A 600 kg rocket is set for a vertical firing.if the exhaust speed is 1000 m/s. Then calculate the mass of gas ejected per second to supply the thrust needed to overcome the weight of rocket.
please please give the answer in handwritten if possible.please
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F = mg = V dm/dt
dm/dt = mg/v
600 * 9.8/ 1000 = 58.6 kg/s
= 58.6 kg/s
hence, this is the answer.
hope it helps.
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