European Facility For Airborne Research Dec. 5, 2025, 07:59
8.7 m
3.0 m
11.9 m
| Min speed | 32 m/s |
| Max speed | 99 m/s |
| Usual speed during measurements | 40 m/s |
| Usual speed during transit flights | 80 m/s |
| Ascent rate | 6 m/s |
| Min altitude |
|
| Max ceiling | 25 000 ft |
| Usual ceiling during measurements | 3 000 ft |
| Ceiling limitations | n/c |
| Empty weight | 1 264 kg |
| Max take-off weight | 2 073 kg |
| Max payload | 809 kg |
| Max scientific payload | 300 kg (X-coordinate of 2nd point) |
| Usual scientific payload during measurements | 50 kg |
| Scientific payload for max endurance | 150 kg (X-coordinate of 1st point) |
| Max endurance at min scientific payload and max fuel | 8 h (Y-coordinate of 1st point) |
| Endurance at max scientific payload | 2 h (Y-coordinate of 2nd point) |
| Max range | 1 811 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 | 1 400 km |
| Weather conditions limitations |
VFR, IFR, de-icing |
| Take-off runway length | 0 m |
| Engines | 2 x Continental TSIO-360-EB-L |
| Avionics | 2 X GARMIN 428 |
| Crew (pilots + operators) |
1 |
| Seats available for scientists | 5 |
| Length | 3.15 m |
| Width | 1.23 m |
| Height | 10.6 m |
| Apertures | 1 door on the right side for cockpit |
| Cabin pressurized | no |
| More information | portable oxygen with four masks available |
| Nose boom | no |
| Windows | no |
| Openings | Hatch: W0.20 m x L0.60 m on the rear bottom of the fuselage |
| Hard points | no |
| Inlets | air inlet via supplementary pitot tube |
| Additionnal systems |
n/c
| Aircraft total electrical power (kW) | 2.5 kW |
| Electrical power (kW) and voltages (V) available for scientists | 24 volts 30 Amps ; 12 volts 10 Amps |