FR1112030A - Chambre de combustion, tuyère et plus particulièrement fusée - Google Patents

Chambre de combustion, tuyère et plus particulièrement fusée

Info

Publication number
FR1112030A
FR1112030A FR1112030DA FR1112030A FR 1112030 A FR1112030 A FR 1112030A FR 1112030D A FR1112030D A FR 1112030DA FR 1112030 A FR1112030 A FR 1112030A
Authority
FR
France
Prior art keywords
nozzle
combustion chamber
rocket
particularly rocket
combustion
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
English (en)
Inventor
Roger-Francis-Louis Fleury
Henri Garnier
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1112030A publication Critical patent/FR1112030A/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
    • F02K9/97—Rocket nozzles
    • F02K9/974—Nozzle- linings; Ablative coatings

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR1112030D 1954-06-03 1954-06-03 Chambre de combustion, tuyère et plus particulièrement fusée Expired FR1112030A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1112030T 1954-06-03

Publications (1)

Publication Number Publication Date
FR1112030A true FR1112030A (fr) 1956-03-07

Family

ID=9627043

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1112030D Expired FR1112030A (fr) 1954-06-03 1954-06-03 Chambre de combustion, tuyère et plus particulièrement fusée

Country Status (1)

Country Link
FR (1) FR1112030A (fr)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1062498B (de) * 1958-05-08 1959-07-30 Daimler Benz Ag Raketenbrennkammer mit Kuehlmantel
DE1086161B (de) * 1958-10-04 1960-07-28 V Max Ltd Strahlantriebseinrichtung, insbesondere fuer Modellflugzeuge und Spielzeuge
US3044257A (en) * 1958-06-02 1962-07-17 Thiokol Chemical Corp Combustion chamber outer jacket
US3073111A (en) * 1959-04-23 1963-01-15 United Aircraft Corp Rocket nozzle
US3131535A (en) * 1960-04-07 1964-05-05 Pneumo Dynamics Corp Rocket nozzle
US3188802A (en) * 1961-11-29 1965-06-15 Thiokol Chemical Corp Solid propellant grain
US3209533A (en) * 1961-04-21 1965-10-05 John S Light Rocket shell construction
US3224191A (en) * 1963-05-20 1965-12-21 Thiokol Chemical Corp Rocket motor construction
US3257803A (en) * 1961-05-08 1966-06-28 Sylvania Electric Prod Thermal boundary construction
US3285518A (en) * 1961-05-08 1966-11-15 Sylvania Electric Prod Substrate for thermal boundary construction and method of making the same
US3305178A (en) * 1963-04-12 1967-02-21 Arthur R Parilla Cooling techniques for high temperature engines and other components
US3597821A (en) * 1968-08-09 1971-08-10 Rohr Corp Method of making an integrated match machining rocket nozzle
US3700171A (en) * 1969-06-26 1972-10-24 Arthur R Parilla Cooling techniques for high temperature engines and other components
FR2506901A1 (fr) * 1981-05-26 1982-12-03 Messerschmitt Boelkow Blohm Couche d'ablation ainsi que procede et dispositif pour sa fabrication
FR2732409A1 (fr) * 1995-03-31 1996-10-04 Nissan Motor Dispositif pour controler la direction de la poussee d'un moteur-fusee

Cited By (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1062498B (de) * 1958-05-08 1959-07-30 Daimler Benz Ag Raketenbrennkammer mit Kuehlmantel
US3044257A (en) * 1958-06-02 1962-07-17 Thiokol Chemical Corp Combustion chamber outer jacket
DE1086161B (de) * 1958-10-04 1960-07-28 V Max Ltd Strahlantriebseinrichtung, insbesondere fuer Modellflugzeuge und Spielzeuge
US3073111A (en) * 1959-04-23 1963-01-15 United Aircraft Corp Rocket nozzle
US3131535A (en) * 1960-04-07 1964-05-05 Pneumo Dynamics Corp Rocket nozzle
US3209533A (en) * 1961-04-21 1965-10-05 John S Light Rocket shell construction
US3257803A (en) * 1961-05-08 1966-06-28 Sylvania Electric Prod Thermal boundary construction
US3285518A (en) * 1961-05-08 1966-11-15 Sylvania Electric Prod Substrate for thermal boundary construction and method of making the same
US3188802A (en) * 1961-11-29 1965-06-15 Thiokol Chemical Corp Solid propellant grain
US3305178A (en) * 1963-04-12 1967-02-21 Arthur R Parilla Cooling techniques for high temperature engines and other components
US3224191A (en) * 1963-05-20 1965-12-21 Thiokol Chemical Corp Rocket motor construction
US3597821A (en) * 1968-08-09 1971-08-10 Rohr Corp Method of making an integrated match machining rocket nozzle
US3700171A (en) * 1969-06-26 1972-10-24 Arthur R Parilla Cooling techniques for high temperature engines and other components
FR2506901A1 (fr) * 1981-05-26 1982-12-03 Messerschmitt Boelkow Blohm Couche d'ablation ainsi que procede et dispositif pour sa fabrication
FR2732409A1 (fr) * 1995-03-31 1996-10-04 Nissan Motor Dispositif pour controler la direction de la poussee d'un moteur-fusee
US5735463A (en) * 1995-03-31 1998-04-07 Nissan Motor Co., Ltd. Jetavator for rocket engine

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