|
|
Wing span :
|
14.35 m (47.1 ft), optional extension to 15 m
|
|
Length overall
:
|
5.35 m (17.6 ft)
|
|
Height overall
:
|
1.95 m (6.4 ft)
|
|
Propeller
diameter :
|
1.60 m (5.3 ft)
|
|
Wing area :
|
21.30 m2 (229.3 sq ft)
|
|
Aspect ratio :
|
9.44:1
|
|
Weight empty :
|
FAI ultralight version
: 265 kg
(573 lb)
experimental version : 290
kg (639
lb)
|
|
Max T-O weight
:
|
FAI ultralight
version : 450 kg
(992 lb)
experimental version : 510
kg (1124
lb)
|
|
Max wing
loading :
|
FAI ultralight
version : 21.12 kg/m2 (4.33 lb/sq ft)
experimental version : 23.94 kg/m2 (4.90 lb/sq ft)
|
Performance
of the prototype, powered by a 503, at maximum take-off weight
|
Cruising speed
at 75% power :
|
130 km/h (70 kt, 81 mph)
|
|
Max speed :
|
180 km/h ( 97 kt, 112 mph)
|
|
Stalling speed
:
|
60 km/h (33 kt, 38 mph)
|
|
Max rate of
climb :
|
180 m/mn (590
ft/mn)
|
|
T-O run :
|
100 m (328 ft)
|
|
Landing run :
|
150 m (492 ft)
|
|
Best glide
ratio :
|
with a fixed propeller
: more than 20:1
with a folding propeller :
24:1 (14.35 m
version)
26:1 (15 m version + winglets)
|
|
Min rate of
sink :
|
less than 1.00 m/s
(3.28 ft/s) with a fixed propeller
|
|
G limits
|
+ 8 / -4 G
|
|
