FR1036540A - Combustion chamber of a rocket motor with adjustable thrust and a rocket motor provided with such a combustion chamber - Google Patents

Combustion chamber of a rocket motor with adjustable thrust and a rocket motor provided with such a combustion chamber

Info

Publication number
FR1036540A
FR1036540A FR1036540DA FR1036540A FR 1036540 A FR1036540 A FR 1036540A FR 1036540D A FR1036540D A FR 1036540DA FR 1036540 A FR1036540 A FR 1036540A
Authority
FR
France
Prior art keywords
combustion chamber
rocket motor
adjustable thrust
motor provided
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
Other languages
French (fr)
Inventor
Hans Schneider
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.)
SOC ET PROPULSION PAR REACTION
Original Assignee
SOC ET PROPULSION PAR REACTION
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 SOC ET PROPULSION PAR REACTION filed Critical SOC ET PROPULSION PAR REACTION
Application granted granted Critical
Publication of FR1036540A publication Critical patent/FR1036540A/en
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
    • F02K9/80—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control
    • F02K9/86—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof characterised by thrust or thrust vector control using nozzle throats of adjustable cross- section

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1036540D 1951-05-07 1951-05-07 Combustion chamber of a rocket motor with adjustable thrust and a rocket motor provided with such a combustion chamber Expired FR1036540A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1036540T 1951-05-07

Publications (1)

Publication Number Publication Date
FR1036540A true FR1036540A (en) 1953-09-08

Family

ID=9586477

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1036540D Expired FR1036540A (en) 1951-05-07 1951-05-07 Combustion chamber of a rocket motor with adjustable thrust and a rocket motor provided with such a combustion chamber

Country Status (1)

Country Link
FR (1) FR1036540A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968919A (en) * 1957-03-25 1961-01-24 Hughes Aircraft Co Variable area nozzle
US3113429A (en) * 1961-02-14 1963-12-10 Cievite Corp Steering and speed control for jet propelled vehicles
US3554448A (en) * 1967-11-24 1971-01-12 Nord Aviat Soc Nationale De Co Method of piloting engines by lateral gaseous jets issuing from the main propulsive means and nozzle with a central obstructing device in particular in the application of said method
FR2933745A1 (en) * 2008-07-11 2010-01-15 Snecma LIQUID PROPERGOL ROCKER MOTOR WITH PROPULSIVE ROOM SHUTTER.

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2968919A (en) * 1957-03-25 1961-01-24 Hughes Aircraft Co Variable area nozzle
US3113429A (en) * 1961-02-14 1963-12-10 Cievite Corp Steering and speed control for jet propelled vehicles
US3554448A (en) * 1967-11-24 1971-01-12 Nord Aviat Soc Nationale De Co Method of piloting engines by lateral gaseous jets issuing from the main propulsive means and nozzle with a central obstructing device in particular in the application of said method
FR2933745A1 (en) * 2008-07-11 2010-01-15 Snecma LIQUID PROPERGOL ROCKER MOTOR WITH PROPULSIVE ROOM SHUTTER.
US8347602B2 (en) 2008-07-11 2013-01-08 Snecma Liquid propellant rocket engine with a propulsion chamber shutter

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