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A rocket has total mass 1000 kg with fuel of 900 kg. It ejects fuel at the rate of 1 kg/s with an exhaust velocity of 2 km/s relative to rocket. The maximum velocity attained by rocket is 

a
2.3 km/s
b
4.6 km/s
c
2 km/s
d
4.6log10⁡109km/s

detailed solution

Correct option is B

Final speed, vb=2.303ulog⁡m0mc=2.303×2km/s×log⁡10001000−900=4.6km/s.    (log10 10 = 1)

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