RU2002100639A - Rocket engine chamber - Google Patents
Rocket engine chamberInfo
- Publication number
- RU2002100639A RU2002100639A RU2002100639/06A RU2002100639A RU2002100639A RU 2002100639 A RU2002100639 A RU 2002100639A RU 2002100639/06 A RU2002100639/06 A RU 2002100639/06A RU 2002100639 A RU2002100639 A RU 2002100639A RU 2002100639 A RU2002100639 A RU 2002100639A
- Authority
- RU
- Russia
- Prior art keywords
- housing
- nozzle
- welding
- expanding
- rocket engine
- Prior art date
Links
- 238000003466 welding Methods 0.000 claims 4
- 238000002485 combustion reaction Methods 0.000 claims 3
- 229910001260 Pt alloy Inorganic materials 0.000 claims 2
- 229910000831 Steel Inorganic materials 0.000 claims 2
- 239000010959 steel Substances 0.000 claims 2
- 210000001503 Joints Anatomy 0.000 claims 1
- 238000010894 electron beam technology Methods 0.000 claims 1
- GKOZUEZYRPOHIO-UHFFFAOYSA-N iridium Chemical compound [Ir] GKOZUEZYRPOHIO-UHFFFAOYSA-N 0.000 claims 1
- 229910052741 iridium Inorganic materials 0.000 claims 1
- MHOVAHRLVXNVSD-UHFFFAOYSA-N rhodium Chemical compound [Rh] MHOVAHRLVXNVSD-UHFFFAOYSA-N 0.000 claims 1
- 229910052703 rhodium Inorganic materials 0.000 claims 1
- 239000010948 rhodium Substances 0.000 claims 1
Claims (4)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19927734A DE19927734C2 (en) | 1999-06-17 | 1999-06-17 | Thrust chamber of a propulsion engine for satellites and transport devices for space applications |
DE19927734.6 | 1999-06-17 |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2002100639A true RU2002100639A (en) | 2003-08-20 |
RU2220313C2 RU2220313C2 (en) | 2003-12-27 |
Family
ID=7911610
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2002100639/06A RU2220313C2 (en) | 1999-06-17 | 2000-06-06 | Rocket engine chamber housing |
Country Status (6)
Country | Link |
---|---|
US (1) | US6705076B1 (en) |
EP (1) | EP1187979B1 (en) |
JP (1) | JP4394320B2 (en) |
DE (2) | DE19927734C2 (en) |
RU (1) | RU2220313C2 (en) |
WO (1) | WO2000079116A1 (en) |
Families Citing this family (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20070012370A1 (en) * | 2005-07-18 | 2007-01-18 | Honeywell International, Inc. | Facetted high temperature thruster design |
JP5098111B2 (en) * | 2006-07-07 | 2012-12-12 | 独立行政法人物質・材料研究機構 | Method for producing mold for glass press |
US20080264372A1 (en) * | 2007-03-19 | 2008-10-30 | Sisk David B | Two-stage ignition system |
US8512808B2 (en) * | 2008-04-28 | 2013-08-20 | The Boeing Company | Built-up composite structures with a graded coefficient of thermal expansion for extreme environment applications |
KR101014787B1 (en) | 2008-08-26 | 2011-02-14 | 한국항공우주연구원 | A Head of the Liquid Rocket Thrust chamber |
US8667776B2 (en) * | 2009-02-23 | 2014-03-11 | Raytheon Company | Pellet-loaded multiple impulse rocket motor |
RU2563289C1 (en) * | 2014-05-13 | 2015-09-20 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр имени М.В. Хруничева" (ФГУП "ГКНПЦ им. М.В. Хруничева") | Method of fabrication of internal shell of nozzle of combustion chamber of liquid-propellant rocket engine (lpre) |
WO2019108306A1 (en) * | 2017-12-02 | 2019-06-06 | Aerojet Rocketdyne, Inc. | Copper combustion chamber attached to injector by non-copper weld transition ring |
CN110159456B (en) * | 2019-04-16 | 2020-07-14 | 上海空间推进研究所 | Rocket engine thrust chamber |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2405465A (en) * | 1943-05-07 | 1946-08-06 | Aerojet Engineering Corp | Jet propulsion motor |
US3044257A (en) * | 1958-06-02 | 1962-07-17 | Thiokol Chemical Corp | Combustion chamber outer jacket |
US3167909A (en) * | 1961-04-24 | 1965-02-02 | Thompson Ramo Wooldridge Inc | Self-cooled rocket nozzle |
US3443384A (en) * | 1967-05-17 | 1969-05-13 | Nasa | Swirling flow nozzle |
DE2166904A1 (en) * | 1971-12-01 | 1976-07-08 | Erno Raumfahrttechnik Gmbh | Rocket motor suitable for diverse fuels - has propulsion nozzle axially adjustable in combustion chamber |
CA1079078A (en) * | 1977-05-25 | 1980-06-10 | Michael N. Clark | Rocket nozzle assembly |
DE3300930C2 (en) * | 1983-01-13 | 1986-06-12 | Heraeus Elektroden GmbH, 6450 Hanau | Apparatus parts, in particular in the form of rings, some of which are provided with a coating material, their manufacturing process and use |
US4882904A (en) * | 1988-03-24 | 1989-11-28 | Aerojet-General Corporation | Two stage rocket combustor |
GB9418705D0 (en) * | 1994-09-16 | 1994-11-16 | Johnson Matthey Plc | Improvements in high temperature articles |
US5613299A (en) * | 1994-11-09 | 1997-03-25 | Ring; Peter J. | Method of fabricating a rocket thrust chamber |
EP0899447B1 (en) * | 1997-08-29 | 2003-12-03 | Hughes Electronics Corporation | Attachment ring for a rocket combustion chamber |
DE69812253T2 (en) * | 1997-08-29 | 2004-02-05 | Hughes Electronics Corp., El Segundo | Manufacture of a rocket engine with a connector between the combustion chamber and injector |
EP0899449B1 (en) * | 1997-08-29 | 2003-03-12 | Hughes Electronics Corporation | Rocket engine having a transition attachment between a combustion chamber and an injector |
US6138451A (en) * | 1998-05-11 | 2000-10-31 | Hughes Electronics Corporation | Rocket engine with combustion chamber step structure insert, and its fabrication |
US6138450A (en) * | 1998-05-11 | 2000-10-31 | Hughes Electronics Corporation | Rocket engine with integral combustion chamber step structure and its fabrication |
US6079101A (en) * | 1998-05-11 | 2000-06-27 | Hughes Electronics Corporation | Rocket engine with one-piece combustion chamber step structure, and its fabrication |
US6397580B1 (en) * | 1998-07-09 | 2002-06-04 | Bi-Propellant Rocket Research Corporation | High performance rocket engine having a stepped expansion combustion chamber and method of making the same |
RU2158666C2 (en) * | 1999-02-04 | 2000-11-10 | Открытое акционерное общество НПО Энергомаш им. акад. В.П. Глушко | Method of manufacturing welded-soldered structure |
US6205661B1 (en) * | 1999-04-15 | 2001-03-27 | Peter John Ring | Method of making a rocket thrust chamber |
-
1999
- 1999-06-17 DE DE19927734A patent/DE19927734C2/en not_active Expired - Fee Related
-
2000
- 2000-06-06 DE DE50009041T patent/DE50009041D1/en not_active Expired - Lifetime
- 2000-06-06 US US10/009,726 patent/US6705076B1/en not_active Expired - Lifetime
- 2000-06-06 EP EP00947783A patent/EP1187979B1/en not_active Expired - Lifetime
- 2000-06-06 JP JP2001505442A patent/JP4394320B2/en not_active Expired - Fee Related
- 2000-06-06 WO PCT/DE2000/001826 patent/WO2000079116A1/en active IP Right Grant
- 2000-06-06 RU RU2002100639/06A patent/RU2220313C2/en not_active IP Right Cessation
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