RU93036173A - METHOD OF PROVIDING SUSTAINABLE COMBUSTION IN A LIQUID ROCKET ENGINE - Google Patents
METHOD OF PROVIDING SUSTAINABLE COMBUSTION IN A LIQUID ROCKET ENGINEInfo
- Publication number
- RU93036173A RU93036173A RU93036173/06A RU93036173A RU93036173A RU 93036173 A RU93036173 A RU 93036173A RU 93036173/06 A RU93036173/06 A RU 93036173/06A RU 93036173 A RU93036173 A RU 93036173A RU 93036173 A RU93036173 A RU 93036173A
- Authority
- RU
- Russia
- Prior art keywords
- nozzles
- gas
- rocket engine
- liquid rocket
- installing
- Prior art date
Links
- 238000002485 combustion reaction Methods 0.000 title claims 3
- 239000007788 liquid Substances 0.000 title claims 2
- 230000000903 blocking Effects 0.000 claims 1
- 239000000446 fuel Substances 0.000 claims 1
- 238000000034 method Methods 0.000 claims 1
- 239000000203 mixture Substances 0.000 claims 1
- 230000001264 neutralization Effects 0.000 claims 1
Claims (1)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU93036173A RU2065069C1 (en) | 1993-07-13 | 1993-07-13 | Method of ensuring stable combustion in liquid-propellant rocket engine |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
RU93036173A RU2065069C1 (en) | 1993-07-13 | 1993-07-13 | Method of ensuring stable combustion in liquid-propellant rocket engine |
Publications (2)
Publication Number | Publication Date |
---|---|
RU93036173A true RU93036173A (en) | 1996-07-27 |
RU2065069C1 RU2065069C1 (en) | 1996-08-10 |
Family
ID=20144997
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
RU93036173A RU2065069C1 (en) | 1993-07-13 | 1993-07-13 | Method of ensuring stable combustion in liquid-propellant rocket engine |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU2065069C1 (en) |
Families Citing this family (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2477383C1 (en) * | 2011-10-18 | 2013-03-10 | Государственный научный центр Российской Федерации - федеральное государственное унитарное предприятие "Исследовательский Центр имени М.В. Келдыша" | Method of low-thrust rocket engine chamber operation |
RU2571997C1 (en) * | 2014-07-14 | 2015-12-27 | Федеральное государственное бюджетное образовательное учреждение высшего профессионального образования "Воронежский государственный технический университет" | Method of fuel components feed in liquid propellant rocket engine combustion chamber |
CN107939551B (en) * | 2017-11-29 | 2024-02-09 | 北京航天动力研究所 | Pre-combustion chamber injector structure |
-
1993
- 1993-07-13 RU RU93036173A patent/RU2065069C1/en active
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP0625673A3 (en) | Premixing burner for operating an internal combustion engine, a combustion chamber of a gas turbo group or a combustion plant. | |
DE60213085D1 (en) | REACTOR FOR THE DECOMPOSITION OF LIQUID MONERGOL FUELS ON AMMONIUM DINITIRID BASE AND DECOMPOSITION PROCESS | |
KR920020069A (en) | Pilot and main fuel injection methods for diesel engines | |
RU93036173A (en) | METHOD OF PROVIDING SUSTAINABLE COMBUSTION IN A LIQUID ROCKET ENGINE | |
WO1995018336A1 (en) | Ignitor plug guide for a gas turbine engine combustor | |
CA2394694A1 (en) | Pilot nozzle of gas turbine combustor | |
BR9805618A (en) | Apparatus for use with a liquid-fueled combustor | |
KR960705135A (en) | METHOD OF OPERATING A GAS TURBINE USING AN ADDITIVE FEED | |
US5115637A (en) | External cartridge gas combustor ignitor | |
CA2335019A1 (en) | A method for starting a combustion device | |
RU2065069C1 (en) | Method of ensuring stable combustion in liquid-propellant rocket engine | |
US9347399B1 (en) | Laser ignition for liquid propellant rocket engine injectors | |
RU1813900C (en) | Method of implementing working process in combustion chamber of air-jet engine | |
JPS5435424A (en) | Vaporizing liquid fuel combustion device | |
SU106500A1 (en) | Wave valveless pulsating jet engine | |
RU2131053C1 (en) | Solid propellant charge for dual thrust rocket engine | |
SU928869A2 (en) | Afterburner of by-pass turbojet engine | |
SU985391A1 (en) | Device for starting i.c.engine | |
SU1548605A1 (en) | Method of igniting a double-component liquid fuel | |
RU2103610C1 (en) | Igniter | |
GB1123921A (en) | Improvements in and relating to gas turbine engines | |
SU1195135A1 (en) | Burner for burning liquid fuel | |
JPS5640027A (en) | Combustor for gas turbine | |
RU2055092C1 (en) | Energotechnological plant | |
JPS5614839A (en) | Solid propellant rocket motor |