DE69905688D1 - Verfahren zur Herstellung eines Raketenschubrohres - Google Patents
Verfahren zur Herstellung eines RaketenschubrohresInfo
- Publication number
- DE69905688D1 DE69905688D1 DE69905688T DE69905688T DE69905688D1 DE 69905688 D1 DE69905688 D1 DE 69905688D1 DE 69905688 T DE69905688 T DE 69905688T DE 69905688 T DE69905688 T DE 69905688T DE 69905688 D1 DE69905688 D1 DE 69905688D1
- 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
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)
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 true DE69905688D1 (de) | 2003-04-10 |
DE69905688T2 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)
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)
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 |
-
1998
- 1998-11-30 US US09/201,476 patent/US6131280A/en not_active Expired - Fee Related
-
1999
- 1999-11-26 JP JP11336068A patent/JP2000158240A/ja active Pending
- 1999-11-26 KR KR1019990052947A patent/KR100581302B1/ko not_active IP Right Cessation
- 1999-11-29 DE DE69905688T patent/DE69905688T2/de not_active Expired - Fee Related
- 1999-11-29 EP EP99309529A patent/EP1005948B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
KR100581302B1 (ko) | 2006-05-22 |
EP1005948A1 (de) | 2000-06-07 |
DE69905688T2 (de) | 2003-10-02 |
KR20000035726A (ko) | 2000-06-26 |
EP1005948B1 (de) | 2003-03-05 |
JP2000158240A (ja) | 2000-06-13 |
US6131280A (en) | 2000-10-17 |
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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 |