A rocket with a mass of 2.0 × 106 kg is designed to take off from the surface of the earth by burning fuel and ejecting it with an exhaust speed of 3500 m/s

What is the minimum rate at which the fuel should be consumed in order to attain liftoff? A)

5.6 × 103 kg/s
B)

1.4 × 103 kg/s
C)

1.8 × 103 kg/s
D)

2.8 × 103 kg/s
E)

18 × 103 kg/s


A

Physics & Space Science

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