Question
In a rocket of mass 1000 kg fuel is consumed at a rate of 40 kg/s. The velocity of the gases ejected from the rocket is 5×104 m/s. The thrust on the rocket is
Answer: Option C
:
C
Thrust on the rocket F=udmdt=5×104(40)=2×106N
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:
C
Thrust on the rocket F=udmdt=5×104(40)=2×106N
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