UA86958C2 - Liquid rocket engine with regulated thrust vector - Google Patents
Liquid rocket engine with regulated thrust vectorInfo
- Publication number
- UA86958C2 UA86958C2 UAA200607625A UAA200607625A UA86958C2 UA 86958 C2 UA86958 C2 UA 86958C2 UA A200607625 A UAA200607625 A UA A200607625A UA A200607625 A UAA200607625 A UA A200607625A UA 86958 C2 UA86958 C2 UA 86958C2
- Authority
- UA
- Ukraine
- Prior art keywords
- nozzle
- injection
- unit
- thrust vector
- collector
- Prior art date
Links
Landscapes
- Jet Pumps And Other Pumps (AREA)
Abstract
A liquid rocket engine with controlled thrust vector has a combustion chamber with nozzle, turbo-pump system for supply of fuel components to the combustion chamber, turbine exhaust collector of which is connected to circular collector of unit for exhaust gas injection to supersonic section of the nozzle. Upstream of circular slot of unit for exhaust gas injection in each one fourth section of the nozzle units for fuel component injection are installed, those are connected to fuel high-pressure line of engine placed downstream of outlet collector of cooling section of the chamber and connected to drives controlled by the system for engine thrust vector control. Each injection unit has either centrifugal, or jet injection nozzles provided in the wall of the nozzle or in movable two-position solid interceptor in the part that is introduced to supersonic flow of the nozzle, at that at inlet to each injection unit a generator of pressure pulses of liquid fuel component supplied to nozzle is installed.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200607625A UA86958C2 (en) | 2006-07-07 | 2006-07-07 | Liquid rocket engine with regulated thrust vector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
UAA200607625A UA86958C2 (en) | 2006-07-07 | 2006-07-07 | Liquid rocket engine with regulated thrust vector |
Publications (1)
Publication Number | Publication Date |
---|---|
UA86958C2 true UA86958C2 (en) | 2009-06-10 |
Family
ID=50631594
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
UAA200607625A UA86958C2 (en) | 2006-07-07 | 2006-07-07 | Liquid rocket engine with regulated thrust vector |
Country Status (1)
Country | Link |
---|---|
UA (1) | UA86958C2 (en) |
-
2006
- 2006-07-07 UA UAA200607625A patent/UA86958C2/en unknown
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