SE452354B - Raketdrivanordning for rymdflyg - Google Patents
Raketdrivanordning for rymdflygInfo
- Publication number
- SE452354B SE452354B SE8503554A SE8503554A SE452354B SE 452354 B SE452354 B SE 452354B SE 8503554 A SE8503554 A SE 8503554A SE 8503554 A SE8503554 A SE 8503554A SE 452354 B SE452354 B SE 452354B
- Authority
- SE
- Sweden
- Prior art keywords
- nozzle
- altitude
- ground
- approximately
- flight
- Prior art date
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)
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 SE8503554D0 (sv) | 1985-07-22 |
SE8503554L SE8503554L (sv) | 1986-01-25 |
SE452354B true 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 (xx) |
DE (1) | DE3427169C2 (xx) |
FR (1) | FR2568316B1 (xx) |
SE (1) | SE452354B (xx) |
Families Citing this family (14)
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)
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 |
-
1984
- 1984-07-24 DE DE19843427169 patent/DE3427169C2/de not_active Expired
-
1985
- 1985-07-22 SE SE8503554A patent/SE452354B/sv not_active IP Right Cessation
- 1985-07-23 FR FR8511239A patent/FR2568316B1/fr not_active Expired - Lifetime
- 1985-07-24 JP JP60162162A patent/JPH0652061B2/ja not_active Expired - Fee Related
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 |
SE8503554D0 (sv) | 1985-07-22 |
DE3427169C2 (de) | 1987-04-30 |
FR2568316B1 (fr) | 1990-07-27 |
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Legal Events
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