KR101968702B1 - 겔형 연료로 작동하는 미사일 및 킬 차량 제어용 장치 및 시스템 - Google Patents

겔형 연료로 작동하는 미사일 및 킬 차량 제어용 장치 및 시스템 Download PDF

Info

Publication number
KR101968702B1
KR101968702B1 KR1020170016424A KR20170016424A KR101968702B1 KR 101968702 B1 KR101968702 B1 KR 101968702B1 KR 1020170016424 A KR1020170016424 A KR 1020170016424A KR 20170016424 A KR20170016424 A KR 20170016424A KR 101968702 B1 KR101968702 B1 KR 101968702B1
Authority
KR
South Korea
Prior art keywords
fuel
gel
gas
combustion chamber
control
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 - Fee Related
Application number
KR1020170016424A
Other languages
English (en)
Korean (ko)
Other versions
KR20170093751A (ko
Inventor
위르겐 람젤
칼다스-핀토 페드로 독터
나우만 칼 빌란트 독터
헬무트 니더마이어
토비아스 메이어
투만 알버트 독터
리세 주잔네 독터
Original Assignee
바이에른-체미 게젤샤프트 퓌르 플루크체미슈 안트리베 엠베하
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 바이에른-체미 게젤샤프트 퓌르 플루크체미슈 안트리베 엠베하 filed Critical 바이에른-체미 게젤샤프트 퓌르 플루크체미슈 안트리베 엠베하
Publication of KR20170093751A publication Critical patent/KR20170093751A/ko
Application granted granted Critical
Publication of KR101968702B1 publication Critical patent/KR101968702B1/ko
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/10—Simultaneous control of position or course in three dimensions
    • G05D1/107—Simultaneous control of position or course in three dimensions specially adapted for missiles

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)
KR1020170016424A 2016-02-05 2017-02-06 겔형 연료로 작동하는 미사일 및 킬 차량 제어용 장치 및 시스템 Expired - Fee Related KR101968702B1 (ko)

Applications Claiming Priority (2)

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

Publications (2)

Publication Number Publication Date
KR20170093751A KR20170093751A (ko) 2017-08-16
KR101968702B1 true KR101968702B1 (ko) 2019-04-12

Family

ID=58462209

Family Applications (1)

Application Number Title Priority Date Filing Date
KR1020170016424A Expired - Fee Related KR101968702B1 (ko) 2016-02-05 2017-02-06 겔형 연료로 작동하는 미사일 및 킬 차량 제어용 장치 및 시스템

Country Status (5)

Country Link
US (1) US11084605B2 (cg-RX-API-DMAC7.html)
KR (1) KR101968702B1 (cg-RX-API-DMAC7.html)
DE (2) DE202017006759U1 (cg-RX-API-DMAC7.html)
FR (1) FR3047557B1 (cg-RX-API-DMAC7.html)
GB (1) GB2549170B (cg-RX-API-DMAC7.html)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR102234721B1 (ko) * 2019-12-31 2021-04-02 (주)테너지 드론용 하이브리드 전원장치를 위한 엔진
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
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
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
CN114963889A (zh) * 2022-06-14 2022-08-30 西北工业大学 一种潜射式跨域跨介质导弹
CN115387934B (zh) * 2022-09-14 2024-05-28 北京中科宇航技术有限公司 一种固体火箭发动机及其喉部调节装置
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 (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3199764B2 (ja) * 1990-03-14 2001-08-20 アエロスパティアル・マトラ ガスジェットによるミサイル操向装置
JP4847588B2 (ja) * 2006-11-10 2011-12-28 アエロジェット ジェネラル コーポレイション 複合サイクルミサイルエンジンシステムを動作させるための方法

Family Cites Families (51)

* 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
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
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
US7654490B2 (en) 2003-10-14 2010-02-02 Lockheed Martin Corporation Precision attitude control system for gimbaled thruster
US7827781B2 (en) * 2005-12-05 2010-11-09 Bendel Timothy B Liquid propellant rocket engine with pintle injector and acoustic dampening
US7851732B2 (en) 2006-03-07 2010-12-14 Raytheon Company System and method for attitude control of a flight vehicle using pitch-over thrusters
US7721551B2 (en) * 2006-06-29 2010-05-25 United Technologies Corporation Fan variable area nozzle for a gas turbine engine fan nacelle
US7762078B2 (en) * 2006-09-13 2010-07-27 Aerojet-General Corporation Nozzle with temperature-responsive throat diameter
US7509796B2 (en) * 2006-09-13 2009-03-31 Aerojet-General Corporation Pintle-controlled propulsion system with external dynamic seal
FR2906868B1 (fr) * 2006-10-06 2011-11-18 Snecma Injecteur de carburant pour chambre de combustion de moteur a turbine a gaz
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
US8242422B2 (en) 2009-02-23 2012-08-14 Raytheon Company Modular divert and attitude control system
WO2012149462A2 (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 (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3199764B2 (ja) * 1990-03-14 2001-08-20 アエロスパティアル・マトラ ガスジェットによるミサイル操向装置
JP4847588B2 (ja) * 2006-11-10 2011-12-28 アエロジェット ジェネラル コーポレイション 複合サイクルミサイルエンジンシステムを動作させるための方法

Also Published As

Publication number Publication date
DE102017102160A1 (de) 2017-08-10
GB2549170A (en) 2017-10-11
FR3047557B1 (fr) 2019-10-11
DE202017006759U1 (de) 2018-04-24
FR3047557A1 (cg-RX-API-DMAC7.html) 2017-08-11
US20180050825A1 (en) 2018-02-22
US11084605B2 (en) 2021-08-10
GB2549170B (en) 2021-01-06
GB201701783D0 (en) 2017-03-22
KR20170093751A (ko) 2017-08-16

Similar Documents

Publication Publication Date Title
KR101968702B1 (ko) 겔형 연료로 작동하는 미사일 및 킬 차량 제어용 장치 및 시스템
RU2445491C2 (ru) Двигательная установка ракеты с нечувствительным снаряжением и с множественными режимами работы и способ ее действия
Li et al. Experimental study on multiple-pulse performance characteristics of ammonium perchlorate/aluminum powder rocket motor
US8528316B2 (en) Solid propellant gas control system and method
US20220381201A1 (en) Hybrid propulsion unit for space vehicle
US11359877B2 (en) Apparatus and method for accelerating an object via an external free jet
EP1960654B1 (en) Hybrid rocket system
US3555826A (en) Inverse hybrid rocket
US4817377A (en) Head end control and steering system: using a forward end maneuvering gas generator
US11655055B2 (en) System and method for aerodynamic drag reduction in airborne systems and vehicles
KR101666776B1 (ko) 물과 반응하여 수소가스를 생성하는 파우더를 사용하는 제트 추진체 및 그의 작동방법.
RU2608193C1 (ru) Устройство для изменения траектории астероида, ядра кометы и других космических объектов
Pinto et al. Green gelled propellant highly throtteable rocket motor and gas generator technology: status and application
RU2484283C2 (ru) Способ утилизации невыработанных остатков компонентов ракетного топлива в отработанных ступенях ракет-носителей
Naumann et al. Gelled green propellant rocket motor and gas generator technology at bayern-chemie-status and applications for space systems
KR20090073642A (ko) 과산화수소 가스발생기를 이용한 이원추진제 로켓이 결합된복합사이클 추진 시스템 및 그 운전방법
Caubet et al. Innovative arianegroup controllable solid propulsion technologies
Naumann et al. Green, Highly Throttleable and Safe Gelled Propellant Rocket Motors–Application Potentials for In-Space Propulsion
RU187155U1 (ru) Бессопловая газопаровая камера жидкостного ракетного двигателя
US20090260343A1 (en) Solid propellant management control system and method
RU2845286C2 (ru) Рулевой механизм универсальной многоступенчатой ракеты
RU10222U1 (ru) Прямоточный воздушно-реактивный двигатель с механической системой подачи псевдоожиженного порошкообразного горючего
Grosse et al. Development of a Hybrid Rocket Motor Using a Diaphragm for a Small Test Rocket
AU2006322650B2 (en) Hybrid rocket system
Musielak Solid Propellant Rocket Propulsion

Legal Events

Date Code Title Description
E13-X000 Pre-grant limitation requested

St.27 status event code: A-2-3-E10-E13-lim-X000

PA0109 Patent application

St.27 status event code: A-0-1-A10-A12-nap-PA0109

P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

PG1501 Laying open of application

St.27 status event code: A-1-1-Q10-Q12-nap-PG1501

A201 Request for examination
PA0201 Request for examination

St.27 status event code: A-1-2-D10-D11-exm-PA0201

E902 Notification of reason for refusal
PE0902 Notice of grounds for rejection

St.27 status event code: A-1-2-D10-D21-exm-PE0902

T11-X000 Administrative time limit extension requested

St.27 status event code: U-3-3-T10-T11-oth-X000

T11-X000 Administrative time limit extension requested

St.27 status event code: U-3-3-T10-T11-oth-X000

T11-X000 Administrative time limit extension requested

St.27 status event code: U-3-3-T10-T11-oth-X000

E13-X000 Pre-grant limitation requested

St.27 status event code: A-2-3-E10-E13-lim-X000

P11-X000 Amendment of application requested

St.27 status event code: A-2-2-P10-P11-nap-X000

P13-X000 Application amended

St.27 status event code: A-2-2-P10-P13-nap-X000

E701 Decision to grant or registration of patent right
PE0701 Decision of registration

St.27 status event code: A-1-2-D10-D22-exm-PE0701

GRNT Written decision to grant
PR0701 Registration of establishment

St.27 status event code: A-2-4-F10-F11-exm-PR0701

PR1002 Payment of registration fee

St.27 status event code: A-2-2-U10-U11-oth-PR1002

Fee payment year number: 1

PG1601 Publication of registration

St.27 status event code: A-4-4-Q10-Q13-nap-PG1601

PR1001 Payment of annual fee

St.27 status event code: A-4-4-U10-U11-oth-PR1001

Fee payment year number: 4

PR1001 Payment of annual fee

St.27 status event code: A-4-4-U10-U11-oth-PR1001

Fee payment year number: 5

P22-X000 Classification modified

St.27 status event code: A-4-4-P10-P22-nap-X000

PC1903 Unpaid annual fee

St.27 status event code: A-4-4-U10-U13-oth-PC1903

Not in force date: 20240409

Payment event data comment text: Termination Category : DEFAULT_OF_REGISTRATION_FEE

P22-X000 Classification modified

St.27 status event code: A-4-4-P10-P22-nap-X000

PC1903 Unpaid annual fee

St.27 status event code: N-4-6-H10-H13-oth-PC1903

Ip right cessation event data comment text: Termination Category : DEFAULT_OF_REGISTRATION_FEE

Not in force date: 20240409