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A model rocket engine has an average thrust of 5.26 N. It has an initial mass of 25.5 g, which includes a fuel mass of 12.7 g. The duration of its burn is 1.90 s. (a) What is the average exhaust speed of the engine? (b) This engine is placed in a rocket body of mass 53.5 g. What is the final velocity of the rocket if it were to be fired from rest in outer space by an astronaut on a space-walk? Assume the fuel burns at a constant rate.

 

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Priyanka
PriyankaLv10
27 Nov 2020

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