European Facility For Airborne Research Dec. 23, 2024, 19:24
Min speed | 40 m/s |
Max speed | 80 m/s |
Usual speed during measurements | 55 m/s |
Usual speed during transit flights | 65 m/s |
Ascent rate | 6 m/s |
Min altitude |
|
Max ceiling | 20 000 ft |
Usual ceiling during measurements | 15 000 ft |
Ceiling limitations | n/c |
Empty weight | 1 300 kg |
Max take-off weight | 2 100 kg |
Max payload | 800 kg |
Max scientific payload | 100 kg (X-coordinate of 2nd point) |
Usual scientific payload during measurements | 40 kg |
Scientific payload for max endurance | 40 kg (X-coordinate of 1st point) |
Max endurance at min scientific payload and max fuel | 5 h (Y-coordinate of 1st point) |
Endurance at max scientific payload | 5 h (Y-coordinate of 2nd point) |
Max range | 970 km (at min scientific payload and max fuel) |
Conditions for max range |
n/c |
Range at max scientific payload | None km |
Usual range during measurement flight | 450 km |
Weather conditions limitations |
VFR, IFR |
Take-off runway length | 0 m |
Engines | 2 x Continental TSIO-360-EB-L |
Avionics | n/c |
Crew (pilots + operators) |
2 + 2 |
Seats available for scientists | 2 |
Length | n/c m |
Width | n/c m |
Height | n/c m |
Apertures | n/c |
Cabin pressurized | n/c |
More information | n/c |
Nose boom | mobile Flux Platform probe, 9 holes pressure sphere, CO2, H2O, temperature |
Windows | n/c |
Openings | two downward looking openings at centre of aircraft |
Hard points | n/c |
Inlets | n/c |
Additionnal systems | n/c |
n/c
Aircraft total electrical power (kW) | n/c |
Electrical power (kW) and voltages (V) available for scientists | 0.8 kW at 12 VDC |