Answer:
C = 1.01
Step-by-step explanation:
Given that,
Mass, m = 75 kg
The terminal velocity of the mass,

Area of cross section,

We need to find the drag coefficient. At terminal velocity, the weight is balanced by the drag on the object. So,
Weight of the object = drag force
R = W
or

Where
is the density of air = 1.225 kg/m³
C is drag coefficient
So,

So, the drag coefficient is 1.01.