FR2489420B1 - Vanne de commande du dosage de l'alimentation d'un moteur-fusee reglable - Google Patents

Vanne de commande du dosage de l'alimentation d'un moteur-fusee reglable

Info

Publication number
FR2489420B1
FR2489420B1 FR8114352A FR8114352A FR2489420B1 FR 2489420 B1 FR2489420 B1 FR 2489420B1 FR 8114352 A FR8114352 A FR 8114352A FR 8114352 A FR8114352 A FR 8114352A FR 2489420 B1 FR2489420 B1 FR 2489420B1
Authority
FR
France
Prior art keywords
power supply
rocket motor
control valve
valve
valve control
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
Application number
FR8114352A
Other languages
English (en)
Other versions
FR2489420A1 (fr
Inventor
Hans Bohatsch
Manfred Biebricher
Willi Zumbroich
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 FR2489420A1 publication Critical patent/FR2489420A1/fr
Application granted granted Critical
Publication of FR2489420B1 publication Critical patent/FR2489420B1/fr
Expired 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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/56—Control
    • F02K9/58—Propellant feed valves

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Fuel-Injection Apparatus (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Containers And Packaging Bodies Having A Special Means To Remove Contents (AREA)
FR8114352A 1980-07-30 1981-07-23 Vanne de commande du dosage de l'alimentation d'un moteur-fusee reglable Expired FR2489420B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19803028824 DE3028824C2 (de) 1980-07-30 1980-07-30 Steuerventil zum Dosieren der Treibstoffmengen von regelbaren Raketentriebwerken

Publications (2)

Publication Number Publication Date
FR2489420A1 FR2489420A1 (fr) 1982-03-05
FR2489420B1 true FR2489420B1 (fr) 1988-02-05

Family

ID=6108431

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8114352A Expired FR2489420B1 (fr) 1980-07-30 1981-07-23 Vanne de commande du dosage de l'alimentation d'un moteur-fusee reglable

Country Status (3)

Country Link
DE (1) DE3028824C2 (fr)
FR (1) FR2489420B1 (fr)
GB (1) GB2081847B (fr)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2702008B1 (fr) * 1993-02-26 1995-05-24 Europ Propulsion Système d'injection mobile à obturation réactivable.
US5839272A (en) * 1994-12-21 1998-11-24 Moog Inc. Dual concentric poppet valves for maintaining substantially constant the ratio of two fluid flows over an operating range of valve opening
US5941062A (en) * 1995-05-11 1999-08-24 Societe Europeenne De Propulsion Pulse rocket engine
FR2734025B1 (fr) * 1995-05-11 1997-08-01 Europ Propulsion Moteur fusee a propergol liquide, a impulsions
US7762058B2 (en) * 2007-04-17 2010-07-27 Pratt & Whitney Rocketdyne, Inc. Ultra-compact, high performance aerovortical rocket thruster
US8904752B2 (en) * 2010-03-12 2014-12-09 Aerojet Rocketdyne Of De, Inc. Injector assembly for a rocket engine
CN109027329B (zh) * 2018-09-19 2023-09-29 北京航天动力研究所 低温发动机用多功能高压点火器阀门
CN113006969B (zh) * 2021-04-16 2021-11-23 西安航天动力研究所 一种用于深度变推力火箭发动机的气液喷注器
CN115419519B (zh) * 2022-11-03 2023-02-07 西安航天动力研究所 一种变推力针栓式喷注器

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1359447A (fr) * 1962-01-10 1964-04-24 North American Aviation Inc Dispositif à poussée variable et son injecteur
DE1228463B (de) * 1962-01-10 1966-11-10 North American Aviation Inc Zumessvorrichtung fuer Stroemungsmittel insbesondere bei einem Raketenmotor
US3232049A (en) * 1962-05-04 1966-02-01 Gen Motors Corp Fluid injection apparatus
US3790088A (en) * 1967-08-29 1974-02-05 Us Army Propellant splash plate having flow directing means
US3998051A (en) * 1975-01-02 1976-12-21 The United States Of America As Represented By The Secretary Of The Army Sustainer-injector slot-alignment

Also Published As

Publication number Publication date
GB2081847A (en) 1982-02-24
FR2489420A1 (fr) 1982-03-05
GB2081847B (en) 1984-01-25
DE3028824C2 (de) 1982-12-02
DE3028824A1 (de) 1982-08-19

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Legal Events

Date Code Title Description
ST Notification of lapse