Center of MassHard
Question
If the thrust force on a rocket which is ejecting gases with a relative velocity of 300 m/s, is 210 N. Then the rate of combustion of the fuel will be :
Options
A.10.7 kg/sec
B.0.07 kg/sec
C.1.4 kg/sec
D.0.7 kg/sec
= 0.7 kg/sMore Center of Mass Questions
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