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Song-Up Ha
Song-Up Ha
Thrust
Kerosene
Heat flux
Hydrogen peroxide
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ANALYSIS OF NONSTATIONARY THERMAL STATE OF LOW-THRUST LIQUID ROCKET ENGINE WITH HIGH-CONCENTRATION HYDROGEN PEROXIDE AND KEROSENE PROPELLANT WITH FILM COOLING.
2014
VESTNIK of the Samara State Aerospace University
A.G. Vorobiev
I.N. Borovik
Song-Up Ha
Russian Federation
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