DE60111317D1 - Raketen-Schubdüse mit drehbaren Zylindern zur Schubregelung - Google Patents

Raketen-Schubdüse mit drehbaren Zylindern zur Schubregelung

Info

Publication number
DE60111317D1
DE60111317D1 DE60111317T DE60111317T DE60111317D1 DE 60111317 D1 DE60111317 D1 DE 60111317D1 DE 60111317 T DE60111317 T DE 60111317T DE 60111317 T DE60111317 T DE 60111317T DE 60111317 D1 DE60111317 D1 DE 60111317D1
Authority
DE
Germany
Prior art keywords
rotating cylinders
thrust control
rocket thruster
thruster
rocket
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
DE60111317T
Other languages
English (en)
Other versions
DE60111317T2 (de
Inventor
David K Mcgrath
Daniel C Dombrowski
Thomas J Kirschner
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
Application granted granted Critical
Publication of DE60111317D1 publication Critical patent/DE60111317D1/de
Publication of DE60111317T2 publication Critical patent/DE60111317T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • F02K9/80—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
    • 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
    • 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
DE60111317T 2000-08-30 2001-08-30 Raketendüsenvorrichtung zur Umsetzung einer Schubänderung durch Betätigung eines Schubsteuerzylinders Expired - Lifetime DE60111317T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US22876500P 2000-08-30 2000-08-30
US228765P 2000-08-30

Publications (2)

Publication Number Publication Date
DE60111317D1 true DE60111317D1 (de) 2005-07-14
DE60111317T2 DE60111317T2 (de) 2006-05-04

Family

ID=22858494

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60111317T Expired - Lifetime DE60111317T2 (de) 2000-08-30 2001-08-30 Raketendüsenvorrichtung zur Umsetzung einer Schubänderung durch Betätigung eines Schubsteuerzylinders

Country Status (3)

Country Link
US (1) US6651438B2 (de)
EP (1) EP1184560B1 (de)
DE (1) DE60111317T2 (de)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7849695B1 (en) 2001-09-17 2010-12-14 Alliant Techsystems Inc. Rocket thruster comprising load-balanced pintle valve
US7461503B2 (en) 2002-06-26 2008-12-09 Alliant Techsystems Inc. Low-cost, low-density, ablative rubber insulation for rocket motors
US6902809B1 (en) * 2004-06-29 2005-06-07 Honeywell International, Inc. Rhenium tantalum metal alloy
US7560888B2 (en) * 2005-09-08 2009-07-14 Honeywell International Inc. Electromechanical actuator including redundant, dissimilar position feedback
KR100742596B1 (ko) * 2006-02-21 2007-08-02 국방과학연구소 측 추력기 모듈
US7509796B2 (en) * 2006-09-13 2009-03-31 Aerojet-General Corporation Pintle-controlled propulsion system with external dynamic seal
US10598128B1 (en) 2014-09-05 2020-03-24 Valley Tech Systems, Inc. Attitude control system
US9927217B1 (en) 2014-09-05 2018-03-27 Valley Tech Systems, Inc. Attitude control system
US10081091B2 (en) * 2015-06-12 2018-09-25 Postech Academy-Industry Foundation Nozzle, device, and method for high-speed generation of uniform nanoparticles
EP3371446B1 (de) * 2015-11-06 2019-08-07 Aerojet Rocketdyne, Inc. Fragmentiertes düsensystem
CN107091169A (zh) * 2017-06-29 2017-08-25 湖北三江航天江河化工科技有限公司 一种火箭发动机
US11143143B1 (en) 2018-05-11 2021-10-12 Valley Tech Systems, Inc. Extinguishable divert system
US11578682B2 (en) * 2018-06-29 2023-02-14 California Institute Of Technology SmallSat hybrid propulsion system

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3130544A (en) * 1961-10-23 1964-04-28 Salvatore J Penza Variable thrust and direction nozzle
US3192709A (en) * 1962-10-17 1965-07-06 Hardy Sammie Lloyd Variable throat nozzle
US3691770A (en) 1966-12-02 1972-09-19 Us Navy Thrust control means for a solid propellant rocket motor
US3806064A (en) 1968-10-03 1974-04-23 A Parilla Missile configurations, controls and utilization techniques
US3692258A (en) 1968-10-03 1972-09-19 Arthur R Parilla Missile configurations,controls and utilization techniques
US3948042A (en) 1968-12-23 1976-04-06 The United States Of America As Represented By The Secretary Of The Navy System for controlling the nozzle throat area of a rocket motor
US3989191A (en) 1971-09-13 1976-11-02 Thiokol Corporation Thrust control nozzle for rockets
US3907222A (en) 1973-09-14 1975-09-23 Hercules Inc Variable thrust rocket motor nozzle assembly, and rocket assembly containing same
US4444006A (en) 1981-02-04 1984-04-24 Hercules Incorporated Nozzle/valve device for a ducted rocket motor
US4442669A (en) 1981-02-12 1984-04-17 Hercules Incorporated Nozzle/valve device for a ducted rocket motor
US4452395A (en) * 1981-12-02 1984-06-05 Mcdonnell Douglas Corporation Nozzle assembly for a reaction engine
US4579299A (en) 1982-04-22 1986-04-01 Morton Thiokol, Inc. Quick turn, 90 degree omniaxial nozzle thrust control system
DE8409528U1 (de) * 1984-03-28 1985-06-27 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Ventileinrichtung zum Steuern strömender Medien, insbesondere zum Dosieren der Mengen der in die Brennkammer von Staustrahl-Raketentriebwerken einströmenden brennstoffreichen Gasen
US5092524A (en) 1990-02-12 1992-03-03 Mcdonnell Douglas Corporation Nozzle throat disc for thrust vectoring
US5294055A (en) 1992-09-08 1994-03-15 Mcdonnell Douglas Corporation Rotatable arms for thrust vectoring and changing the area of a nozzle throat
US5491973A (en) 1994-10-17 1996-02-20 Aerojet General Corporation Self-actuating control for rocket motor nozzle

Also Published As

Publication number Publication date
US20030046922A1 (en) 2003-03-13
EP1184560B1 (de) 2005-06-08
EP1184560A3 (de) 2004-02-04
DE60111317T2 (de) 2006-05-04
EP1184560A2 (de) 2002-03-06
US6651438B2 (en) 2003-11-25

Similar Documents

Publication Publication Date Title
DE69817235D1 (de) Schubumkehrvorrichtung mit synchronisierten Klappenstellantrieben
DE60111317D1 (de) Raketen-Schubdüse mit drehbaren Zylindern zur Schubregelung
DE69818115D1 (de) Schubumkehrvorrichtung mit optimierter Anordnung des Gitterbetätigungsorgans
DE69509344T2 (de) Schubumkehrvorrichtung mit schwenkbaren, gebogenen Klappen
DE60042987D1 (de) Multifunktionelle kombinierte Trägerrakete mit Flüssigkeitsraketentriebwerkssystemen
IT1304796B1 (it) Impiego di macrolidi nel controllo di organismi nocivi.
DK0935553T3 (da) Dobbeltpropeller-drev til fartøjer
DE59808465D1 (de) Einspritzventil mit steuerventil
ZA200305263B (en) Rocket launcher system and method for controlling a rocket launcher system.
DE69606809D1 (de) Zweikreistriebwerk mit Schubumkehrklappen
NO20030004L (no) Halestabilisert rakett
DE59706370D1 (de) Lenkflugkörper mit Staustrahlantrieb
DE69724033D1 (de) Schubumkehrvorrichtung mit beweglichen Auskleidungen in den Klappen
DE69909855D1 (de) Flugzeugmotor-Steuerungssystem
AUPQ923000A0 (en) Engine speed control system
DE50009041D1 (de) Raketenschubkammer
DE69931385D1 (de) Hydraulisch betätigtes, elektronisch gesteuertes brennstoffeinspritzsystem
DE50103219D1 (de) Zweimotoren-schiffsantriebsanlage
DE69813229T2 (de) Hydraulische betätigungsvorrichtung mit metall-gegen-metall dichtungen
NO963387D0 (no) Missil med ikke-sylindrisk fremdriftsseksjon
ATE197142T1 (de) Gegossene sprengstoffzusammensetzung mit mikrohohlkugeln
DK1243504T3 (da) Fremdriftsystem til både
BR0005806B1 (pt) processo e disposição para o comando da unidade de propulsão.
BR9604766A (pt) Propulsor aperfeiçoado
NO973695L (no) Propell

Legal Events

Date Code Title Description
8364 No opposition during term of opposition