or restartable rocket- engine plants; Intermittently operated rocket-engine plants
    • 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
    • F02K9/97—Rocket nozzles
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F41—WEAPONS
    • F41H—ARMOUR; ARMOURED TURRETS; ARMOURED OR ARMED VEHICLES; MEANS OF ATTACK OR DEFENCE, e.g. CAMOUFLAGE, IN GENERAL
    • F41H11/00—Defence installations; Defence devices
    • F41H11/02—Anti-aircraft or anti-guided missile or anti-torpedo defence installations or systems
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F42—AMMUNITION; BLASTING
    • F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
    • F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
    • F42B15/01—Arrangements thereon for guidance or control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • Plasma & Fusion (AREA)
  • Organic Chemistry (AREA)
  • Fluid Mechanics (AREA)
  • Inorganic Chemistry (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
DE102017102160.4A 2016-02-05 2017-02-03 Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird Ceased DE102017102160A1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102016102104 2016-02-05
DE102016102104.0 2016-02-05

Publications (1)

Publication Number Publication Date
DE102017102160A1 true DE102017102160A1 (de) 2017-08-10

Family

ID=58462209

Family Applications (2)

Application Number Title Priority Date Filing Date
DE102017102160.4A Ceased DE102017102160A1 (de) 2016-02-05 2017-02-03 Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird
DE202017006759.5U Expired - Lifetime DE202017006759U1 (de) 2016-02-05 2017-02-03 Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE202017006759.5U Expired - Lifetime DE202017006759U1 (de) 2016-02-05 2017-02-03 Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird

Country Status (5)

Country Link
US (1) US11084605B2 (enExample)
KR (1) KR101968702B1 (enExample)
DE (2) DE102017102160A1 (enExample)
FR (1) FR3047557B1 (enExample)
GB (1) GB2549170B (enExample)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102021124815A1 (de) 2021-09-26 2023-03-30 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verwendung eines Raketentreibstoffs, Antriebsvorrichtung mit einem Raketentreibstoff und Unterwassertransportgerät

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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CN111664024A (zh) * 2020-07-07 2020-09-15 西安空天引擎科技有限公司 一种过氧化氢煤油自增压动力系统
CN112078831B (zh) * 2020-09-17 2023-06-23 兰州空间技术物理研究所 一种基于流量计的μN推力器及使用方法
CN113091513B (zh) * 2021-03-03 2023-02-28 上海机电工程研究所 舰载导弹武器系统的实时动态标定方法、系统及介质
CN114778757B (zh) * 2022-04-01 2024-04-05 北京理工大学 一种“十字”型可视化振动实验发动机
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CN116291966B (zh) * 2023-03-09 2025-11-18 西北工业大学 一种粉末燃料喷注压降和速度无级调控的方法与装置
CN119555391B (zh) * 2024-10-18 2025-09-16 南京理工大学 一种凝胶推进剂雾化试验装置

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3941389A1 (de) 1989-12-15 1991-06-20 Messerschmitt Boelkow Blohm Verfahren zur selbstaendigen lenkung eines flugkoerpers
US5098041A (en) 1990-06-07 1992-03-24 Hughes Aircraft Company Attitude control system for momentum-biased spacecraft
WO2008048702A2 (en) 2006-03-07 2008-04-24 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US8113468B2 (en) 2003-10-14 2012-02-14 Lockheed Martin Corporation Precision attitude control system for gimbaled thruster
US8242422B2 (en) 2009-02-23 2012-08-14 Raytheon Company Modular divert and attitude control system

Family Cites Families (48)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2552497A (en) * 1945-08-13 1951-05-08 Franklin E Roach Variable throat rocket nozzle
US3908933A (en) * 1956-06-26 1975-09-30 Us Navy Guided missile
US3115009A (en) * 1959-06-17 1963-12-24 United Aircraft Corp Injector head for rockets
US3286469A (en) * 1961-07-07 1966-11-22 United Aircraft Corp Rocket nozzle cooling and thrust recovery device
US3137130A (en) * 1961-07-25 1964-06-16 United Aircraft Corp Variable thrust liquid propellant rocket injector
US3064903A (en) * 1961-09-12 1962-11-20 Gen Motors Corp Variable area fuel injector
US3230704A (en) * 1961-10-30 1966-01-25 Thiokol Chemical Corp Rocket engine
US3192714A (en) * 1961-10-31 1965-07-06 Frederick R Hickerson Variable thrust rocket engine incorporating thrust vector control
US3244199A (en) * 1962-06-25 1966-04-05 Kelsey Hayes Co Rocket nozzle with adjustable throat
US3242670A (en) * 1962-08-27 1966-03-29 United Aircraft Corp Segmented baffle injector design
US3308619A (en) * 1965-05-14 1967-03-14 Curtiss Wright Corp Incremental thrust control system
US3698642A (en) * 1966-11-04 1972-10-17 Thiokol Chemical Corp Thrust vector control system
US3527056A (en) * 1967-11-20 1970-09-08 Trw Inc Flow positioned injector
DE1941296B2 (de) * 1969-08-14 1971-09-30 Messerschmitt Bolkow Blohm GmbH, 8000 München Durch ein fluessiges medium regenerativ gekuehlte brenn kammer mit schubduese
US3732693A (en) * 1970-11-27 1973-05-15 Chin Chu Ju Controllable solid propulsion system
US3722219A (en) * 1971-04-26 1973-03-27 Us Navy Variable area injector for rocket engine
US3726088A (en) * 1971-08-20 1973-04-10 Us Navy On-demand variable flow closed loop gas generator system with a variable area injector
US3807657A (en) * 1972-01-31 1974-04-30 Rca Corp Dual thrust level monopropellant spacecraft propulsion system
US3814324A (en) * 1972-06-19 1974-06-04 Gen Electric Propulsion nozzle and actuator system employed therein
US3848806A (en) * 1973-04-30 1974-11-19 Rockwell International Corp Throttling venturi valve
DE2515845C3 (de) * 1975-04-11 1981-10-15 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Flüssigkeitsraketentriebwerk regelbaren Schubs
US3986687A (en) * 1975-06-30 1976-10-19 General Electric Company Aircraft propulsion system with flight maneuverable exhaust nozzle
US4090359A (en) * 1976-06-10 1978-05-23 Oscar Leonard Doellner Radiant energy power source for jet aircraft and missiles
DE3031689A1 (de) * 1980-08-22 1982-03-04 MTU Motoren- und Turbinen-Union München GmbH, 8000 München Keramische brennkammer
US4618931A (en) * 1984-03-21 1986-10-21 The United States Of America As Represented By The Secretary Of The Air Force Gas generator fuel flow throttle control system
US4836451A (en) * 1987-09-10 1989-06-06 United Technologies Corporation Yaw and pitch convergent-divergent thrust vectoring nozzle
FR2659734B1 (fr) * 1990-03-14 1992-07-03 Aerospatiale Systeme pour le pilotage d'un missile au moyen de jets gazeux lateraux.
US5133183A (en) * 1991-03-01 1992-07-28 The United States Of America As Represented By The Secretary Of The Army Gel/solid bipropellant propulsion system with energy management capability
US5394690A (en) * 1993-09-20 1995-03-07 The United States Of America As Represented By The Secretary Of The Army Constant pressure, variable thrust bipropellant engine
US5491973A (en) * 1994-10-17 1996-02-20 Aerojet General Corporation Self-actuating control for rocket motor nozzle
FR2730555B1 (fr) * 1995-02-15 1997-03-14 Snecma Ensemble d'injection de carburant pour chambre de combustion de turbines a gaz
DE19730674A1 (de) * 1997-07-17 1999-01-21 Deutsch Zentr Luft & Raumfahrt Brennkammer und Verfahren zur Herstellung einer Brennkammer
RU2158839C2 (ru) * 1999-01-21 2000-11-10 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Жидкостный ракетный двигатель с дожиганием турбогаза
RU2158840C2 (ru) * 1999-01-21 2000-11-10 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Корпус камеры жидкостного ракетного двигателя
JP2003294398A (ja) * 2002-04-03 2003-10-15 Mitsubishi Electric Corp サイドスラスタ
JP4218798B2 (ja) * 2003-04-28 2009-02-04 株式会社Ｉｈｉエアロスペース ガス分配装置
US7827781B2 (en) * 2005-12-05 2010-11-09 Bendel Timothy B Liquid propellant rocket engine with pintle injector and acoustic dampening
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
US7509796B2 (en) * 2006-09-13 2009-03-31 Aerojet-General Corporation Pintle-controlled propulsion system with external dynamic seal
US7762078B2 (en) * 2006-09-13 2010-07-27 Aerojet-General Corporation Nozzle with temperature-responsive throat diameter
FR2906868B1 (fr) * 2006-10-06 2011-11-18 Snecma Injecteur de carburant pour chambre de combustion de moteur a turbine a gaz
US8056319B2 (en) * 2006-11-10 2011-11-15 Aerojet—General Corporation Combined cycle missile engine system
GB0625016D0 (en) * 2006-12-15 2007-01-24 Rolls Royce Plc Fuel injector
US20090211228A1 (en) * 2007-03-12 2009-08-27 Honeywell International, Inc. High performance liquid fuel combustion gas generator
US20120272640A1 (en) * 2011-04-29 2012-11-01 Firestar Engineering, Llc Variable suction exhaust
GB201113421D0 (en) * 2011-08-04 2011-09-21 Rolls Royce Plc Fuel injector
FR2997179B1 (fr) * 2012-10-22 2015-01-16 Roxel France Dispositif combine de pilotage de trajectoire et de reduction de trainee.
US9644845B2 (en) * 2014-02-03 2017-05-09 General Electric Company System and method for reducing modal coupling of combustion dynamics

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3941389A1 (de) 1989-12-15 1991-06-20 Messerschmitt Boelkow Blohm Verfahren zur selbstaendigen lenkung eines flugkoerpers
US5098041A (en) 1990-06-07 1992-03-24 Hughes Aircraft Company Attitude control system for momentum-biased spacecraft
US8113468B2 (en) 2003-10-14 2012-02-14 Lockheed Martin Corporation Precision attitude control system for gimbaled thruster
WO2008048702A2 (en) 2006-03-07 2008-04-24 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US8242422B2 (en) 2009-02-23 2012-08-14 Raytheon Company Modular divert and attitude control system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102021124815A1 (de) 2021-09-26 2023-03-30 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verwendung eines Raketentreibstoffs, Antriebsvorrichtung mit einem Raketentreibstoff und Unterwassertransportgerät

Also Published As

Publication number Publication date
GB2549170B (en) 2021-01-06
FR3047557B1 (fr) 2019-10-11
KR101968702B1 (ko) 2019-04-12
GB201701783D0 (en) 2017-03-22
GB2549170A (en) 2017-10-11
FR3047557A1 (enExample) 2017-08-11
DE202017006759U1 (de) 2018-04-24
KR20170093751A (ko) 2017-08-16
US20180050825A1 (en) 2018-02-22
US11084605B2 (en) 2021-08-10

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