The mass of a rocket is 2400 kg. The nozzle of the rocket is designed to give velocity of 200 m/s to the gases produced after combustion of the fuel. If the rocket has to achieve an acceleration of 15 m/s2, what should be the rate of burning of the fuel? (Take g=10 m/s2)

The mass of a rocket is 2400 kg. The nozzle of the rocket is designed

1.	The mass of a rocket is 2400 kg. The nozzle of the rocket is designed to give velocity of 200 m/s to the gases produced after combustion of the fuel. If the rocket has to achieve an acceleration of 15 m/s2, what should be the rate of burning of the fuel? (Take g=10 m/s2)
Answer» The mass of a rocket is $2400 kg$ . The nozzle of the rocket is designed to give velocity of $200 m/s$ to the gases produced after combustion of the fuel. If the rocket has to achieve an acceleration of $15 {m/s}^{2}$ , what should be the rate of burning of the fuel? (Take $g = 10 {m/s}^{2}$ )

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The mass of a rocket is 2400 kg. The nozzle of the rocket is designed to give velocity of 200 m/s to the gases produced after combustion of the fuel. If the rocket has to achieve an acceleration of 15 m/s2, what should be the rate of burning of the fuel? (Take g=10 m/s2)

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