Fuel is consumed at the rate of `100 kg s^(-1)` in a rocket. The exhaust gases are ejected at speed of `4.5 xx 10^(4) ms^(-1)`. What is thrust experienced by the rocket?

Fuel is consumed at the rats of 100kg//s in a rocket The exhaust gases are ejected at a speed of 4.5 xx 10^(4) ms^(-1) w.r.t the rocket What is the thrust experienced by the rocket Also calculate velocity of the rocket at the instant when its mass is reduced of rocket to be zero .

Fuel is consumend at the rate of 50 g per second in a rocket. The exhaust gases are rejected at the rate of 5xx10^(5)cms^(-1) . What is the thrust experienced by the rocket?

Fuel is consumed in a rocket at the rate of 200 kg//s . What is the thrust experienced by the roket if exhaust gases are ejected at a speed of 45 km//s ?

In a rocket of mass 1000 kg fuel is consumed at a rate of 40 kg/s . The velocity of the gases ejected from the rocket is 5xx10^(4)m//s . The thrust on the rocket is

A rocket motor consumes 100 kg of fuel per second exhausting it with a speed of 6 xx 10^(3) ms^(-1) What thrust is exerted on the rocket ? What will be the velocity of the rocket at the instant its mass is reduced to (1 // 40) of its initial mass ? Take initial velocity of rocket as zero . Neglect gravity .

A Diwali rocket is ejecting 5 gram of gases/second at a velocity of 4m/s. What is the accelerating force acting on the rocket?

What is the thrust of a rocket that bums fuel at a rate of 1.3 X10^(4) kg/sec if the exhaust gases have a velocity 2.5 x10^(3) m/s with respect to the rocket.

The rate of burning of fuel in a rocket is 50 gm/sec. and comes out with and velocity 4 xx 10^(3) m/s. The force exerted by gas on rocket will be -

A rocket motor consumes 100 kg of fuel per second, exhausting it with a speed of 5xx10^(3)ms^(-1) . (i) What force is exerted on the rocket ? (ii) What will be the velocity of the rocket at the instant its mass is reduced (1//20) th of its initial mass, its initial velocity being zero. Neglect gravity.