DE69511016D1 - Mit Rohren ausgekleidetes Schubrohr einer Rakete - Google Patents

Mit Rohren ausgekleidetes Schubrohr einer Rakete

Info

Publication number
DE69511016D1
DE69511016D1 DE69511016T DE69511016T DE69511016D1 DE 69511016 D1 DE69511016 D1 DE 69511016D1 DE 69511016 T DE69511016 T DE 69511016T DE 69511016 T DE69511016 T DE 69511016T DE 69511016 D1 DE69511016 D1 DE 69511016D1
Authority
DE
Germany
Prior art keywords
rocket
lined
pipes
thrust tube
thrust
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 - Fee Related
Application number
DE69511016T
Other languages
English (en)
Other versions
DE69511016T2 (de
Inventor
Joaquin H Castro
Samuel S Owen
Salvatore Santangelo
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.)
Raytheon Technologies Corp
Original Assignee
United Technologies 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 United Technologies Corp filed Critical United Technologies Corp
Publication of DE69511016D1 publication Critical patent/DE69511016D1/de
Application granted granted Critical
Publication of DE69511016T2 publication Critical patent/DE69511016T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02K9/42—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)
  • Heat-Exchange Devices With Radiators And Conduit Assemblies (AREA)
  • Testing Of Engines (AREA)
DE69511016T 1994-08-16 1995-04-20 Mit Rohren ausgekleidetes Schubrohr einer Rakete Expired - Fee Related DE69511016T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/291,385 US5557928A (en) 1994-08-16 1994-08-16 Tube rocket thrust chamber construction and method

Publications (2)

Publication Number Publication Date
DE69511016D1 true DE69511016D1 (de) 1999-09-02
DE69511016T2 DE69511016T2 (de) 2000-02-03

Family

ID=23120088

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69511016T Expired - Fee Related DE69511016T2 (de) 1994-08-16 1995-04-20 Mit Rohren ausgekleidetes Schubrohr einer Rakete

Country Status (4)

Country Link
US (1) US5557928A (de)
EP (1) EP0697515B1 (de)
JP (1) JP3681442B2 (de)
DE (1) DE69511016T2 (de)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6579085B1 (en) 2000-05-05 2003-06-17 The Boc Group, Inc. Burner and combustion method for the production of flame jet sheets in industrial furnaces
US6832471B2 (en) * 2003-03-12 2004-12-21 Aerojet-General Corporation Expander cycle rocket engine with staged combustion and heat exchange
US7051513B2 (en) * 2003-06-06 2006-05-30 United Technologies Corporation Rocket engine tubular chamber with single piece jacket
US7213392B2 (en) * 2003-06-10 2007-05-08 United Technologies Corporation Rocket engine combustion chamber
US7373774B2 (en) * 2004-02-12 2008-05-20 United Technologies Corporation Enhanced performance torroidal coolant-collection manifold
US7464537B2 (en) * 2005-04-04 2008-12-16 United Technologies Corporation Heat transfer enhancement features for a tubular wall combustion chamber
US20110116934A1 (en) * 2009-11-16 2011-05-19 Meng Sen Y Pumping element design
US9194335B2 (en) 2012-03-09 2015-11-24 Aerojet Rocketdyne Of De, Inc. Rocket engine coolant system including an exit manifold having at least one flow guide within the manifold
DE102016215244A1 (de) * 2016-08-16 2018-02-22 Airbus Ds Gmbh Brennkammerstruktur, insbesondere für ein raketentriebwerk
CN114112417A (zh) * 2021-11-24 2022-03-01 中国人民解放军国防科技大学 一种可重复使用液体火箭发动机推力室寿命预估方法

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2991617A (en) * 1950-12-01 1961-07-11 Gen Electric Jet motor combustion chamber
US2956399A (en) * 1956-11-16 1960-10-18 Clair M Beighley Fluid cooled homogeneous ceramic rocket motor wall structure
US3004386A (en) * 1959-06-23 1961-10-17 United Aircraft Corp Rocket nozzle tube construction
US3062566A (en) * 1959-06-25 1962-11-06 United Aircraft Corp Manifold attachment to tubular wall
US3714785A (en) * 1966-02-11 1973-02-06 North American Rockwell Rocket engine nozzle with gas spike
DE1264160B (de) * 1966-12-15 1968-03-21 Boelkow Gmbh Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
US3516254A (en) * 1967-09-11 1970-06-23 United Aircraft Corp Closed-loop rocket propellant cycle
US3578030A (en) * 1967-09-27 1971-05-11 Hitco Ablative and insulative structures
DE1941296B2 (de) * 1969-08-14 1971-09-30 Messerschmitt Bolkow Blohm GmbH, 8000 München Durch ein fluessiges medium regenerativ gekuehlte brenn kammer mit schubduese
DE2015024B2 (de) * 1970-03-28 1971-10-14 Messerschmitt Bolkow Blohm GmbH, 8000 München Verfahren zur herstellung von regenerativ gekuehlten brenn kammern und oder schubduesen
US3714695A (en) * 1970-09-17 1973-02-06 Us Air Force Method for forming thrust chambers
US3713293A (en) * 1970-10-08 1973-01-30 Maschf Augsburg Nuernberg Ag Combustion chamber and nozzle arrangement for a rocket engine
US3782118A (en) * 1972-12-18 1974-01-01 Messerschmitt Boelkow Blohm Regeneratively cooled thrust gas generator construction and method of making same
US4107919A (en) * 1975-03-19 1978-08-22 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Heat exchanger
US4781019A (en) * 1983-04-04 1988-11-01 Rockwell International Corporation Keel-rib coolant channels for rocket combustors
US4912925A (en) * 1985-10-04 1990-04-03 United Technologies Corporation Rocket engine with redundant capabilities
US5267437A (en) * 1991-05-23 1993-12-07 United Technologies Corporation Dual mode rocket engine

Also Published As

Publication number Publication date
DE69511016T2 (de) 2000-02-03
EP0697515B1 (de) 1999-07-28
US5557928A (en) 1996-09-24
JPH0861149A (ja) 1996-03-05
JP3681442B2 (ja) 2005-08-10
EP0697515A3 (de) 1996-09-04
EP0697515A2 (de) 1996-02-21

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee