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Questions  

If force on a rocket having exhaust velocity of 300 m/sec is 210 N, then rate of combustion of the fuel is

a
0.7kg/s
b
1.4kg/s
c
0.07kg/s
d
10.7kg/s

detailed solution

Correct option is A

F=udmdt⇒dmdt=Fu=210300=0.7kg/s.

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