DE69905688T2 - Verfahren zur Herstellung eines Raketenschubrohres - Google Patents

Verfahren zur Herstellung eines Raketenschubrohres

Info

Publication number
DE69905688T2
DE69905688T2 DE69905688T DE69905688T DE69905688T2 DE 69905688 T2 DE69905688 T2 DE 69905688T2 DE 69905688 T DE69905688 T DE 69905688T DE 69905688 T DE69905688 T DE 69905688T DE 69905688 T2 DE69905688 T2 DE 69905688T2
Authority
DE
Germany
Prior art keywords
making
push tube
rocket
rocket push
tube
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
DE69905688T
Other languages
English (en)
Other versions
DE69905688D1 (de
Inventor
Louis W Cote
Michael R Morton
Thomas R Hernacki
Richard L Rose
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
Application granted granted Critical
Publication of DE69905688D1 publication Critical patent/DE69905688D1/de
Publication of DE69905688T2 publication Critical patent/DE69905688T2/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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00—Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/008—Rocket engine parts, e.g. nozzles, combustion chambers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23P—METAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00—Restoring or reconditioning objects
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/49346—Rocket or jet device making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/4935—Heat exchanger or boiler making
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00—Metal working
    • Y10T29/49—Method of mechanical manufacture
    • Y10T29/4998—Combined manufacture including applying or shaping of fluent material
    • Y10T29/49982—Coating

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • General Engineering & Computer Science (AREA)
  • Powder Metallurgy (AREA)
  • Coating By Spraying Or Casting (AREA)
DE69905688T 1998-11-30 1999-11-29 Verfahren zur Herstellung eines Raketenschubrohres Expired - Fee Related DE69905688T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/201,476 US6131280A (en) 1998-11-30 1998-11-30 Method of repairing a rocket thrust chamber

Publications (2)

Publication Number Publication Date
DE69905688D1 DE69905688D1 (de) 2003-04-10
DE69905688T2 true DE69905688T2 (de) 2003-10-02

Family

ID=22745980

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69905688T Expired - Fee Related DE69905688T2 (de) 1998-11-30 1999-11-29 Verfahren zur Herstellung eines Raketenschubrohres

Country Status (5)

Country Link
US (1) US6131280A (de)
EP (1) EP1005948B1 (de)
JP (1) JP2000158240A (de)
KR (1) KR100581302B1 (de)
DE (1) DE69905688T2 (de)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10043303B4 (de) * 2000-09-02 2004-06-09 Astrium Gmbh Raketentriebwerk in Segmentbauweise
CN110732844B (zh) * 2019-10-25 2020-10-09 湖北三江航天江北机械工程有限公司 多接头火箭壳体加工方法

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1264160B (de) * 1966-12-15 1968-03-21 Boelkow Gmbh Fluessigkeitsgekuehlte Bauteile, wie Raketenbrennkammern, und Verfahren zu deren Herstellung
JPS6082603A (ja) * 1983-10-07 1985-05-10 Natl Aerospace Lab ロケツト燃焼器製作法
FR2669966B1 (fr) * 1990-11-30 1993-03-26 Europ Propulsion Procede de fabrication de paroi de chambre de combustion, notamment pour moteur-fusee, et chambre de combustion obtenue par ce procede.
US5386628A (en) * 1991-12-23 1995-02-07 United Technologies Corporation Method of making a diffusion bonded rocket chamber
US5249357A (en) * 1993-01-27 1993-10-05 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of fabricating a rocket engine combustion chamber
US5477613A (en) * 1993-12-21 1995-12-26 United Technologies Corporation Method of simultaneously forming rocket thrust chamber cooling tubes
US5473817A (en) * 1993-12-21 1995-12-12 United Technologies Corporation Method of making cooled rocket combustion chamber construction
EP0758283B1 (de) * 1994-04-29 1998-01-28 United Technologies Corporation Herstellung von rohrwand-raketenbrennkammern mit hilfe von laser-auftragschweissen
US5546656A (en) * 1994-11-30 1996-08-20 United Technologies Corporation Fabrication of rocket thrust chambers
US5832719A (en) * 1995-12-18 1998-11-10 United Technologies Corporation Rocket thrust chamber
FR2776215B1 (fr) 1998-03-20 2000-06-16 Snecma Procede de fabrication d'un circuit regeneratif a fort flux thermique, notamment pour chambre de combustion de moteur-fusee

Also Published As

Publication number Publication date
DE69905688D1 (de) 2003-04-10
EP1005948A1 (de) 2000-06-07
KR20000035726A (ko) 2000-06-26
EP1005948B1 (de) 2003-03-05
JP2000158240A (ja) 2000-06-13
US6131280A (en) 2000-10-17
KR100581302B1 (ko) 2006-05-22

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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