FR2197118B1 - - Google Patents

Info

Publication number
FR2197118B1
FR2197118B1 FR7330512A FR7330512A FR2197118B1 FR 2197118 B1 FR2197118 B1 FR 2197118B1 FR 7330512 A FR7330512 A FR 7330512A FR 7330512 A FR7330512 A FR 7330512A FR 2197118 B1 FR2197118 B1 FR 2197118B1
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
FR7330512A
Other versions
FR2197118A1 (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 FR2197118A1 publication Critical patent/FR2197118A1/fr
Application granted granted Critical
Publication of FR2197118B1 publication Critical patent/FR2197118B1/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
    • 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
    • F02K9/68—Decomposition chambers
    • 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
    • F02K9/88—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using auxiliary rocket nozzles

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Organic Low-Molecular-Weight Compounds And Preparation Thereof (AREA)
  • Filling Or Discharging Of Gas Storage Vessels (AREA)
FR7330512A 1972-08-23 1973-08-22 Expired FR2197118B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19722241424 DE2241424C3 (de) 1972-08-23 1972-08-23 Verfahren zum Betreiben eines Flüssigkeitsraketentriebwerkes

Publications (2)

Publication Number Publication Date
FR2197118A1 FR2197118A1 (fr) 1974-03-22
FR2197118B1 true FR2197118B1 (fr) 1978-01-06

Family

ID=5854307

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7330512A Expired FR2197118B1 (fr) 1972-08-23 1973-08-22

Country Status (3)

Country Link
DE (1) DE2241424C3 (fr)
FR (1) FR2197118B1 (fr)
GB (1) GB1439368A (fr)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8609228D0 (en) * 1986-04-16 1986-05-21 Marconi Co Ltd Thrusters
GB8610849D0 (en) * 1986-05-02 1986-08-20 Marconi Co Ltd Gas thruster
EP0272284A1 (fr) * 1986-06-19 1988-06-29 Hughes Aircraft Company Systeme hybride de correction de position pour engin spatial
US5263666A (en) * 1988-12-16 1993-11-23 General Electric Co. Spacecraft with increased stationkeeping fuel load
US5282357A (en) * 1990-04-19 1994-02-01 Trw Inc. High-performance dual-mode integral propulsion system
US5417049A (en) * 1990-04-19 1995-05-23 Trw Inc. Satellite propulsion and power system
FR2697587B1 (fr) * 1992-11-04 1995-01-20 Europ Propulsion Système optimisé d'alimentation de moteur fusée réallumable.
US6135393A (en) * 1997-11-25 2000-10-24 Trw Inc. Spacecraft attitude and velocity control thruster system
US6393830B1 (en) 1999-03-26 2002-05-28 Alliant Techsystems Inc. Hybrid rocket propulsion system including array of hybrid or fluid attitude-control rocket engines
EP1172545B1 (fr) 2000-07-15 2013-05-29 Astrium GmbH Système d'allumage pour des chambres de combustion de moteurs-fusées
FR2828524B1 (fr) * 2001-08-07 2003-10-31 Air Liquide Systeme propulsif annexe d'etage cryotechnique de lanceur et etage de lanceur comprenant un tel systeme
DE102005005156B4 (de) * 2005-02-04 2007-06-06 Astrium Gmbh Triebwerk
CN107701330B (zh) * 2017-09-14 2019-08-09 北京控制工程研究所 一种不基于气体旁路的系统混合比主动控制方法

Also Published As

Publication number Publication date
GB1439368A (en) 1976-06-16
FR2197118A1 (fr) 1974-03-22
DE2241424C3 (de) 1978-06-22
DE2241424B2 (de) 1977-10-06
DE2241424A1 (de) 1974-03-07

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Legal Events

Date Code Title Description
ST Notification of lapse