model |
VIRUS 912 SW 80 |
VIRUS 912 SW 100 |
ENGINE ROTAX |
ROTAX 912 UL |
ROTAX 912 ULS |
max power(with 2 carb.) |
80 hp at 5800 rpm |
100 hp at 5800 rpm |
PROPELLER |
Pipistrel VARIO |
Variable pitch |
SIZES |
|
|
wing span |
10,71 m |
10,71 m |
length |
6,5 m |
6,5 m |
height |
1,85 |
1,85 |
wing area |
9,51 m2 |
9,51 m2 |
rudder area |
1,1 m2 |
1,1 m2 |
tail area |
1,08 m2 |
1,08 m2 |
aspect ratio |
11,3 |
11,3 |
positive flaps |
9 deg, 19 deg |
9 deg, 19 deg |
negative flaps |
5 deg |
5 deg |
center of gravity |
25% - 37% |
25% - 37% |
WEIGHTS |
|
|
empty weight |
287 kg |
289 kg |
max take off weight (MTOW) |
472.5 / 544 / 600 kg |
472.5 / 544 / 600 kg |
fuel tanks capacity |
2 x 50 l |
2 x 50 l |
useful fuel |
2 x 47 l |
2 x 47 l |
PERFORMANCES |
DATA PUBLISHED FOR TOM 472.5 kg |
stall with flaps |
64 km/h |
64 km/h |
stall without flaps |
79 km/h |
79 km/h |
cruising speed (75% power) |
246 km/h |
273 km/h |
max. horizontal speed |
264 km/h |
283 km/h |
VNE |
302 km/h |
302 km/h |
max speed with airbrakes out |
205 km/h |
205 km/h |
max speed with flaps down |
130 km/h |
130 km/h |
turbulence penetration speed Vb |
250 km/h |
250 km/h |
best climb speed |
140 km/h |
140 km/h |
max climb rate (450 kg) |
6,1 m/sec |
8,4 m/sec |
best glide ratio speed |
118 km/h |
118 km/h |
best glide |
1:17 |
1:15 |
take off run (450 kg) |
140 m |
95 m |
take off over 15 m obstacle |
225 m |
175 m |
service ceiling (450 kg) |
6200 m |
6800 m |
45° - 45° roll time |
1,6 sec |
1,6 sec |
fuel consum. at cruis. speed |
13,6 l/hour |
17,8 l/hour |
endurance |
6,9 hours |
5,3 hours |
range distance |
1650 km |
1450 km |
max load factor permitted ( x 1,8) |
+4g -2g |
+4g -2g |
design safety factors & tested |
minumum 1.875 |
minumum 1.875 |
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