SE0100078D0 - Rocket engines - Google Patents
Rocket enginesInfo
- Publication number
- SE0100078D0 SE0100078D0 SE0100078A SE0100078A SE0100078D0 SE 0100078 D0 SE0100078 D0 SE 0100078D0 SE 0100078 A SE0100078 A SE 0100078A SE 0100078 A SE0100078 A SE 0100078A SE 0100078 D0 SE0100078 D0 SE 0100078D0
- Authority
- SE
- Sweden
- Prior art keywords
- nozzle
- rocket engines
- cooling channels
- wall structure
- wall
- Prior art date
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)
- Testing Of Engines (AREA)
- Laser Beam Processing (AREA)
Abstract
The nozzle member(10) has an outer load bearing wall structure(14) with multiple tubular cooling channels(11) running from inlet(12) to exit(13) of the nozzle along the inside of the wall(14). A material with a higher thermal conductivity than the wall structure(14) is applied to the inside of the nozzle to link and/or surround the cooling channels(11).
Priority Applications (9)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0100078A SE520268C2 (en) | 2001-01-11 | 2001-01-11 | Liquid fuel rocket engine nozzle member and associated method of manufacture |
RU2003123786/06A RU2273756C2 (en) | 2001-01-11 | 2002-01-09 | Component of rocket engine and method for manufacture of rocket engine component |
PCT/SE2002/000025 WO2002055862A1 (en) | 2001-01-11 | 2002-01-09 | Rocket engine member and method for manufacturing a rocket engine member |
JP2002556492A JP4019217B2 (en) | 2001-01-11 | 2002-01-09 | Rocket engine member and method for manufacturing rocket engine member |
AT02729605T ATE331133T1 (en) | 2001-01-11 | 2002-01-09 | ROCKET ENGINE ELEMENT AND METHOD FOR PRODUCING A ROCKET ENGINE ELEMENT |
ES02729605T ES2266498T3 (en) | 2001-01-11 | 2002-01-09 | ROCKET ENGINE ELEMENT AND PROCEDURE FOR THE SAME MANUFACTURE. |
EP02729605A EP1352168B1 (en) | 2001-01-11 | 2002-01-09 | Rocket engine member and method for manufacturing a rocket engine member |
DE60212568T DE60212568T2 (en) | 2001-01-11 | 2002-01-09 | ROCKET DEVICE MEMBER AND METHOD FOR PRODUCING A ROCKET DEVICE MEMBER |
US10/604,329 US6799418B2 (en) | 2001-01-11 | 2003-07-11 | Rocket engine member and method for manufacturing a rocket engine member |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE0100078A SE520268C2 (en) | 2001-01-11 | 2001-01-11 | Liquid fuel rocket engine nozzle member and associated method of manufacture |
Publications (3)
Publication Number | Publication Date |
---|---|
SE0100078D0 true SE0100078D0 (en) | 2001-01-11 |
SE0100078L SE0100078L (en) | 2002-07-12 |
SE520268C2 SE520268C2 (en) | 2003-06-17 |
Family
ID=20282598
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE0100078A SE520268C2 (en) | 2001-01-11 | 2001-01-11 | Liquid fuel rocket engine nozzle member and associated method of manufacture |
Country Status (1)
Country | Link |
---|---|
SE (1) | SE520268C2 (en) |
-
2001
- 2001-01-11 SE SE0100078A patent/SE520268C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
SE0100078L (en) | 2002-07-12 |
SE520268C2 (en) | 2003-06-17 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NUG | Patent has lapsed |