RU2001133736A - DEVICE FOR REGULATING TRANSMISSION OF HEAT TO THE WALL OF THE NOZZLE OF ROCKET ENGINES WITH AN EXTENSION CYCLE - Google Patents
DEVICE FOR REGULATING TRANSMISSION OF HEAT TO THE WALL OF THE NOZZLE OF ROCKET ENGINES WITH AN EXTENSION CYCLEInfo
- Publication number
- RU2001133736A RU2001133736A RU2001133736/06A RU2001133736A RU2001133736A RU 2001133736 A RU2001133736 A RU 2001133736A RU 2001133736/06 A RU2001133736/06 A RU 2001133736/06A RU 2001133736 A RU2001133736 A RU 2001133736A RU 2001133736 A RU2001133736 A RU 2001133736A
- Authority
- RU
- Russia
- Prior art keywords
- nozzle
- wall
- rocket engines
- heat
- extension cycle
- Prior art date
Links
- 230000005540 biological transmission Effects 0.000 title 1
- 230000001105 regulatory Effects 0.000 title 1
- 230000003746 surface roughness Effects 0.000 claims 3
- 230000002708 enhancing Effects 0.000 claims 2
- 238000001816 cooling Methods 0.000 claims 1
- 230000003094 perturbing Effects 0.000 claims 1
- 239000003507 refrigerant Substances 0.000 claims 1
Claims (3)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0000895-3 | 2000-03-17 | ||
SE0000895A SE516046C2 (en) | 2000-03-17 | 2000-03-17 | Device for controlling the heat transfer to the nozzle wall of rocket-type rocket motors |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2001133736A true RU2001133736A (en) | 2003-08-10 |
RU2264555C2 RU2264555C2 (en) | 2005-11-20 |
Family
ID=20278854
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2001133736/06A RU2264555C2 (en) | 2000-03-17 | 2001-03-16 | Device to control transfer of heat to wall of nozzle of rocket engines with expansion cycle |
Country Status (11)
Country | Link |
---|---|
US (1) | US6675571B2 (en) |
EP (1) | EP1179132B1 (en) |
JP (1) | JP4570310B2 (en) |
CN (1) | CN1178000C (en) |
AU (1) | AU4294201A (en) |
DE (1) | DE60108016T2 (en) |
ES (1) | ES2233617T3 (en) |
RU (1) | RU2264555C2 (en) |
SE (1) | SE516046C2 (en) |
UA (1) | UA70364C2 (en) |
WO (1) | WO2001069070A1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
SE512942C2 (en) * | 1998-10-02 | 2000-06-12 | Volvo Aero Corp | Procedure for manufacturing rocket engine outlet nozzles |
DE10054333B4 (en) | 2000-11-02 | 2006-11-30 | Eads Space Transportation Gmbh | Combustion chamber with increased heat input into a cooling device |
US20080264372A1 (en) * | 2007-03-19 | 2008-10-30 | Sisk David B | Two-stage ignition system |
Family Cites Families (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2022517A1 (en) * | 1970-05-08 | 1971-11-25 | Messerschmitt Boelkow Blohm | Rocket engine nozzle with boundary layer suction |
JPS62261652A (en) * | 1986-05-07 | 1987-11-13 | Natl Space Dev Agency Japan<Nasda> | Liquid rocket engine |
US4799543A (en) * | 1987-11-12 | 1989-01-24 | Arthur H. Iversen | Means for temperature control of heated surfaces |
US5410874A (en) * | 1990-11-19 | 1995-05-02 | United Technologies Corporation | Method and apparatus for increasing combustion chamber pressure in a high pressure expander cycle rocket engine |
DE4116396C2 (en) * | 1991-05-18 | 1996-04-25 | Grace Gmbh | Modified amorphous silica, process for their preparation and antiblocking agents |
US5267437A (en) * | 1991-05-23 | 1993-12-07 | United Technologies Corporation | Dual mode rocket engine |
FR2691209B1 (en) | 1992-05-18 | 1995-09-01 | Europ Propulsion | ENCLOSURE CONTAINING HOT GASES COOLED BY BREATHING, IN PARTICULAR A PROPULSIVE CHAMBER OF A ROCKET ENGINE, AND A MANUFACTURING METHOD THEREOF. |
JPH07243351A (en) * | 1994-03-03 | 1995-09-19 | Mitsubishi Heavy Ind Ltd | Fluid heat exchanger |
US5832719A (en) * | 1995-12-18 | 1998-11-10 | United Technologies Corporation | Rocket thrust chamber |
DE10054333B4 (en) * | 2000-11-02 | 2006-11-30 | Eads Space Transportation Gmbh | Combustion chamber with increased heat input into a cooling device |
-
2000
- 2000-03-17 SE SE0000895A patent/SE516046C2/en not_active IP Right Cessation
-
2001
- 2001-03-16 EP EP01915998A patent/EP1179132B1/en not_active Expired - Lifetime
- 2001-03-16 RU RU2001133736/06A patent/RU2264555C2/en not_active IP Right Cessation
- 2001-03-16 ES ES01915998T patent/ES2233617T3/en not_active Expired - Lifetime
- 2001-03-16 AU AU42942/01A patent/AU4294201A/en not_active Abandoned
- 2001-03-16 DE DE60108016T patent/DE60108016T2/en not_active Expired - Lifetime
- 2001-03-16 UA UA2001117853A patent/UA70364C2/en unknown
- 2001-03-16 WO PCT/SE2001/000555 patent/WO2001069070A1/en active IP Right Grant
- 2001-03-16 CN CNB018005497A patent/CN1178000C/en not_active Expired - Fee Related
- 2001-03-16 US US09/980,481 patent/US6675571B2/en not_active Expired - Fee Related
- 2001-03-16 JP JP2001567925A patent/JP4570310B2/en not_active Expired - Fee Related
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