European Facility For Airborne Research Dec. 3, 2024, 18:33
Min speed | 41 m/s |
Max speed | 95 m/s |
Usual speed during measurements | 57 m/s |
Usual speed during transit flights | 82 m/s |
Ascent rate | 4 m/s |
Min altitude |
|
Max ceiling | 25 000 ft |
Usual ceiling during measurements | 10 000 ft |
Ceiling limitations | payload weight |
Empty weight | 2 779 kg |
Max take-off weight | 4 375 kg |
Max payload | 1 595 kg |
Max scientific payload | 1 045 kg (X-coordinate of 2nd point) |
Usual scientific payload during measurements | 250 kg |
Scientific payload for max endurance | 275 kg (X-coordinate of 1st point) |
Max endurance at min scientific payload and max fuel | 7 h (Y-coordinate of 1st point) |
Endurance at max scientific payload | 2 h (Y-coordinate of 2nd point) |
Max range | 1 806 km (at min scientific payload and max fuel) |
Conditions for max range |
At FL100, max fuel, 77 m/s |
Range at max scientific payload | None km |
Usual range during measurement flight | 1 222 km |
Weather conditions limitations |
no flight if severe icing conditions |
Take-off runway length | 750 m |
Engines | 1 x Pratt&Whitney PT6A 114A |
Avionics | n/c |
Crew (pilots + operators) |
1 + 1 |
Seats available for scientists | 3 |
Length | 6.50 m |
Width | 1.60 m |
Height | 1.40 m |
Apertures | cargo door: W1.27 m x H1.24 m ; 2 x pilot door ; 1 x passenger door |
Cabin pressurized | no |
More information | no |
Nose boom | no |
Windows | no |
Openings | 2 x W0.63 m x H0.66 m |
Hard points | no |
Inlets | no |
Additionnal systems | 2 x GPS antenna and irradiance sensor on the upper side of the fuselage |
2 x POS/AV, computer and a fast external hard drive for storage
Aircraft total electrical power (kW) | 8.4 kW |
Electrical power (kW) and voltages (V) available for scientists | 4.2 kW at 28 VDC |