A mixture of combustion products of hydrocarbon fuel and a LOX oxidizer contains 10kg of carbon monoxide CO(mCO=10kg),6.75kg of carbon dioxide CO2(mCO2=6.75kg),0.25kg of molecular hydrogen H2(mH2=0.25kg),6kg of H2O(mH2O=6.0kg), and 1kg of OH(mOH=1.0kg) at a temperature typical for conditions in combustion chambers of highperforming rocket engines. At this temperature specific heat ratios of H2O and OH are 120=1.175 and OH=1.29, respectively; specific heats for CO,CO2, and H2 are cp,Co=37.0kJ/(kmolK),cp,CO2=62.0kJ/(kmolK), and cp,H2=37.0kJ/(kmolK), respectively. Assume the constituents are perfect gases; assume the following atomic weights: MH=1;MC=12 ; and M0=16. Calculate the molecular weight MM, specific heats cp,M and cv,M, and specific heat ratio M of the mixture