JPH0652061B2 - 宇宙飛行のためのロケツトエンジン - Google Patents

宇宙飛行のためのロケツトエンジン

Info

Publication number
JPH0652061B2
JPH0652061B2 JP60162162A JP16216285A JPH0652061B2 JP H0652061 B2 JPH0652061 B2 JP H0652061B2 JP 60162162 A JP60162162 A JP 60162162A JP 16216285 A JP16216285 A JP 16216285A JP H0652061 B2 JPH0652061 B2 JP H0652061B2
Authority
JP
Japan
Prior art keywords
propulsion
nozzle
altitude
ground
propulsion nozzle
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
JP60162162A
Other languages
English (en)
Japanese (ja)
Other versions
JPS6138147A (ja
Inventor
ギユンテル・シユミツト
Original Assignee
メツセルシユミツト‐ベルコウ‐ブローム・ゲゼルシヤフト・ミト・ベシユレンクテル・ハフツング
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 メツセルシユミツト‐ベルコウ‐ブローム・ゲゼルシヤフト・ミト・ベシユレンクテル・ハフツング filed Critical メツセルシユミツト‐ベルコウ‐ブローム・ゲゼルシヤフト・ミト・ベシユレンクテル・ハフツング
Publication of JPS6138147A publication Critical patent/JPS6138147A/ja
Publication of JPH0652061B2 publication Critical patent/JPH0652061B2/ja
Anticipated expiration legal-status Critical
Expired - Fee Related 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)
JP60162162A 1984-07-24 1985-07-24 宇宙飛行のためのロケツトエンジン Expired - Fee Related JPH0652061B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE3427169.4 1984-07-24
DE19843427169 DE3427169C2 (de) 1984-07-24 1984-07-24 Raketentriebwerk für Raumflüge

Publications (2)

Publication Number Publication Date
JPS6138147A JPS6138147A (ja) 1986-02-24
JPH0652061B2 true JPH0652061B2 (ja) 1994-07-06

Family

ID=6241379

Family Applications (1)

Application Number Title Priority Date Filing Date
JP60162162A Expired - Fee Related JPH0652061B2 (ja) 1984-07-24 1985-07-24 宇宙飛行のためのロケツトエンジン

Country Status (4)

Country Link
JP (1) JPH0652061B2 (xx)
DE (1) DE3427169C2 (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
SE8503554L (sv) 1986-01-25
FR2568316A1 (fr) 1986-01-31
DE3427169A1 (de) 1986-01-30
JPS6138147A (ja) 1986-02-24
SE8503554D0 (sv) 1985-07-22
DE3427169C2 (de) 1987-04-30
SE452354B (sv) 1987-11-23
FR2568316B1 (fr) 1990-07-27

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Legal Events

Date Code Title Description
R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees