European Facility For Airborne Research Oct. 16, 2024, 07:28
Min speed | 0 m/s |
Max speed | 93 m/s |
Usual speed during measurements | 0 m/s |
Usual speed during transit flights | 0 m/s |
Ascent rate | 0 m/s |
Min altitude |
|
Max ceiling | 30 000 ft |
Usual ceiling during measurements | 20 000 ft |
Ceiling limitations | oxigen |
Empty weight | 640 kg |
Max take-off weight | 1 050 kg |
Max payload | 410 kg |
Max scientific payload | 250 kg (X-coordinate of 2nd point) |
Usual scientific payload during measurements | n/c |
Scientific payload for max endurance | n/c |
Max endurance at min scientific payload and max fuel | 10 h (Y-coordinate of 1st point) |
Endurance at max scientific payload | n/c |
Max range | 1 800 km (at min scientific payload and max fuel) |
Conditions for max range |
min scientific payload and max fuel |
Range at max scientific payload | None km |
Usual range during measurement flight | 0 km |
Weather conditions limitations |
n/a |
Take-off runway length | 0 m |
Engines | 1 x Rotax 914F |
Avionics | 1x Air Speed Indicator(Beleuchtet)-United |
Crew (pilots + operators) |
1 - 2 |
Seats available for scientists | n/a |
Length | 1.50 m |
Width | 1.10 m |
Height | 1.10 m |
Apertures | n/a |
Cabin pressurized | no |
More information | no |
Nose boom | no |
Windows | no |
Openings | no |
Hard points | hard points for payload under inner wing module. |
Inlets | no |
Additionnal systems | external & internal payload container. |
n/c
Aircraft total electrical power (kW) | 1.0 kW at 14 VDC ; battery 24 Amp / 12 VDC, |
Electrical power (kW) and voltages (V) available for scientists | 1.5 kW at 28 VDC ; 24 Amp / 24 VDC buffer battery system. |