A rocket has a mass of 13600kg when Feuled on the launching pad. It is fired vertically upward and burned out and consume 9100 kg gases. Gases are emitted at the rate of 146kg per second. What is the upward thrust. What would be the speed of rocket at this burn out with or without gravity consideration?
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it is very easy question 13600 its upon to the launching period and 9100 kg gas the gas is limited to the rate of 146 case edge and a per second to what it's upon 13600 Upon In 9100 that the equation is that the equation is one upon 46 approx it is made
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