FR2031047A6 - - Google Patents

Info

Publication number
FR2031047A6
FR2031047A6 FR6945657A FR6945657A FR2031047A6 FR 2031047 A6 FR2031047 A6 FR 2031047A6 FR 6945657 A FR6945657 A FR 6945657A FR 6945657 A FR6945657 A FR 6945657A FR 2031047 A6 FR2031047 A6 FR 2031047A6
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
FR6945657A
Other languages
French (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.)
MAN Turbo GmbH
Original Assignee
MAN Turbo GmbH
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 MAN Turbo GmbH filed Critical MAN Turbo GmbH
Application granted granted Critical
Publication of FR2031047A6 publication Critical patent/FR2031047A6/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
    • F02K9/44—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)
  • Supercharger (AREA)
FR6945657A 1969-10-07 1969-12-31 Expired FR2031047A6 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19691950407 DE1950407B2 (en) 1969-10-07 1969-10-07 FUEL SUPPLY SYSTEM FOR A ROCKET ENGINE

Publications (1)

Publication Number Publication Date
FR2031047A6 true FR2031047A6 (en) 1970-11-13

Family

ID=5747482

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6945657A Expired FR2031047A6 (en) 1969-10-07 1969-12-31

Country Status (3)

Country Link
DE (1) DE1950407B2 (en)
FR (1) FR2031047A6 (en)
GB (1) GB1320766A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2404744A1 (en) * 1977-09-30 1979-04-27 Messerschmitt Boelkow Blohm ROCKET MOTOR WITH LIQUID PROPERGOLS OF THE DRIFT FLOW TYPE, FOR OPERATION IN VACUUM
EP0252238A1 (en) * 1986-05-07 1988-01-13 Mitsubishi Jukogyo Kabushiki Kaisha Liquid fuel rocket engine
FR2981127A1 (en) * 2011-10-11 2013-04-12 Snecma REACTION PROPULSION DEVICE AND FEEDING METHOD

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4583362A (en) * 1983-12-12 1986-04-22 Rockwell International Corporation Expander-cycle, turbine-drive, regenerative rocket engine
CN103133183B (en) * 2013-02-06 2015-11-04 北京航天试验技术研究所 A kind of thrust chamber low temperature hydrogen secure processing device
CN113404621B (en) * 2021-06-19 2022-08-16 西北工业大学 Solid-liquid mixed engine and method for Mars ascending aircraft
CN113586286A (en) * 2021-07-08 2021-11-02 北京星途探索科技有限公司 Liquid oxygen methane propellant supply system
CN114030656B (en) * 2021-11-09 2022-08-05 西安交通大学 Novel variable-thrust nuclear heat propulsion system

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2404744A1 (en) * 1977-09-30 1979-04-27 Messerschmitt Boelkow Blohm ROCKET MOTOR WITH LIQUID PROPERGOLS OF THE DRIFT FLOW TYPE, FOR OPERATION IN VACUUM
EP0252238A1 (en) * 1986-05-07 1988-01-13 Mitsubishi Jukogyo Kabushiki Kaisha Liquid fuel rocket engine
FR2981127A1 (en) * 2011-10-11 2013-04-12 Snecma REACTION PROPULSION DEVICE AND FEEDING METHOD
WO2013054027A1 (en) 2011-10-11 2013-04-18 Snecma Jet propulsion device and fuel supply method
US9771897B2 (en) 2011-10-11 2017-09-26 Snecma Jet propulsion device and fuel supply method

Also Published As

Publication number Publication date
DE1950407B2 (en) 1972-03-30
GB1320766A (en) 1973-06-20
DE1950407A1 (en) 1971-04-22

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