BE530924A - - Google Patents

Info

Publication number
BE530924A
BE530924A BE530924DA BE530924A BE 530924 A BE530924 A BE 530924A BE 530924D A BE530924D A BE 530924DA BE 530924 A BE530924 A BE 530924A
Authority
BE
Belgium
Application number
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 filed Critical
Publication of BE530924A publication Critical patent/BE530924A/xx

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
    • F02K9/42—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)
  • Testing Of Engines (AREA)
  • Spray-Type Burners (AREA)
BE530924D 1951-12-06 1954-08-04 BE530924A (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB28596/51A GB759901A (en) 1951-12-06 1951-12-06 Combustion chambers

Publications (1)

Publication Number Publication Date
BE530924A true BE530924A (de) 1957-10-25

Family

ID=10278106

Family Applications (1)

Application Number Title Priority Date Filing Date
BE530924D BE530924A (de) 1951-12-06 1954-08-04

Country Status (6)

Country Link
US (1) US2705399A (de)
BE (1) BE530924A (de)
CH (1) CH328859A (de)
DE (1) DE953206C (de)
FR (1) FR1106090A (de)
GB (1) GB759901A (de)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1097764B (de) * 1956-07-05 1961-01-19 Bristol Siddeley Engines Ltd Raketenantrieb
US3383858A (en) * 1956-08-09 1968-05-21 North American Rockwell Nuclear rocket engine
US2956399A (en) * 1956-11-16 1960-10-18 Clair M Beighley Fluid cooled homogeneous ceramic rocket motor wall structure
US2933888A (en) * 1956-11-23 1960-04-26 Africano Alfred Cooling system for a rocket engine
US2926490A (en) * 1957-03-19 1960-03-01 Thiokol Chemical Corp Laminated fluid-jacketed thrust chamber structure
US2977754A (en) * 1958-01-29 1961-04-04 Thiokol Chemical Corp Rocket chamber with multi-pass axial flow coolant passageways
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
US3122883A (en) * 1959-11-20 1964-03-03 Thompson Ramo Wooldridge Inc Heat resistant wall structure for rocket motor nozzles and the like
DE1159694B (de) * 1960-08-26 1963-12-19 United Aircraft Corp Einspritzkopf fuer eine Fluessigkeitsrakete
US3142541A (en) * 1961-08-18 1964-07-28 Chandler Evans Corp Gas generator for rocket propellants
US3439502A (en) * 1966-01-25 1969-04-22 North American Rockwell Cooling of gas generators
US3439503A (en) * 1966-01-25 1969-04-22 North American Rockwell Rocket engine cooling
US3353359A (en) * 1966-01-26 1967-11-21 James E Webb Multislot film cooled pyrolytic graphite rocket nozzle
GB1220223A (en) * 1967-01-16 1971-01-20 Messerschmitt Boelkow Blohm A liquid cooled rocket combustion chamber with thrust nozzle
US3585800A (en) * 1967-07-27 1971-06-22 Aerojet General Co Transpiration-cooled devices
US3710574A (en) * 1969-07-22 1973-01-16 R Pearson Fluid distribution and injection systems
US4625509A (en) * 1980-04-21 1986-12-02 Sheppard Sr Darrel J Combustion engine
US4800718A (en) * 1986-12-24 1989-01-31 The United States Of America As Represented By The Secretary Of The Air Force Surface cooling system
JPH0659502B2 (ja) * 1987-03-26 1994-08-10 宇宙科学研究所長 ロケット用高圧燃焼器の燃焼室及びその製造方法
EP0374382A1 (de) * 1988-12-21 1990-06-27 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Kühlung von Hyperschallantriebskomponenten
US7213392B2 (en) * 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
DE10340826A1 (de) * 2003-09-04 2005-03-31 Rolls-Royce Deutschland Ltd & Co Kg Homogene Gemischbildung durch verdrallte Einspritzung des Kraftstoffs
US7370469B2 (en) * 2004-12-13 2008-05-13 United Technologies Corporation Rocket chamber heat exchanger
FR2963063B1 (fr) * 2010-07-26 2015-11-27 Snecma Chambre de combustion munie d'un element tubulaire
DE102016215244A1 (de) * 2016-08-16 2018-02-22 Airbus Ds Gmbh Brennkammerstruktur, insbesondere für ein raketentriebwerk
US11598290B2 (en) * 2021-07-02 2023-03-07 Korea Aerospace Research Institute Combustor of liquid rocket engine

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH66802A (de) * 1913-07-25 1914-10-16 Maschf Augsburg Nuernberg Ag Verbrennungskammer für Verbrennungskraftmaschinen
DE716175C (de) * 1935-02-09 1942-01-14 Eugen Saenger Dr Ing Raketenmotor
BE446918A (de) * 1941-07-12
GB578007A (en) * 1941-11-07 1946-06-12 Asiatic Petroleum Co Ltd Improvements in combustion chamber linings
DE850254C (de) * 1949-05-06 1952-09-22 Metz Carl Brennkraftturbine
DE811890C (de) * 1949-06-29 1951-08-23 Karl Dr-Ing Roeder Gas-Dampf-Turbine

Also Published As

Publication number Publication date
CH328859A (fr) 1958-03-31
DE953206C (de) 1956-11-29
FR1106090A (fr) 1955-12-12
US2705399A (en) 1955-04-05
GB759901A (en) 1956-10-24

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