FIELD: rocketry; liquid-propellant rocket engines. SUBSTANCE: combustion chamber includes gas passage, center injector face and unit of injector faces with gas and gas-and-liquid injectors. Injectors connect gas passage cavity with injector face cavity. Perforated diaphragm is mounted in gas passage above injector face unit forming resonance cavity of acoustic absorber. Inlet end faces of gas injectors are located at level of or above upper surface of diaphragm. EFFECT: enhanced operational reliability and stability of combustion at minor amount of additional parts. 7 cl, 8 dwg
Title | Year | Author | Number |
---|---|---|---|
LIQUID-PROPELLANT ROCKET ENGINE | 1999 |
|
RU2168049C2 |
LIQUID-PROPELLANT ROCKET ENGINE GAS GENERATOR | 1999 |
|
RU2179256C2 |
COMBUSTION CHAMBER OF CLOSED-LOOP LIQUID-PROPELLANT ROCKET ENGINE | 1995 |
|
RU2141052C1 |
GAS GENERATOR OF LIQUID-PROPELLANT ROCKET ENGINE | 2000 |
|
RU2204732C2 |
LIQUID-PROPELLANT ROCKET ENGINE WITH AFTERBURNING | 1999 |
|
RU2173785C2 |
GAS TURBINE DRIVE OF LIQUID-PROPELLANT ROCKET ENGINE | 1999 |
|
RU2168051C2 |
GAS PASSAGE OF LIQUID PROPELLANT ROCKET ENGINE | 2000 |
|
RU2186236C1 |
DEVICE DETERMINING BOUNDARY OF APPEARANCE OF INSTABILITY OF OPERATION PROCESS IN GAS GENERATOR OF LIQUID-PROPELLANT ROCKET ENGINE | 2000 |
|
RU2186357C2 |
ANNULAR COMBUSTION CHAMBER | 1996 |
|
RU2161756C2 |
LIQUID-PROPELLANT THRUST CHAMBER AND ITS CASING | 1999 |
|
RU2158841C2 |
Authors
Dates
2000-12-27—Published
1999-01-25—Filed