OXYGEN-HYDROGEN LIQUID-PROPELLANT ENGINE Russian patent published in 2013 - IPC F02K9/48 

Abstract RU 2484285 C1

FIELD: engines and pumps.

SUBSTANCE: oxygen-hydrogen liquid-propellant engine containing a combustion chamber having a regenerative cooling system of the nozzle with second fuel, two turbo-pump units, including an oxidiser turbo-pump unit and a fuel turbo-pump unit; at that, all turbo-pump units contain the main turbine, pumps; at that, it additionally includes at least one additional hydrogen turbo-pump unit, hydrogen pumps of all turbo-pump units are connected in series, main turbines of hydrogen turbo-pump units are also connected in series; at that, oxidiser and fuel turbo-pump units have gas generators structurally combined with their turbo-pump units.

EFFECT: improving specific characteristics, reliability and controllability of a liquid-propellant engine.

21 cl, 17 dwg

Similar patents RU2484285C1

Title Year Author Number
OXYGEN-HYDROGEN LIQUID-PROPELLANT ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2484286C1
HYDROGEN-OXYGEN LIQUID PROPELLANT ROCKET ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2474719C1
THREE-COMPONENT LIQUID-PROPELLANT ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2484287C1
THREE-COMPONENT LIQUID-PROPELLANT ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2477809C1
LIQUID PROPELLANT ROCKET ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2476706C1
LIQUID PROPELLANT ROCKET ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2476709C1
LIQUID PROPELLANT ROCKET ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2476708C1
THREE-COMPONENT LIQUID-PROPELLANT ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2481488C1
LIQUID-PROPELLANT ENGINE 2011
  • Bolotin Nikolaj Borisovich
RU2466292C1
LIQUID PROPELLANT ROCKET ENGINE 2014
  • Bolotin Nikolaj Borisovich
  • Dudyshev Valerij Dmitrievich
RU2545613C1

RU 2 484 285 C1

Authors

Bolotin Nikolaj Borisovich

Dates

2013-06-10Published

2011-12-29Filed