European Facility For Airborne Research Dec. 5, 2025, 07:57
12.7 m
4.7 m
15.88 m
| 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 |