To find the maximum height of the rocket, we can use the following kinematic equation for vertical motion:
\[
v_y^2 = v_{0y}^2 - 2g h
\]
Where:
- \( v_y \) is the final vertical velocity (0 m/s at the maximum height),
- \( v_{0y} \) is the initial vertical velocity,
- \( g \) is the acceleration due to gravity (approximately \( 9.81 , \text{m/s}^2 \)),
- \( h \) is the maximum height.
First, we need to calculate the initial vertical velocity \( v_{0y} \):
\[
v_{0y} = v \sin(\theta)
\]
Where:
- \( v = 26 , \text{m/s} \) (the launch speed),
- \( \theta = 15° \).
Calculating \( v_{0y} \):
\[
v_{0y} = 26 \sin(15°) \approx 26 \times 0.2588 \approx 6.728 , \text{m/s}
\]
Now we can substitute \( v_y = 0 \), \( v_{0y} \approx 6.728 , \text{m/s} \), and \( g = 9.81 , \text{m/s}^2 \) into the kinematic equation:
\[
0 = (6.728)^2 - 2(9.81)h
\]
Solving for \( h \):
\[
0 = 45.229 - 19.62h
\]
\[
19.62h = 45.229
\]
\[
h = \frac{45.229}{19.62} \approx 2.31 , \text{m}
\]
Thus, the maximum height the rocket reaches is approximately \( 2.3 , \text{m} \).
The correct answer is:
c) 2.3 m