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[" For a Rocket "9" mould ion velocity o...

[" For a Rocket "9" mould ion velocity of exhays fgases relative "],[" to rocketis "2" kms .If mass of rocket system is "1000kg" ,"M],[" then the rate of fuel consumption for a rocket to rise "],[" up with an acceleration "4.9m/s^(2)" will be : Fthement - "]

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For a Rocket propulsion velocity of exhaust gases relative to rocket is 2km/s. If mass of rocket system is 1000 kg, then the rate of fuel consumption for a rockt to rise up with acceleration 4.9 m//s^(2) will be:-

For a Rocket propulsion velocity of exhaust gases relative to rocket is 2km/s. If mass of rocket system is 1000 kg, then the rate of fuel consumption for a rockt to rise up with acceleration 4.9 m//s^(2) will be:-

For a Rocket propulsion velocity of exhaust gases relative to rocket is 2km/s. If mass of rocket system is 1000 kg, then the rate of fuel consumption for a rockt to rise up with acceleration 4.9 m//s^(2) will be:-

The exhaust velocity of gases with respect to a small rocket of mass 25 kg. is 28xx10^(2)m//s . At what rate the fuel must burn so that it may rise up with an acceleration of 9.8 m//s^(2) ?

The exhaust velocity of gases with respect to a small rocket of mass 25 kg. is 28xx10^(2)m//s . At what rate the fuel must burn so that it may rise up with an acceleration of 9.8 m//s^(2) ?

The exhaust velocity of gases with respect to a small rocket of mass 25 kg. is 28xx10^(2)m//s . At what rate the fuel must burn so that it may rise up with an acceleration of 9.8 m//s^(2) ?

A rocket is set for a vertical firing . If the exhaust speed is 2000 m//s , find the rate of fuel consumption initial vertical upward acceleration of 30 m//s^(2) . Take mass of rocket = 6000 kg .

The force on a rocket moving with a veloctiy 300 m/s is 210N. The rate of consumption of fuel of rocket is

The force on a rocket moving with a veloctiy 300 m/s is 210N. The rate of consumption of fuel of rocket is

The force on a rocket moving with a veloctiy 300 m/s is 210N. The rate of consumption of fuel of rocket is