According to Newton's second law of motion, F = ma, where F is the force, m is the mass, and a is the acceleration.
For the first rocket:
F = 100 N
m = 0.8 kg
a= F / m = 100 N / 0.8 kg = 125 m/s^2
For the second rocket:
F = 100 N
a= 1/2 * 125 m/s^2 = 62.5 m/s^2
Let's assume the mass of the second rocket is m2.
F = 100 N
m = m2
a = 62.5 m/s^2
Using the equation F = ma, we can solve for m2:
100 N = m2 * 62.5 m/s^2
Divide both sides by 62.5 m/s^2:
100 N / 62.5 m/s^2 = m2
m2 = 1.6 kg
So, the mass of the second rocket is 1.6 kg.
A rocket has a mass of 0.8 kg and an engine that provides 100 N of force. A second rocket is being designed to use the same engine but accelerate at half the rate of the first rocket. What is the mass of the second rocket?
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