Density altitude is pressure altitude corrected for non-standard temperature, and it is the altitude the aircraft actually behaves as though it is flying at. Three factors thin the air: elevation, heat and humidity. Here two of them are working together — a 2,000-foot field and 95°F, well above the roughly 52°F standard temperature at that elevation — so the density altitude is far higher than the field elevation. Thin air gives the propellers less mass to accelerate, so each rotation produces less thrust, and the motors compensate by drawing more current. The practical consequences for a small unmanned aircraft are reduced climb rate, longer response to control input, shorter endurance and less margin in an aborted descent.