| Standard Atmospheric Table | ||||
| Altitude (Feet) |
Density of Air (D) |
Altitude (Feet) |
Density of Air (D) |
|
| 0 | 0.002377 | 15,000 | 0.001496 | |
| 1,000 | 0.002308 | 20,000 | 0.001266 | |
| 2,000 | 0.002241 | 25,000 | 0.001065 | |
| 3,000 | 0.002175 | 30,000 | 0.000889 | |
| 4,000 | 0.002111 | 35,000 | 0.000737 | |
| 5,000 | 0.002048 | 36,089* | 0.000706 | |
| 6,000 | 0.001987 | 40,000 | 0.000585 | |
| 7,000 | 0.001927 | 45,000 | 0.000460 | |
| 8,000 | 0.001868 | 50,000 | 0.000362 | |
| 9,000 | 0.001811 | 55,000 | 0.000285 | |
| 10,000 | 0.001755 | *Geopotential of Tropopause | ||
3 Minutes Find the correct air density for the altitude at which they will be flying.HINT: Look at the chart above to determine it. The altitude is 20,000 feet. A) 0.001266B) 0.001496C) 0.001065D) 0.000889 |