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Answer :
Final answer:
The thrust on the rocket is 430.92 kN (kilonewtons).
Explanation:
To calculate the thrust on the rocket, we can use the formula:
Thrust = Fuel consumption rate * Exhaust velocity
Given that the fuel consumption rate is 114 kg/s and the exhaust velocity is 3780 m/s, we can substitute these values into the formula to get:
Thrust = 114 kg/s * 3780 m/s
= 430,920 N
The thrust on the rocket is 430,920 N, which is equal to 430.92 kN (kilonewtons).
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