Question
For a Rocket propulsion velocity of exhaust gases relative to rocket is 2 km/s. If mass of rocket system is 1000 kg, then the rate of fuel consumption for a rocket to rise up with an acceleration 4.9 m/s^2 will be:-
1) 12.25 kg/s
2) 17.5 kg/s
3) 7.35 kg/s
4) 5.2 kg/s