To determine the appropriate mass for the second model rocket to achieve half the acceleration of the first rocket, we can use Newton's second law of motion, which states that \( F = m \cdot a \), where \( F \) is the force applied, \( m \) is the mass, and \( a \) is the acceleration.
For the first rocket:
- Mass \( m_1 = 0.2 , \text{kg} \)
- Force \( F = 100 , \text{N} \)
We can calculate the acceleration \( a_1 \) of the first rocket: \[ a_1 = \frac{F}{m_1} = \frac{100 , \text{N}}{0.2 , \text{kg}} = 500 , \text{m/s}^2 \]
To achieve half the acceleration for the second rocket, the target acceleration \( a_2 \) is: \[ a_2 = \frac{a_1}{2} = \frac{500 , \text{m/s}^2}{2} = 250 , \text{m/s}^2 \]
Now we can rearrange Newton's second law for the second rocket, which has the same force \( F \): \[ a_2 = \frac{F}{m_2} \] Solving for the mass \( m_2 \): \[ m_2 = \frac{F}{a_2} = \frac{100 , \text{N}}{250 , \text{m/s}^2} = 0.4 , \text{kg} \]
Thus, to achieve half the acceleration of the first rocket, the mass of the second rocket should be 0.4 kg.
The correct response is: The mass of the second rocket should be 0.4 kg.