if the maximum possible exhaustion velocity of a rocket be 2km/sec, calculate the ratio m0/m for it to acquire a velocity of 11.2km/sec after starting from rest.
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rocket be 2km//s calculate the ratio m_(0)//m for it to acquire a veocity of 11.2km//s after starting from rest . m0m=270.4 . Here, u=2km/s,υ=11.2km/s,(m0m)= ? m0m=antilog2.432=270.4
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If the maximum possible exhaust velocity of a rocket be 2km//s calculate the ratio m_(0)//m for it to acquire a veocity of 11.2km//s after starting from rest . m0m=270.4 . Here, u=2km/s,υ=11.2km/s,(m0m)= ? m0m=antilog2.432=270.4 .
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