FR2307138A1 - Moteur-fusee a propergol liquide - Google Patents

Moteur-fusee a propergol liquide

Info

Publication number
FR2307138A1
FR2307138A1 FR7610276A FR7610276A FR2307138A1 FR 2307138 A1 FR2307138 A1 FR 2307138A1 FR 7610276 A FR7610276 A FR 7610276A FR 7610276 A FR7610276 A FR 7610276A FR 2307138 A1 FR2307138 A1 FR 2307138A1
Authority
FR
France
Prior art keywords
propergol
liquid
rocket engine
rocket
engine
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.)
Granted
Application number
FR7610276A
Other languages
English (en)
Other versions
FR2307138B3 (fr
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
Publication of FR2307138A1 publication Critical patent/FR2307138A1/fr
Application granted granted Critical
Publication of FR2307138B3 publication Critical patent/FR2307138B3/fr
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
    • F02K9/80—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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)
  • Cylinder Crankcases Of Internal Combustion Engines (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Nozzles (AREA)
FR7610276A 1975-04-11 1976-04-08 Moteur-fusee a propergol liquide Granted FR2307138A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE2515845A DE2515845C3 (de) 1975-04-11 1975-04-11 Flüssigkeitsraketentriebwerk regelbaren Schubs

Publications (2)

Publication Number Publication Date
FR2307138A1 true FR2307138A1 (fr) 1976-11-05
FR2307138B3 FR2307138B3 (fr) 1979-01-05

Family

ID=5943606

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7610276A Granted FR2307138A1 (fr) 1975-04-11 1976-04-08 Moteur-fusee a propergol liquide

Country Status (3)

Country Link
US (1) US4109460A (fr)
DE (1) DE2515845C3 (fr)
FR (1) FR2307138A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6579085B1 (en) 2000-05-05 2003-06-17 The Boc Group, Inc. Burner and combustion method for the production of flame jet sheets in industrial furnaces
WO2002029233A1 (fr) * 2000-10-05 2002-04-11 Federal State Unitary Enterprise Chemical Automatic Design Bureau (Cadb) Chambre annulaire de moteur-fusee a propergol liquide
DE202017006759U1 (de) * 2016-02-05 2018-04-24 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Vorrichtung und System zur Steuerung von Flugkörpern und Kill-Vehicles, die mit gelförmigen Treibstoffen betrieben wird
US11220979B1 (en) * 2020-11-10 2022-01-11 Mountain Aerospace Research Solutions, Inc. Liquid-cooled air-breathing rocket engine
CN116252970B (zh) * 2022-09-07 2023-08-29 中国科学院空间应用工程与技术中心 用于微小卫星的变推力气体推力器、气体供应系统及方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2570629A (en) * 1945-10-05 1951-10-09 Anxionnaz Adjustable pipe for the intake of air and expansion of the driving gases in reactionjet propellers for projectiles and vehicles
US2637973A (en) * 1949-04-01 1953-05-12 Reaction Motors Inc Rocket engine having turbine located in nozzle for driving auxiliaries
DE1191178B (de) * 1959-06-11 1965-04-15 Bendix Corp Strahltriebwerk
US3377803A (en) * 1960-08-10 1968-04-16 Gen Motors Corp Jet engine cooling system
US3286469A (en) * 1961-07-07 1966-11-22 United Aircraft Corp Rocket nozzle cooling and thrust recovery device
US3871173A (en) * 1970-03-24 1975-03-18 Us Navy Constant chamber pressure throttling injector

Also Published As

Publication number Publication date
DE2515845B2 (de) 1981-02-19
DE2515845C3 (de) 1981-10-15
US4109460A (en) 1978-08-29
DE2515845A1 (de) 1976-10-21
FR2307138B3 (fr) 1979-01-05

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