Modeling of Radiation Heat Transfer in Liquid Rocket Engines
Modeling of Radiation Heat Transfer in Liquid Rocket Engines
Modeling of Radiation Heat Transfer in Liquid Rocket Engines
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Results for a RP1-LO2 Eng<strong>in</strong>eThe specifications <strong>of</strong> this eng<strong>in</strong>e are:Chamber pressure2,000 psiO/F (mixture ratio) 1.8Contraction ratio 3.4Expansion ratio 7.20Throat diameter2.6 <strong>in</strong>chPropellantRP1-LO2CoolantLO2Total coolant flow rate32.893 lb/sCoolant <strong>in</strong>let temperature 160°RCoolant <strong>in</strong>let pressure3,000 psiNumber <strong>of</strong> cool<strong>in</strong>g channels 100Throat region channel aspect ratio 2.5
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