FR2599429B1 - SUPPORT STRUCTURE FOR A MOTOR ROCKET EXPANSION NOZZLE. - Google Patents

SUPPORT STRUCTURE FOR A MOTOR ROCKET EXPANSION NOZZLE.

Info

Publication number
FR2599429B1
FR2599429B1 FR8707375A FR8707375A FR2599429B1 FR 2599429 B1 FR2599429 B1 FR 2599429B1 FR 8707375 A FR8707375 A FR 8707375A FR 8707375 A FR8707375 A FR 8707375A FR 2599429 B1 FR2599429 B1 FR 2599429B1
Authority
FR
France
Prior art keywords
support structure
expansion nozzle
rocket
motor
motor 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 - Lifetime
Application number
FR8707375A
Other languages
French (fr)
Other versions
FR2599429A1 (en
Inventor
Manfred Lechner
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2599429A1 publication Critical patent/FR2599429A1/en
Application granted granted Critical
Publication of FR2599429B1 publication Critical patent/FR2599429B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Nozzles (AREA)
FR8707375A 1986-05-28 1987-05-26 SUPPORT STRUCTURE FOR A MOTOR ROCKET EXPANSION NOZZLE. Expired - Lifetime FR2599429B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19863618038 DE3618038A1 (en) 1986-05-28 1986-05-28 SUPPORT STRUCTURE FOR LIQUID-COOLED EXPANSION NOZZLES

Publications (2)

Publication Number Publication Date
FR2599429A1 FR2599429A1 (en) 1987-12-04
FR2599429B1 true FR2599429B1 (en) 1993-06-11

Family

ID=6301849

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8707375A Expired - Lifetime FR2599429B1 (en) 1986-05-28 1987-05-26 SUPPORT STRUCTURE FOR A MOTOR ROCKET EXPANSION NOZZLE.

Country Status (3)

Country Link
DE (1) DE3618038A1 (en)
FR (1) FR2599429B1 (en)
SE (1) SE461995B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0374382A1 (en) * 1988-12-21 1990-06-27 Messerschmitt-Bölkow-Blohm Gesellschaft mit beschränkter Haftung Cooling for components of hypersonic propulsors
DE4317807C1 (en) * 1993-05-28 1994-08-04 Mtu Muenchen Gmbh Thruster for jet drives with fasteners
US6715293B2 (en) * 2002-03-28 2004-04-06 United Technologies Corporation Scram jet engine design
RU2665601C1 (en) * 2017-04-13 2018-08-31 Акционерное общество "Конструкторское бюро химавтоматики" Nozzle of the liquid-propellant engine chamber

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2183313A (en) * 1938-07-07 1939-12-12 Robert H Goddard Combustion chamber for aircraft
GB607824A (en) * 1946-02-12 1948-09-06 Lucas Ltd Joseph Improvements relating to combustion chambers for prime movers
US2795108A (en) * 1953-10-07 1957-06-11 Westinghouse Electric Corp Combustion apparatus
US3908933A (en) * 1956-06-26 1975-09-30 Us Navy Guided missile
US2976679A (en) * 1956-12-10 1961-03-28 Robert C Veit Tubular rocket combustion chamber
US3105522A (en) * 1956-12-10 1963-10-01 Robert C Veit Tube of uniform depth and variable width
US3031844A (en) * 1960-08-12 1962-05-01 William A Tomolonius Split combustion liner
US3267664A (en) * 1963-03-19 1966-08-23 North American Aviation Inc Method of and device for cooling
US3398527A (en) * 1966-05-31 1968-08-27 Air Force Usa Corrugated wall radiation cooled combustion chamber
DE1273907B (en) * 1966-10-27 1968-07-25 Boelkow Gmbh Thermally highly stressed components, such as rocket combustion chambers, with sweat cooling and processes for their production
DE2356572C3 (en) * 1973-11-13 1979-03-29 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Liquid-cooled rocket combustion chamber with thrust nozzle
US4148121A (en) * 1974-06-12 1979-04-10 Messerschmitt-Bolkow-Blohm Gesellschaft Mit Beschrankter Haftung Method and apparatus for manufacturing rotationally symmetrical constructional parts such as nozzles and combination chambers of rocket engines
US4292810A (en) * 1979-02-01 1981-10-06 Westinghouse Electric Corp. Gas turbine combustion chamber
US4232527A (en) * 1979-04-13 1980-11-11 General Motors Corporation Combustor liner joints
US4512159A (en) * 1984-04-02 1985-04-23 United Technologies Corporation Clip attachment

Also Published As

Publication number Publication date
DE3618038A1 (en) 1987-12-03
SE461995B (en) 1990-04-23
SE8702012D0 (en) 1987-05-15
FR2599429A1 (en) 1987-12-04
SE8702012L (en) 1987-11-29
DE3618038C2 (en) 1988-10-20

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