DE60005497D1 - Hybrid-raketenantrieb mit einer anordnung von zusatzraketenmotoren zur positionskontrolle - Google Patents

Hybrid-raketenantrieb mit einer anordnung von zusatzraketenmotoren zur positionskontrolle

Info

Publication number
DE60005497D1
DE60005497D1 DE60005497T DE60005497T DE60005497D1 DE 60005497 D1 DE60005497 D1 DE 60005497D1 DE 60005497 T DE60005497 T DE 60005497T DE 60005497 T DE60005497 T DE 60005497T DE 60005497 D1 DE60005497 D1 DE 60005497D1
Authority
DE
Germany
Prior art keywords
rocket
arrangement
position control
additional
drive
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 - Lifetime
Application number
DE60005497T
Other languages
English (en)
Other versions
DE60005497T2 (de
Inventor
E Hamke
M Rohrbaugh
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.)
Northrop Grumman Innovation Systems LLC
Original Assignee
Alliant Techsystems Inc
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 Alliant Techsystems Inc filed Critical Alliant Techsystems Inc
Publication of DE60005497D1 publication Critical patent/DE60005497D1/de
Application granted granted Critical
Publication of DE60005497T2 publication Critical patent/DE60005497T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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
    • F02K9/74—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant
    • F02K9/76—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof combined with another jet-propulsion plant with another rocket-engine plant; Multistage 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
    • F02K9/88—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
    • F02K9/97—Rocket nozzles
DE60005497T 1999-03-26 2000-03-22 Hybrid-raketenantrieb mit einer anordnung von zusatzraketenmotoren zur positionskontrolle Expired - Lifetime DE60005497T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US12637799P 1999-03-26 1999-03-26
US126377P 1999-03-26
PCT/US2000/007443 WO2000058619A1 (en) 1999-03-26 2000-03-22 Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines

Publications (2)

Publication Number Publication Date
DE60005497D1 true DE60005497D1 (de) 2003-10-30
DE60005497T2 DE60005497T2 (de) 2004-05-06

Family

ID=22424510

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60005497T Expired - Lifetime DE60005497T2 (de) 1999-03-26 2000-03-22 Hybrid-raketenantrieb mit einer anordnung von zusatzraketenmotoren zur positionskontrolle

Country Status (6)

Country Link
US (1) US6393830B1 (de)
EP (1) EP1173668B1 (de)
JP (1) JP4113333B2 (de)
AU (1) AU6046100A (de)
DE (1) DE60005497T2 (de)
WO (1) WO2000058619A1 (de)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2367197A1 (en) * 2001-01-10 2002-07-10 Cesaroni Technology Incorporated Liquid/solid fuel hybrid propellant system for a rocket
US6576072B2 (en) * 2001-02-27 2003-06-10 The United States Of Americas As Represented By The Secretary Of The Navy Insensitive high energy booster propellant
US6739121B2 (en) * 2002-01-22 2004-05-25 Environmental Areoscience Corp. Flame holder for a hybrid rocket motor
US20040103170A1 (en) * 2002-11-21 2004-05-27 Borzilleri James V. Extended domain name method, apparatus, and system
US7008111B2 (en) * 2002-12-16 2006-03-07 Aerojet-General Corporation Fluidics-balanced fluid bearing
US7281367B2 (en) * 2003-12-05 2007-10-16 Alliant Techsystems Inc. Steerable, intermittently operable rocket propulsion system
US7069717B2 (en) * 2004-04-15 2006-07-04 Spacedev, Inc. Hybrid propulsion system
CA2504993A1 (en) * 2004-04-28 2005-10-28 Anthony Joseph Cesaroni Injector system for rocket motors
DE102004045855B4 (de) * 2004-09-20 2006-06-29 Eads Space Transportation Gmbh Steuer- und/oder Antriebseinrichtung für einen Flugkörper
US7503165B2 (en) * 2004-09-29 2009-03-17 Spacedev, Inc. Hybrid propulsion system
US7404288B2 (en) * 2004-10-28 2008-07-29 Spacedev, Inc. High propulsion mass fraction hybrid propellant system
US7966809B2 (en) 2006-02-01 2011-06-28 Spacedev, Inc. Single-piece hybrid rocket motor
US7716912B2 (en) * 2006-03-02 2010-05-18 Alliant Techsystems Inc. Propulsion thrust control system and method
US7633917B2 (en) * 2006-03-10 2009-12-15 Cisco Technology, Inc. Mobile network device multi-link optimizations
US8539753B2 (en) * 2006-06-29 2013-09-24 Spacedev, Inc. Hybrid rocket motor with annular, concentric solid fuel elements
US7966805B2 (en) * 2007-05-15 2011-06-28 Raytheon Company Hydroxyl amine based staged combustion hybrid rocket motor
DE102007036881B3 (de) * 2007-08-04 2009-01-22 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Anzündvorrichtung für gelförmige Treibstoffe
US8336287B1 (en) * 2008-03-27 2012-12-25 University Of Central Florida Research Foundation, Inc. Solid propellant rocket motor having self-extinguishing propellant grain and systems therefrom
FR2929339B1 (fr) * 2008-03-27 2012-10-05 Snpe Materiaux Energetiques Procede et dispositifs de propulsion pyrotechnique avec modulation de poussee, engin spatial comprenant un tel dispositif
US8024918B2 (en) * 2008-04-29 2011-09-27 Honeywell International Inc. Rocket motor having a catalytic hydroxylammonium (HAN) decomposer and method for combusting the decomposed HAN-based propellant
US9677504B2 (en) 2010-05-11 2017-06-13 Orbital Atk, Inc. Rockets, methods of rocket control and methods of rocket evaluation utilizing pressure compensation
IT1403760B1 (it) * 2011-01-07 2013-10-31 Hypotheses Srl Camere di combustione con presenza di vorticatori e sistemi di iniezione injectorless per motori ibridi
US8735788B2 (en) * 2011-02-18 2014-05-27 Raytheon Company Propulsion and maneuvering system with axial thrusters and method for axial divert attitude and control
FR2975481B1 (fr) * 2011-05-19 2017-09-01 Snecma Propulsion Solide Systeme pour le pilotage en force et le controle d'attitude en vol d'un vehicule et engin comportant un tel systeme
US8975565B2 (en) * 2012-07-17 2015-03-10 Raytheon Company Integrated propulsion and attitude control system from a common pressure vessel for an interceptor
US10774789B2 (en) 2012-07-30 2020-09-15 Utah State University Methods and systems for restartable, hybrid-rockets
US11408376B2 (en) 2012-07-30 2022-08-09 Utah State University Thrust augmentation of an additively manufactured hybrid rocket system using secondary oxidizer injection
US10527004B2 (en) 2012-07-30 2020-01-07 Utah State University Restartable ignition devices, systems, and methods thereof
US11407531B2 (en) 2012-07-30 2022-08-09 Utah State University Space Dynamics Laboratory Miniaturized green end-burning hybrid propulsion system for CubeSats
JP6000091B2 (ja) 2012-11-27 2016-09-28 三菱重工業株式会社 軌道姿勢制御装置、軌道姿勢制御方法
JP2014105657A (ja) * 2012-11-28 2014-06-09 Mitsubishi Heavy Ind Ltd 軌道姿勢制御装置、軌道姿勢制御方法
JP6008713B2 (ja) 2012-11-28 2016-10-19 三菱重工業株式会社 軌道姿勢制御装置、軌道姿勢制御方法
RU2611707C1 (ru) * 2016-03-31 2017-02-28 Акционерное общество "Конструкторское бюро химавтоматики" Многокамерный жидкостный ракетный двигатель
RU2725345C1 (ru) * 2019-10-01 2020-07-02 Акционерное общество "Конструкторское бюро химавтоматики" Многокамерный жидкостный ракетный двигатель с дожиганием с управляемым вектором тяги
US20220042479A1 (en) * 2020-08-05 2022-02-10 Stephen A. Whitmore Hybrid Rocket Motor
RU2771474C1 (ru) * 2021-06-09 2022-05-04 Акционерное общество "Конструкторское бюро химавтоматики" Многокамерный жидкостный ракетный двигатель с управляемым вектором тяги

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2637161A (en) * 1949-11-10 1953-05-05 Us Army Process of ignition for rockets and the like
US3112611A (en) * 1958-07-21 1963-12-03 Gen Electric Rocket motor employing a plug type nozzle
US3102386A (en) * 1958-09-26 1963-09-03 Standard Oil Co Discharge pressure controlled gas generators
US3107485A (en) 1959-05-27 1963-10-22 Ohio Commw Eng Co Propulsion means and method for space vehicles employing a volatile alkene and metalcarbonyl
US3135088A (en) * 1961-03-02 1964-06-02 United Aircraft Corp Sequencing system
US3311130A (en) * 1963-10-25 1967-03-28 Marquardt Corp Thrust vectoring system and control valve therefor
US3557556A (en) 1968-05-20 1971-01-26 Us Air Force Thrust modulator for hybrid rockets
FR1595755A (de) 1968-11-25 1970-06-15
US3677011A (en) 1969-01-22 1972-07-18 Us Air Force Thrust control system for hybrid rocket motors
US3732693A (en) 1970-11-27 1973-05-15 Chin Chu Ju Controllable solid propulsion system
DE2241424C3 (de) 1972-08-23 1978-06-22 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Verfahren zum Betreiben eines Flüssigkeitsraketentriebwerkes
US4527389A (en) 1982-06-21 1985-07-09 Thiokol Corporation Highly soluble, non-hazardous hydroxylammonium salt solutions for use in hybrid rocket motors
GB8610849D0 (en) 1986-05-02 1986-08-20 Marconi Co Ltd Gas thruster
JP3136065B2 (ja) * 1994-12-28 2001-02-19 株式会社アイ・エイチ・アイ・エアロスペース ロケットエンジンおよびロケットエンジンの姿勢制御方法
DE69619913T2 (de) 1995-09-18 2002-10-24 Microcosm Inc Wirtschaftliche Trägerrakete

Also Published As

Publication number Publication date
AU6046100A (en) 2000-10-16
EP1173668A1 (de) 2002-01-23
DE60005497T2 (de) 2004-05-06
JP2003524096A (ja) 2003-08-12
JP4113333B2 (ja) 2008-07-09
US6393830B1 (en) 2002-05-28
EP1173668B1 (de) 2003-09-24
WO2000058619A1 (en) 2000-10-05

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