Task id16911
📂 Physics
👤 nerdmavr
Product Description
The speed of exhaust of combustion products from the nozzle of a space rocket is 2.0 km/s, the temperature is 600 °C. Determine the temperature in the combustion chamber and the maximum efficiency. Assume that the fuel burns completely and carbon dioxide flows out of the nozzle.
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Answer. Format gif
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