CH446814A - Combustion chamber for a rocket engine - Google Patents

Combustion chamber for a rocket engine

Info

Publication number
CH446814A
CH446814A CH111763A CH111763A CH446814A CH 446814 A CH446814 A CH 446814A CH 111763 A CH111763 A CH 111763A CH 111763 A CH111763 A CH 111763A CH 446814 A CH446814 A CH 446814A
Authority
CH
Switzerland
Prior art keywords
combustion chamber
rocket engine
rocket
engine
combustion
Prior art date
Application number
CH111763A
Other languages
German (de)
Inventor
Vincent Milewski John
Selig Katz Harry
Original Assignee
Thiokol Chemical 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 Thiokol Chemical Corp filed Critical Thiokol Chemical Corp
Publication of CH446814A publication Critical patent/CH446814A/en

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
    • F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
    • F02K9/32—Constructional parts; Details not otherwise provided for
    • F02K9/34—Casings; Combustion chambers; Liners thereof
    • F02K9/346—Liners, e.g. inhibitors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Reinforced Plastic Materials (AREA)
  • Manufacture Of Porous Articles, And Recovery And Treatment Of Waste Products (AREA)
CH111763A 1962-01-29 1963-01-29 Combustion chamber for a rocket engine CH446814A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US16931962A 1962-01-29 1962-01-29

Publications (1)

Publication Number Publication Date
CH446814A true CH446814A (en) 1967-11-15

Family

ID=22615160

Family Applications (1)

Application Number Title Priority Date Filing Date
CH111763A CH446814A (en) 1962-01-29 1963-01-29 Combustion chamber for a rocket engine

Country Status (3)

Country Link
CH (1) CH446814A (en)
DE (1) DE1235675B (en)
GB (1) GB984486A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2499977A1 (en) * 1981-02-18 1982-08-20 Messerschmitt Boelkow Blohm INSULATING LAYER FOR PROPULSIVE LOADS

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3536656A (en) * 1966-02-21 1970-10-27 Gen Tire & Rubber Co Light-weight flexible insulating material
US5802842A (en) * 1996-07-29 1998-09-08 Trw Inc. Dimensionally stable throat insert for rocket thrusters
DE10245741B4 (en) * 2002-10-01 2005-10-06 Bayern-Chemie Gesellschaft Für Flugchemische Antriebe Mbh Discharge nozzle for a solid rocket

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT182911B (en) * 1951-02-09 1955-08-25 Plansee Metallwerk Nozzle for jet propulsion (rockets)
GB759350A (en) * 1953-12-01 1956-10-17 English Electric Co Ltd Improvements in and relating to blast tubes
DE1069951B (en) * 1954-09-11 1959-11-26 The Carborundum Company, Niagara Fall's, N. Y. (V. St. A.) Device for burning fuel and for directed discharge of Verforeninuriigsgase, in particular for rocket engines
US2849860A (en) * 1955-10-17 1958-09-02 Norton Co Rocket motor with recrystallized silicon carbide throat insert
US2835107A (en) * 1956-12-21 1958-05-20 Haveg Industries Inc Resins and use thereof
DE1039787B (en) * 1957-06-08 1958-09-25 Ici Ltd Nozzles for engines with rocket propulsion
US3001362A (en) * 1957-07-26 1961-09-26 Russell Mfg Co Insulator for rocket motor
FR1281740A (en) * 1961-02-27 1962-01-12 Ici Ltd Expansion cone for the nozzle of a rocket engine

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2499977A1 (en) * 1981-02-18 1982-08-20 Messerschmitt Boelkow Blohm INSULATING LAYER FOR PROPULSIVE LOADS

Also Published As

Publication number Publication date
DE1235675B (en) 1967-03-02
GB984486A (en) 1965-02-24

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