European Facility For Airborne Research Dec. 23, 2024, 17:41
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 |