FIELD: engines and pumps.
SUBSTANCE: proposed engine comprises oxidiser and fuel pumps, turbine to drive said pumps, chamber with cooling circuit with its outlet communicated with turbine inlet. In compliance with proposed invention, cooling circuit inlet communicates with oxidiser pump outlet, while chamber cooling circuit outlet accommodates temperature gauge connected with engine control system. Chamber cooling circuit, in contact with oxidiser, is made from copper alloys. Filter made from copper alloys is arranged at chamber cooling circuit inlet.
EFFECT: simplified design, reduced operating costs and expanded range of applicable fuels.
3 cl, 1 dwg
Title | Year | Author | Number |
---|---|---|---|
LIQUID PROPELLANT ROCKET ENGINE | 2014 |
|
RU2551713C1 |
LIQUID PROPELLANT ROCKET ENGINE | 2011 |
|
RU2450153C1 |
LIQUID PROPELLANT ROCKET ENGINE | 2013 |
|
RU2514466C1 |
LIQUID PROPELLANT JET ENGINE | 2007 |
|
RU2352804C1 |
LIQUID PROPELLANT ROCKET ENGINE | 2014 |
|
RU2544684C1 |
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF FUEL AND OXYGEN OXIDIZER AND LIQUID-PROPELLANT ROCKET ENGINE FOR IMPLEMENTING SAID METHOD | 2001 |
|
RU2197629C2 |
LIQUID-PROPELLANT ENGINE | 2015 |
|
RU2579295C1 |
METHOD OF OPERATION OF LIQUID-PROPELLANT ROCKET ENGINE WITH TURBOPUMP DELIVERY OF CRYOGENIC PROPELLANT ON BASIS OF OXYGEN OXIDIZER AND HYDROCARBON FUEL AND LIQUID- PROPELLANT ROCKET ENGINE IMPLEMENTING SAID METHOD | 2001 |
|
RU2197628C2 |
METHOD OF LIQUID PROPELLANT ROCKET ENGINE BOOSTING BY THRUST AND LIQUID PROPELLANT ROCKET ENGINE | 2013 |
|
RU2532454C1 |
METHOD OF AUGMENTING LIQUID-PROPELLANT ROCKET ENGINE THRUST AND LIQUID-PROPELLANT ROCKET ENGINE | 2011 |
|
RU2451202C1 |
Authors
Dates
2010-08-10—Published
2009-01-22—Filed