NOTE: This is a multi-part question. Once an answer is submitted, you will be unable to return to this part. A radar system is used to track a new experimental space launch vehicle. Early in the vehicle’s flight trajectory, the azimuth angle β is increasing with the constant rate dβ/dt = 20°/s. The elevation angle γ is increasing at the rate dγ/dt = 40°/s, and this rate is increasing at 5°/s2. Know that the distance between O and P is 2 m and that at this instant β = 0° and γ = 30°.