| Temperatur ϑ in °C | Temperatur T in K | Luftdichte ρ in kg/m³ | |
|---|---|---|---|
| +35 | 308,15 | 1,1455 | |
| +30 | 303,15 | 1,1644 | |
| +25 | 298,15 | 1,1839 | |
| +20 | 293,15 | 1,2041 | Laborbedingungen |
| +15 | 288,15 | 1,2250 | Luftfahrt-Normatmosphäre |
| +10 | 283,15 | 1,2466 | |
| +5 | 278,15 | 1,2690 | |
| 0 | 273,15 | 1,2922 | physikalische Normbedingungen |
| −5 | 268,15 | 1,3163 | |
| −10 | 263,15 | 1,3413 | |
| −15 | 258,15 | 1,3673 | |
| −20 | 253,15 | 1,3943 | |
| −25 | 248,15 | 1,4224 |