FR947656A - Perfectionnements apportés aux chambres de combustion pour réacteurs du type fusée - Google Patents

Perfectionnements apportés aux chambres de combustion pour réacteurs du type fusée

Info

Publication number
FR947656A
FR947656A FR947656DA FR947656A FR 947656 A FR947656 A FR 947656A FR 947656D A FR947656D A FR 947656DA FR 947656 A FR947656 A FR 947656A
Authority
FR
France
Prior art keywords
rocket
combustion chambers
type reactors
reactors
type
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)
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.)
ILE D ETUDE de la PROPULSION P
Original Assignee
ILE D ETUDE de la PROPULSION P
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 ILE D ETUDE de la PROPULSION P filed Critical ILE D ETUDE de la PROPULSION P
Application granted granted Critical
Publication of FR947656A publication Critical patent/FR947656A/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
    • 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
    • F02K9/60—Constructional parts; Details not otherwise provided for
    • F02K9/62—Combustion or thrust chambers
    • F02K9/64—Combustion or thrust chambers having cooling arrangements

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
FR947656D 1947-05-20 1947-05-20 Perfectionnements apportés aux chambres de combustion pour réacteurs du type fusée Expired FR947656A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR947656T 1947-05-20

Publications (1)

Publication Number Publication Date
FR947656A true FR947656A (fr) 1949-07-08

Family

ID=9473568

Family Applications (1)

Application Number Title Priority Date Filing Date
FR947656D Expired FR947656A (fr) 1947-05-20 1947-05-20 Perfectionnements apportés aux chambres de combustion pour réacteurs du type fusée

Country Status (1)

Country Link
FR (1) FR947656A (fr)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1042971B (de) * 1954-01-02 1958-11-06 Carborundum Co Vorrichtung zur Leitung und gerichteten Freigabe von Gasen, insbesondere fuer Raketenantriebe
US3165888A (en) * 1959-09-18 1965-01-19 Edward F Keon Exhaust nozzle for reaction engines and the like
DE1200072B (de) * 1954-12-10 1965-09-02 Bristol Aerojet Ltd Duese fuer einen Raketenmotor und Vorrichtung zur Herstellung der Duese
DE1214476B (de) * 1956-12-21 1966-04-14 Haveg Industries Inc Hochtemperaturfestes Bau- bzw. Schutzschicht-material fuer Raketenbrennkammern oder Flugkoerperaussenhuellen

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1042971B (de) * 1954-01-02 1958-11-06 Carborundum Co Vorrichtung zur Leitung und gerichteten Freigabe von Gasen, insbesondere fuer Raketenantriebe
DE1200072B (de) * 1954-12-10 1965-09-02 Bristol Aerojet Ltd Duese fuer einen Raketenmotor und Vorrichtung zur Herstellung der Duese
DE1214476B (de) * 1956-12-21 1966-04-14 Haveg Industries Inc Hochtemperaturfestes Bau- bzw. Schutzschicht-material fuer Raketenbrennkammern oder Flugkoerperaussenhuellen
US3165888A (en) * 1959-09-18 1965-01-19 Edward F Keon Exhaust nozzle for reaction engines and the like

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