FR1276441A - Rocket engine using two liquid propellants - Google Patents

Rocket engine using two liquid propellants

Info

Publication number
FR1276441A
FR1276441A FR847470A FR847470A FR1276441A FR 1276441 A FR1276441 A FR 1276441A FR 847470 A FR847470 A FR 847470A FR 847470 A FR847470 A FR 847470A FR 1276441 A FR1276441 A FR 1276441A
Authority
FR
France
Prior art keywords
rocket engine
liquid propellants
propellants
liquid
rocket
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
FR847470A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Priority to FR847470A priority Critical patent/FR1276441A/en
Application granted granted Critical
Publication of FR1276441A publication Critical patent/FR1276441A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/44Feeding propellants
    • F02K9/56Control

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR847470A 1960-12-20 1960-12-20 Rocket engine using two liquid propellants Expired FR1276441A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR847470A FR1276441A (en) 1960-12-20 1960-12-20 Rocket engine using two liquid propellants

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR847470A FR1276441A (en) 1960-12-20 1960-12-20 Rocket engine using two liquid propellants

Publications (1)

Publication Number Publication Date
FR1276441A true FR1276441A (en) 1961-11-17

Family

ID=8745140

Family Applications (1)

Application Number Title Priority Date Filing Date
FR847470A Expired FR1276441A (en) 1960-12-20 1960-12-20 Rocket engine using two liquid propellants

Country Status (1)

Country Link
FR (1) FR1276441A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2965305A1 (en) * 2010-09-28 2012-03-30 Snecma PROPULSIVE SPATIAL LAUNCHER SYSTEM USING A METHOD OF CONTROLLING THE CONSUMPTION OF ERGOLS

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2965305A1 (en) * 2010-09-28 2012-03-30 Snecma PROPULSIVE SPATIAL LAUNCHER SYSTEM USING A METHOD OF CONTROLLING THE CONSUMPTION OF ERGOLS
WO2012045939A1 (en) * 2010-09-28 2012-04-12 Snecma Thruster for a space launcher, and method for controlling propellant consumption

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