SE8503554D0 - Raketdrivanordning for rymdflyg - Google Patents

Raketdrivanordning for rymdflyg

Info

Publication number
SE8503554D0
SE8503554D0 SE8503554A SE8503554A SE8503554D0 SE 8503554 D0 SE8503554 D0 SE 8503554D0 SE 8503554 A SE8503554 A SE 8503554A SE 8503554 A SE8503554 A SE 8503554A SE 8503554 D0 SE8503554 D0 SE 8503554D0
Authority
SE
Sweden
Prior art keywords
altitude
nozzle
thrust
approximately
thrust nozzle
Prior art date
Application number
SE8503554A
Other languages
English (en)
Other versions
SE8503554L (sv
SE452354B (sv
Inventor
G Schmidt
Original Assignee
Messerschmitt Boelkow Blohm
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 Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm
Publication of SE8503554D0 publication Critical patent/SE8503554D0/sv
Publication of SE8503554L publication Critical patent/SE8503554L/sv
Publication of SE452354B publication Critical patent/SE452354B/sv

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)
SE8503554A 1984-07-24 1985-07-22 Raketdrivanordning for rymdflyg SE452354B (sv)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
SE8503554D0 true SE8503554D0 (sv) 1985-07-22
SE8503554L SE8503554L (sv) 1986-01-25
SE452354B SE452354B (sv) 1987-11-23

Family

ID=6241379

Family Applications (1)

Application Number Title Priority Date Filing Date
SE8503554A SE452354B (sv) 1984-07-24 1985-07-22 Raketdrivanordning for rymdflyg

Country Status (4)

Country Link
JP (1) JPH0652061B2 (sv)
DE (1) DE3427169C2 (sv)
FR (1) FR2568316B1 (sv)
SE (1) SE452354B (sv)

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
JPH0652061B2 (ja) 1994-07-06
DE3427169A1 (de) 1986-01-30
JPS6138147A (ja) 1986-02-24
DE3427169C2 (de) 1987-04-30
SE452354B (sv) 1987-11-23
FR2568316B1 (fr) 1990-07-27

Similar Documents

Publication Publication Date Title
SE8503554L (sv) Raketdrivanordning for rymdflyg
US2943821A (en) Directional control means for a supersonic vehicle
US5214914A (en) Translating cowl inlet with retractable propellant injection struts
RU2265132C2 (ru) Реактивная двигательная установка
GB629276A (en) Improvements in or relating to jet propulsion engines
GB1418905A (en) Gas turbine engines
GB1386232A (en) Fluid propulsion systems
US2924174A (en) Combustible pre-spin turbine for spinner rockets
US3049876A (en) Annular rocket motor and nozzle configuration
GB926117A (en) Improvements relating to propulsion arrangements for aircraft
GB960106A (en) Jet propulsion engines with orientable jet nozzles
GB1009269A (en) Improvements in or relating to aircraft
GB868408A (en) Improvements in and relating to an improved nozzle and tailplane device for a self-propelling missile
US3316716A (en) Composite powerplant and shroud therefor
RU2142058C1 (ru) Пульсирующий двигатель детонационного горения типа порфед
US4050243A (en) Combination solid fuel ramjet injector/port cover
GB1151273A (en) Variable-Area Nozzle, especially for Jet Engines of Supersonic Aircraft
GB1092012A (en) Improvements in thrust reversers for jet propelled aircraft
GB900040A (en) Exhaust nozzle with thrust deflector
GB761235A (en) Improvements in or relating to air intakes for jet-propulsion power plants
GB1387160A (en) Exhaust nozzles for jet propulsion engines for supersonic aircraft or vehicles
US3067573A (en) Telescoping-spike supersonic inlet for aircraft engines
US3430445A (en) Combined rocket-ramjet aircraft
GB1211192A (en) Improvements in low drag exhaust nozzle and nacelle arrangement for turbofan engines
US5317866A (en) Free-flying tubular vehicle

Legal Events

Date Code Title Description
NAL Patent in force

Ref document number: 8503554-1

Format of ref document f/p: F

NUG Patent has lapsed