RU2011145928A - LIQUID ROCKET ENGINE BLOCK - Google Patents
LIQUID ROCKET ENGINE BLOCK Download PDFInfo
- Publication number
- RU2011145928A RU2011145928A RU2011145928/11A RU2011145928A RU2011145928A RU 2011145928 A RU2011145928 A RU 2011145928A RU 2011145928/11 A RU2011145928/11 A RU 2011145928/11A RU 2011145928 A RU2011145928 A RU 2011145928A RU 2011145928 A RU2011145928 A RU 2011145928A
- Authority
- RU
- Russia
- Prior art keywords
- protection device
- rocket engine
- combustion chamber
- engine block
- cooling
- Prior art date
Links
Landscapes
- Testing Of Engines (AREA)
Abstract
Блок тяги жидкостного ракетного двигателя, содержащий раму, камеру сгорания с соплом и устройство защиты блока тяги, имеющее донные экраны, отличающийся тем, что устройство защиты блока тяги дополнительно оснащено устройством тепловой защиты рамы, выполненным в виде устройства охлаждения стенки камеры сгорания.A thrust unit of a liquid propellant rocket engine comprising a frame, a combustion chamber with a nozzle, and a thrust block protection device having bottom screens, characterized in that the thrust block protection device is additionally equipped with a thermal frame protection device made in the form of a cooling device for cooling the wall of the combustion chamber.
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011145928/11A RU2502645C2 (en) | 2011-11-11 | 2011-11-11 | Liquid-propellant rocket engine thrust unit |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU2011145928/11A RU2502645C2 (en) | 2011-11-11 | 2011-11-11 | Liquid-propellant rocket engine thrust unit |
Publications (2)
Publication Number | Publication Date |
---|---|
RU2011145928A true RU2011145928A (en) | 2013-05-20 |
RU2502645C2 RU2502645C2 (en) | 2013-12-27 |
Family
ID=48788885
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU2011145928/11A RU2502645C2 (en) | 2011-11-11 | 2011-11-11 | Liquid-propellant rocket engine thrust unit |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2502645C2 (en) |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5832719A (en) * | 1995-12-18 | 1998-11-10 | United Technologies Corporation | Rocket thrust chamber |
US6799417B2 (en) * | 2003-02-05 | 2004-10-05 | Aerojet-General Corporation | Diversion of combustion gas within a rocket engine to preheat fuel |
RU2347725C2 (en) * | 2006-11-20 | 2009-02-27 | Федеральное государственное унитарное предприятие Государственный научно-производственный ракетно-космический центр "ЦСКБ-ПРОГРЕСС" (ФГУП ГНПРКЦ "ЦСКБ-ПРОГРЕСС") | Rocket-carrier rocket tail compartment bottom protection |
RU2431756C1 (en) * | 2010-05-18 | 2011-10-20 | Николай Борисович Болотин | Liquid propellant engine with controlled thrust vector, and nozzle block of roll |
-
2011
- 2011-11-11 RU RU2011145928/11A patent/RU2502645C2/en not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2502645C2 (en) | 2013-12-27 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MM4A | The patent is invalid due to non-payment of fees |
Effective date: 20201112 |