Sinus
UL Motorglider
912
ENGINE ROTAX
ROTAX 912 UL
max. horizontal speed
220 km/h
max. power
80 hp at 5800 rpm
manoevring speed
141 km/h
best climb speed
120 km/h
PROPELLER
Pipistrel VARIO
max climb rate (450 kg)
6,5 m/sec
climb rate at 140 km/h
6,3 m/sec
SIZES
min. sink speed
90 km/h
wing span
14,97 m
min sink*
1,03 m/sec
length
6,60 m
best glide ratio speed
95 km/h
height
1,70
best glide*
1:27
wing area
12,26 m²
take off run (450 kg)
88 m
aspect ratio
18,3
take off over 15 m
148 m
positive flaps
9 deg, 18 deg
service ceiling (450 kg)
8100 m
negative flaps
5 deg
45° - 45° roll time
4,2 sec
fuel consum @cruis. speed
9,2 l/hour
WEIGHTS
endurance
5,8 hours
max. Weight (MTOW)
450kg/472,5kg/544kg
range distance
1200 km
fuel tanks capacity
2 x 30 l /2 x 50 l
Max. load factor (x1,8)
+4 g-2 g
Max. load factor tested
+7,2 g -7,2 g
PERFORMANCE
stall with flaps
63 km/h
* (prop. 90 deg)
cruising speed (75%)
200 km/h
Kijk en vergelijk t.o.v. vliegtuigen in dezelfde klasse
