European Facility For Airborne Research Dec. 22, 2024, 12:09
Min speed | 50 m/s |
Max speed | 70 m/s |
Usual speed during measurements | 55 m/s |
Usual speed during transit flights | 70 m/s |
Ascent rate | 2 m/s |
Min altitude |
|
Max ceiling | 19 586 ft |
Usual ceiling during measurements | 11 500 ft |
Ceiling limitations | some instruments are limited to 10000 ft or below |
Empty weight | 1 266 kg |
Max take-off weight | 2 122 kg |
Max payload | 856 kg |
Max scientific payload | 400 kg (X-coordinate of 2nd point) |
Usual scientific payload during measurements | 300 kg |
Scientific payload for max endurance | n/c |
Max endurance at min scientific payload and max fuel | 4 h (Y-coordinate of 1st point) |
Endurance at max scientific payload | 4 h (Y-coordinate of 2nd point) |
Max range | 800 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 | 800 km |
Weather conditions limitations |
IFR non icing, VFR |
Take-off runway length | 600 m |
Engines | 1 x TSIO-520-M 310PS |
Avionics | SM2000, GSM3000 stabilized Platforms |
Crew (pilots + operators) |
3 |
Seats available for scientists | 2 |
Length | 4.32 m |
Width | 0.94 m |
Height | 1.22 m |
Apertures | n/c |
Cabin pressurized | no |
More information | no |
Nose boom | n/c |
Windows | n/c |
Openings | 1 x W0.49 m x H0.55 m |
Hard points | n/c |
Inlets | wing air inlet |
Additionnal systems | no |
CDAS
Aircraft total electrical power (kW) | 28 VDC 95A |
Electrical power (kW) and voltages (V) available for scientists | 28 VDC 80A, 230 VAC 1kW |