FR2197117A1 - - Google Patents

Info

Publication number
FR2197117A1
FR2197117A1 FR7328704A FR7328704A FR2197117A1 FR 2197117 A1 FR2197117 A1 FR 2197117A1 FR 7328704 A FR7328704 A FR 7328704A FR 7328704 A FR7328704 A FR 7328704A FR 2197117 A1 FR2197117 A1 FR 2197117A1
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.)
Granted
Application number
FR7328704A
Other languages
French (fr)
Other versions
FR2197117B3 (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
Application filed by Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2197117A1 publication Critical patent/FR2197117A1/fr
Application granted granted Critical
Publication of FR2197117B3 publication Critical patent/FR2197117B3/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
    • F02K9/46—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
    • 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

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)
  • Testing Of Engines (AREA)
  • Cooling, Air Intake And Gas Exhaust, And Fuel Tank Arrangements In Propulsion Units (AREA)
FR7328704A 1972-08-23 1973-08-06 Expired FR2197117B3 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19722241383 DE2241383C3 (en) 1972-08-23 1972-08-23 Main flow type liquid rocket engine

Publications (2)

Publication Number Publication Date
FR2197117A1 true FR2197117A1 (en) 1974-03-22
FR2197117B3 FR2197117B3 (en) 1976-07-16

Family

ID=5854287

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7328704A Expired FR2197117B3 (en) 1972-08-23 1973-08-06

Country Status (4)

Country Link
JP (2) JPS49108414A (en)
DE (1) DE2241383C3 (en)
FR (1) FR2197117B3 (en)
GB (1) GB1439535A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2550277A1 (en) * 1983-08-04 1985-02-08 Messerschmitt Boelkow Blohm Operating liquid oxygen-hydrogen rocket
FR2728627A1 (en) * 1994-12-27 1996-06-28 Europ Propulsion TANK SELF-PRESSURIZATION
WO2015019000A1 (en) * 2013-08-06 2015-02-12 Snecma Device for pressurizing propellant reservoirs of a rocket engine

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3209251C2 (en) * 1982-03-13 1984-04-05 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Method for pushing liquid in a container in a weightless state towards outflow openings and device for carrying out the method
DE19958310C2 (en) * 1999-12-03 2002-01-17 Daimler Chrysler Ag Rocket engine for liquid fuels with a closed engine circuit
JP3870252B2 (en) * 2001-07-19 2007-01-17 独立行政法人 宇宙航空研究開発機構 Cavitation suppression pump system
JP5144365B2 (en) * 2008-05-13 2013-02-13 株式会社Ｉｈｉエアロスペース Propellant tank pressure control system
JP6227931B2 (en) * 2013-08-21 2017-11-08 株式会社Ｉｈｉエアロスペース Two-stage combustion type two-component thruster
IT201700087235A1 (en) * 2017-07-28 2019-01-28 Angelo Minotti Space propulsion system
CN112412660B (en) * 2020-12-03 2021-11-02 西安航天动力研究所 Space power system combining extrusion and electric pump auxiliary pressurization
CN114542315B (en) * 2022-01-18 2023-02-21 北京理工大学 Turbulent jet flow spontaneous combustion ignition engine
CN114941800B (en) * 2022-04-29 2024-05-17 北京航天试验技术研究所 Rocket combustible propellant filling platform and filling method

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3170295A (en) * 1963-04-09 1965-02-23 Hugh L Dryden Propellant tank pressurization system
DE977815C (en) * 1963-12-21 1970-12-03 Messerschmitt Boelkow Blohm Liquid rocket engine
GB1167948A (en) * 1967-06-03 1969-10-22 Rolls Royce Rocket Engine.
US3577735A (en) * 1969-11-05 1971-05-04 Bolkow Ges Mit Beschrankter Liquid fuel rocket engine construction

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2550277A1 (en) * 1983-08-04 1985-02-08 Messerschmitt Boelkow Blohm Operating liquid oxygen-hydrogen rocket
FR2728627A1 (en) * 1994-12-27 1996-06-28 Europ Propulsion TANK SELF-PRESSURIZATION
EP0719935A1 (en) * 1994-12-27 1996-07-03 Societe Europeenne De Propulsion Self pressurizing tank
US5697212A (en) * 1994-12-27 1997-12-16 Societe Europeenne De Propulsion Rocket propellant tank self-pressurization
WO2015019000A1 (en) * 2013-08-06 2015-02-12 Snecma Device for pressurizing propellant reservoirs of a rocket engine
FR3009587A1 (en) * 2013-08-06 2015-02-13 Snecma PRESSURIZATION DEVICE FOR ERGOL TANKS OF A ROTOR MOTOR
US10533523B2 (en) 2013-08-06 2020-01-14 Arianegroup Sas Device for pressurizing propellant tanks of a rocket engine

Also Published As

Publication number Publication date
JPS59557U (en) 1984-01-05
GB1439535A (en) 1976-06-16
FR2197117B3 (en) 1976-07-16
DE2241383C3 (en) 1978-07-27
DE2241383B2 (en) 1977-11-10
JPS49108414A (en) 1974-10-15
DE2241383A1 (en) 1974-02-28

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