European Facility For Airborne Research Dec. 22, 2024, 22:09
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 |