Final answer:
The initial mass of the rocket was 2400 kg.
Step-by-step explanation:
To solve this problem, we can use the principle of conservation of momentum. The change in momentum of the rocket is equal to the momentum imparted to the exhaust gases. The initial momentum of the rocket is zero because it starts from rest, and the final momentum is the mass of the rocket multiplied by its final velocity. The change in momentum of the gases is the mass of the fuel burned multiplied by the exhaust speed. Equating these two expressions and solving for the initial mass of the rocket:
Initial momentum of rocket = Final momentum of rocket
0 = (mass of rocket + mass of fuel burned) × final velocity of rocket - mass of fuel burned × exhaust speed
Simplifying this equation:
Initial mass of rocket = mass of fuel burned × (exhaust speed - final velocity of rocket) / final velocity of rocket
Substituting the given values:
Initial mass of rocket = 100 kg × (1500 m/s - 100 m/s) / 100 m/s = 2400 kg
Therefore, the initial mass of the rocket was 2400 kg.