The rate of fuel consumption in a rocket is $40 \ kg/s$. The velocity of the exhaust gases coming out of the rocket is $5 \times 10^4 \ m/s$. What is the thrust force acting on the rocket?
- A$2 \times 10^5 \ N$
- B$2 \times 10^3 \ N$
- C$2 \times 10^6 \ N$
- D$2 \times 10^9 \ N$
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