LOW-THRUST LIQUID-PROPELLANT ROCKET ENGINE COMBUSTION CHAMBER Russian patent published in 2012 - IPC F02K9/52 

Abstract RU 2453722 C2

FIELD: machine building.

SUBSTANCE: proposed combustion chamber comprises mixing head with oxidiser and propellant jet nozzles communicated with aft-of-valve chambers and having extra chambers in combustion chamber walls or inside. In compliance with this invention, said extra chambers are made up of loop channels with jet nozzles at outlet extending to wedge-type mixer surface. Said loop channels may be made up of capillary tubes arranged inside combustion chamber while wedge-type mixer may represent a cone.

EFFECT: higher operating performances.

3 cl, 1 dwg

Similar patents RU2453722C2

Title Year Author Number
LOW-THRUST LIQUID-PROPELLANT ENGINE COMBUSTION CHAMBER 2017
  • Andreev Yurij Zakharovich
RU2716778C2
COMBUSTION CHAMBER OF LOW-THRUST LIQUID-PROPELLANT ENGINE 2016
  • Andreev Yurij Zakharovich
RU2685166C2
LOW-THRUST LIQUID-PROPELLANT ROCKET ENGINE COMBUSTION CHAMBER 2013
  • Andreev Jurij Zakharovich
RU2572261C2
CHAMBER OF LIQUID-PROPELLANT THRUSTER 2004
  • Andreev Jurij Zakharovich
RU2288370C2
COMBUSTION CHAMBER OF LOW-THRUST LIQUID-PROPELLANT ENGINE 2012
  • Andreev Jurij Zakharovich
RU2558489C2
CHAMBER OF LIQUID PROPELLANT LOW-THRUST ROCKET ENGINE 1999
  • Ivanov V.N.
RU2217620C2
CHAMBER OF LIQUID PROPELLANT THRUSTER 2000
  • Kazankin F.A.
  • Kutuev R.Kh.
  • Larin E.G.
  • Mezenin P.B.
RU2192555C2
LOW-THRUST LIQUID-PROPELLANT ENGINE CHAMBER 2013
  • Evseev Alekandr Vasilevich
  • Andreev Jurij Zakharovich
RU2581756C2
MIXING HEAD 2009
  • Andreev Jurij Zakharovich
RU2463469C2
LOW-THRUST LIQUID ROCKET ENGINE 2019
  • Kutuev Rashit Khurmatovich
RU2755862C2

RU 2 453 722 C2

Authors

Andreev Jurij Zakharovich

Dates

2012-06-20Published

2009-10-14Filed