Answer:
The terminal velocity v_t= 202.96 m/s, approximately 203 m/s.
Explanation:
The formula for terminal velocity is given by

Here, C_d represents the drag coefficient for the cylindrical shape, which is 1.15.
The air's surface density at 20°C is
ρ_surface = 1.2041 kg/m³.
At an altitude of 39,000 m, the air density is calculated as
ρ = 4.3/100 × 39000 = 0.05177 kg/m³.
Substituting these values back into the formula yields

The found terminal velocity v_t is 202.96 m/s, or roughly 203 m/s.