JEE — Thrust ForceHardQuestion 30569
Question
A rocket has initial mass 2000 kg and burns fuel at 10 kg/s with exhaust velocity 3000 m/s. Initial thrust is:
- A6000 N
- B30000 NCorrect
- C20000 N
- D3000000 N
Correct answer
30000 N
Explanation
Thrust = u × (dM/dt) = 3000 × 10 = 30000 N = 30 kN.