$$ P = P_0 * e^{(-gh/RT)}$$
where:
- P is the pressure at the given altitude (in Pascals)
- P0 is the pressure at sea level (in Pascals)
- g is the acceleration due to gravity (approximately 9.81 m/s²)
- h is the altitude above sea level (in meters)
- R is the gas constant for air (approximately 287 J/kg-K)
- T is the air temperature (in Kelvin)
Let's assume the following values for Key West:
- P0 = 101325 Pa (standard atmospheric pressure)
- h1 = 8000 m (altitude at 8 km)
- h2 = 10000 m (altitude at 10 km)
- T = 298 K (approximately 25°C)
Plugging these values into the formula, we can calculate the pressure at 8 km:
$$ P_1 = 101325 * e^{(-9.81 * 8000 / (287 * 298)}$$
$$ P_1 = 50247 Pa $$
Now, we can calculate the pressure at 10 km:
$$ P_2 = 101325 * e^{(-9.81 * 10000 / (287 * 298)}$$
$$ P_2 = 34865 Pa$$
Finally, we can calculate the pressure drop by subtracting the pressure at 10 km from the pressure at 8 km:
$$ \Delta P = P_1 - P_2 $$
$$ \Delta P = 50247 - 34865 = 15382 Pa $$
Therefore, the pressure drop when moving from 8 km to 10 km at Key West is approximately 15382 Pa or 15.382 kPa.