DE3427169C2 - - Google Patents

Info

Publication number
DE3427169C2
DE3427169C2 DE19843427169 DE3427169A DE3427169C2 DE 3427169 C2 DE3427169 C2 DE 3427169C2 DE 19843427169 DE19843427169 DE 19843427169 DE 3427169 A DE3427169 A DE 3427169A DE 3427169 C2 DE3427169 C2 DE 3427169C2
Authority
DE
Germany
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
DE19843427169
Other languages
German (de)
Other versions
DE3427169A1 (de
Inventor
Guenther Dr. 8028 Taufkirchen De Schmidt
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
Priority to DE19843427169 priority Critical patent/DE3427169A1/de
Priority to SE8503554A priority patent/SE452354B/sv
Priority to FR8511239A priority patent/FR2568316B1/fr
Priority to JP60162162A priority patent/JPH0652061B2/ja
Publication of DE3427169A1 publication Critical patent/DE3427169A1/de
Application granted granted Critical
Publication of DE3427169C2 publication Critical patent/DE3427169C2/de
Granted 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
    • F02K9/97—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
    • F02K9/976—Deployable nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Testing Of Engines (AREA)
  • Toys (AREA)
DE19843427169 1984-07-24 1984-07-24 Raketentriebwerk fuer raumfluege Granted DE3427169A1 (de)

Priority Applications (4)

Application Number Priority Date Filing Date Title
DE19843427169 DE3427169A1 (de) 1984-07-24 1984-07-24 Raketentriebwerk fuer raumfluege
SE8503554A SE452354B (sv) 1984-07-24 1985-07-22 Raketdrivanordning for rymdflyg
FR8511239A FR2568316B1 (fr) 1984-07-24 1985-07-23 Propulseur-fusee pour vols spatiaux
JP60162162A JPH0652061B2 (ja) 1984-07-24 1985-07-24 宇宙飛行のためのロケツトエンジン

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19843427169 DE3427169A1 (de) 1984-07-24 1984-07-24 Raketentriebwerk fuer raumfluege

Publications (2)

Publication Number Publication Date
DE3427169A1 DE3427169A1 (de) 1986-01-30
DE3427169C2 true DE3427169C2 (xx) 1987-04-30

Family

ID=6241379

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19843427169 Granted DE3427169A1 (de) 1984-07-24 1984-07-24 Raketentriebwerk fuer raumfluege

Country Status (4)

Country Link
JP (1) JPH0652061B2 (xx)
DE (1) DE3427169A1 (xx)
FR (1) FR2568316B1 (xx)
SE (1) SE452354B (xx)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5052176A (en) * 1988-09-28 1991-10-01 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Combination turbojet-ramjet-rocket propulsion system
FR2637017B1 (fr) * 1988-09-28 1990-11-30 Snecma Structure de tuyere pour propulseur combine turbo-stato-fusee
FR2639404B1 (fr) * 1988-11-21 1994-04-15 Propulsion Ste Europeenne Divergent de moteur-fusee a tuyere annulaire complementaire
FR2656382B1 (fr) * 1989-12-21 1994-07-08 Europ Propulsion Moteur a propulsion combinee a haute adaptabilite pour aeronef ou avion spatial.
DE4222947C2 (de) * 1992-07-11 1995-02-02 Deutsche Aerospace Strahltriebwerk
FR2705738B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à diffuseur éjectable.
FR2705739B1 (fr) * 1993-05-28 1995-08-18 Europ Propulsion Tuyère de moteur-fusée à section de sortie sélectivement réduite.
FR2754566B1 (fr) 1996-10-11 1999-02-05 Europ Propulsion Tuyere de moteur-fusee a inserts ejectables
DE102005039742B4 (de) * 2005-08-23 2008-10-02 Technische Universität Dresden Schubdüse für Raketen mit ausfahrbarer Düsenverlängerung
FR2949821B1 (fr) * 2009-09-10 2011-09-30 Snecma Moteur fusee a divergent deployable
GB2519156A (en) * 2013-10-11 2015-04-15 Reaction Engines Ltd A nozzle arrangement for an engine
RU2595006C1 (ru) * 2015-09-02 2016-08-20 Акционерное общество "Конструкторское бюро химавтоматики" Жидкостный ракетный двигатель с выдвижным соплом
RU2705677C2 (ru) * 2016-11-21 2019-11-11 Федеральное государственное казенное военное образовательное учреждение высшего образования "Военный учебно-научный центр Военно-воздушных сил "Военно-воздушная академия имени профессора Н.Е. Жуковского и Ю.А. Гагарина" (г. Воронеж) Министерства обороны Российской Федерации Пиротехнический патрон для стимулирования осадков
RU2699867C1 (ru) * 2018-08-16 2019-09-11 Акционерное общество "НПО Энергомаш имени академика В.П. Глушко" Способ повышения энергетических характеристик серийно изготавливаемых жидкостных ракетных двигателей

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR763118A (fr) * 1933-09-25 1934-04-24 Machine thermique propulsive à réaction
FR980029A (fr) * 1942-06-18 1951-05-07 Regent Perfectionnements apportés aux dispositifs de propulsion
US3198459A (en) * 1961-06-30 1965-08-03 Geary Milford Imposion thrust engine and vehicle
US3229457A (en) * 1962-10-15 1966-01-18 James R Rowe Variable area ratio rocket nozzle
US3316716A (en) * 1964-07-01 1967-05-02 William J D Escher Composite powerplant and shroud therefor
US3469787A (en) * 1966-09-07 1969-09-30 Thiokol Chemical Corp Rocket motor thrust nozzle with means to direct atmospheric air into the interior of the nozzle
US3568443A (en) * 1969-08-14 1971-03-09 Robert S Estes Starting apparatus for a fluid-dynamic engine
US4220001A (en) * 1977-08-17 1980-09-02 Aerojet-General Corporation Dual expander rocket engine
US4387564A (en) * 1980-10-03 1983-06-14 Textron Inc. Extendible rocket engine exhaust nozzle assembly
JPS5932656A (ja) * 1982-08-18 1984-02-22 Natl Aerospace Lab ブ−スタエンジン用のノズル

Also Published As

Publication number Publication date
DE3427169A1 (de) 1986-01-30
FR2568316B1 (fr) 1990-07-27
SE8503554D0 (sv) 1985-07-22
SE452354B (sv) 1987-11-23
JPS6138147A (ja) 1986-02-24
FR2568316A1 (fr) 1986-01-31
SE8503554L (sv) 1986-01-25
JPH0652061B2 (ja) 1994-07-06

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Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 M

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLERCHRYSLER AEROSPACE AKTIENGESELLSCHAFT, 8099

8327 Change in the person/name/address of the patent owner

Owner name: DAIMLERCHRYSLER AEROSPACE AG, 85521 OTTOBRUNN, DE

8320 Willingness to grant licenses declared (paragraph 23)