European Facility For Airborne Research Nov. 21, 2024, 12:54
Min speed | 22 m/s |
Max speed | 72 m/s |
Usual speed during measurements | 62 m/s |
Usual speed during transit flights | 62 m/s |
Ascent rate | 0 m/s |
Min altitude |
|
Max ceiling | 25 000 ft |
Usual ceiling during measurements | 15 000 ft |
Ceiling limitations | n/c |
Empty weight | n/c |
Max take-off weight | 5 670 kg |
Max payload | n/c |
Max scientific payload | n/c |
Usual scientific payload during measurements | n/c |
Scientific payload for max endurance | n/c |
Max endurance at min scientific payload and max fuel | n/c |
Endurance at max scientific payload | n/c |
Max range | 0 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 | 0 km |
Weather conditions limitations |
n/c |
Take-off runway length | 0 m |
Engines | 2 x Pratt&Whitney PT6A-20 |
Avionics | n/c |
Crew (pilots + operators) |
1 |
Seats available for scientists | 1 - 4 |
Length | n/c m |
Width | n/c m |
Height | n/c m |
Apertures | n/c |
Cabin pressurized | no |
More information | no |
Nose boom | turbulence measurements |
Windows | n/c |
Openings | roof hatch and camera bay in floor |
Hard points | two wing mounted pylons for PMS pods |
Inlets | 3 Rosemount inlets for chemistry, 1 isokinetic inlet |
Additionnal systems | oxygen system, internal Long Range tank can be fitted |
PC running lab view
Aircraft total electrical power (kW) | 8.4 kW at 28 VDC |
Electrical power (kW) and voltages (V) available for scientists | 4.2 kW at 28 VDC |