European Facility For Airborne Research Dec. 5, 2025, 07:57
7.6 m
2.56 m
9.68 m
| Min speed | 25 m/s |
| Max speed | 55 m/s |
| Usual speed during measurements | 40 m/s |
| Usual speed during transit flights | 45 m/s |
| Ascent rate | 4 m/s |
| Min altitude |
|
| Max ceiling | 12 000 ft |
| Usual ceiling during measurements | 9 000 ft |
| Ceiling limitations | n/c |
| Empty weight | 400 kg |
| Max take-off weight | 650 kg |
| Max payload | 250 kg |
| Max scientific payload | 80 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 | 4 h (Y-coordinate of 1st point) |
| Endurance at max scientific payload | 4 h (Y-coordinate of 2nd point) |
| Max range | 500 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 | 300 km |
| Weather conditions limitations |
VFR |
| Take-off runway length | 600 m |
| Engines | 1 x Rotax 912 S |
| Avionics | n/c |
| Crew (pilots + operators) |
1 |
| Seats available for scientists | 1 |
| Length | n/c m |
| Width | n/c m |
| Height | n/c m |
| Apertures | n/c |
| Cabin pressurized | no |
| More information | 2 seats in tandem ; downward looking instruments installed in the cabin |
| Nose boom | certified probe for 3D wind pressure sphere, open path CO2 and H2O IRGA mounting, fast tamperature mounting |
| Windows | no |
| Openings | two openings on the bottom for remote sensing downward looking instrumentation |
| Hard points | no |
| Inlets | no |
| Additionnal systems | no |
industrial PC, power distribution system
| Aircraft total electrical power (kW) | 0.9 kW |
| Electrical power (kW) and voltages (V) available for scientists | 0.25 kW at 12 VDC |