Question: A rocket motor is operating steadily, as shown in Fig. P3.34. The products of combustion flowing out the exhaust nozzle approximate a perfect gas with
Liquid oxygen 1 5 lbf/ 1100 F D, 5.5in 4000-R. 400 Ibf/n2- GLiquid fuel o.l slugis
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Exit gas Molecular weight 28 thus Rgas 4970028 1775 ft2s... View full answer
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