If the force on a rocket moving with a velocity of 300 m/s is 210 N, then the rate of combustion of the fuel is
0.7 kg/s
1.4 kg/s
0.07 kg/s
10.7 kg/s
Force on the rocket =udmdt∴ Rate of combustion of fuel (dmdt)=Fu=210300=0.7kg/s