1.

An ideal rocket has a chamber pressure of 1 MPa and a temperature of 1600 K. Determine the density of the combustion product if its molecular mass is 24 kg/kmol.

A. 1.2 kg/m<sup>3</sup>
B. 2.4 kg/m<sup>3</sup>
C. 1.8 kg/m<sup>3</sup>
D. 3.6 kg/m<sup>3</sup>
Answer» D. 3.6 kg/m<sup>3</sup>


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