FR2232685B1 - - Google Patents

Info

Publication number
FR2232685B1
FR2232685B1 FR7419403A FR7419403A FR2232685B1 FR 2232685 B1 FR2232685 B1 FR 2232685B1 FR 7419403 A FR7419403 A FR 7419403A FR 7419403 A FR7419403 A FR 7419403A FR 2232685 B1 FR2232685 B1 FR 2232685B1
Authority
FR
France
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
FR7419403A
Other languages
French (fr)
Other versions
FR2232685A1 (en
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
Priority claimed from DE19732329624 external-priority patent/DE2329624C3/de
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2232685A1 publication Critical patent/FR2232685A1/fr
Application granted granted Critical
Publication of FR2232685B1 publication Critical patent/FR2232685B1/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
    • F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44—Feeding propellants
    • F02K9/46—Feeding propellants using pumps
    • F02K9/48—Feeding propellants using pumps driven by a gas turbine fed by propellant combustion gases or fed by vaporized propellants or other gases

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)
FR7419403A 1973-06-09 1974-06-05 Fluid drive system for rockets - with pre-combustion chamber to raise oxydator-rich gas mixture, and based on main drive electrical system Granted FR2232685A1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19732329624 DE2329624C3 (de) 1973-06-09 Raketensystem, umfassend ein Flüssigkeitsraketentriebwerk der Hauptstrombauart und mehrere Steuerraketentriebwerke

Publications (2)

Publication Number Publication Date
FR2232685A1 FR2232685A1 (en) 1975-01-03
FR2232685B1 true FR2232685B1 (ja) 1979-04-20

Family

ID=5883635

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7419403A Granted FR2232685A1 (en) 1973-06-09 1974-06-05 Fluid drive system for rockets - with pre-combustion chamber to raise oxydator-rich gas mixture, and based on main drive electrical system

Country Status (3)

Country Link
JP (1) JPS5032308A (ja)
FR (1) FR2232685A1 (ja)
IN (1) IN141928B (ja)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4589253A (en) * 1984-04-16 1986-05-20 Rockwell International Corporation Pre-regenerated staged-combustion rocket engine
GB8609228D0 (en) * 1986-04-16 1986-05-21 Marconi Co Ltd Thrusters
RU2158839C2 (ru) * 1999-01-21 2000-11-10 Открытое акционерное общество "НПО Энергомаш им. акад. В.П. Глушко" Жидкостный ракетный двигатель с дожиганием турбогаза
FR2921979B1 (fr) * 2007-10-08 2014-06-13 Astrium Sas Dispositif et procede de motorisation de pompe pour moteur fusee par moteur a combustion interne
FR2998926B1 (fr) * 2012-11-30 2014-12-26 Snecma Ensemble propulsif pour fusee
WO2018017788A1 (en) * 2016-07-22 2018-01-25 Aerojet Rocketdyne, Inc. Boost turbo-pump with axially fed turbine
PL439009A1 (pl) * 2021-09-22 2023-03-27 Sieć Badawcza Łukasiewicz-Instytut Lotnictwa Komora spalania wstępnego do zasilania turbiny w silnikach rakietowych na ciekłe materiały pędne

Also Published As

Publication number Publication date
FR2232685A1 (en) 1975-01-03
DE2329624B2 (de) 1975-06-19
IN141928B (ja) 1977-05-07
DE2329624A1 (de) 1975-01-02
JPS5032308A (ja) 1975-03-29

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Legal Events

Date Code Title Description
ST Notification of lapse