 
S 8 - Performance and Dimensions
|
S 8 |
S 8-RT |
MTOW |
850 kg |
850 kg |
empty weight |
614 kg |
630 kg |
total payload |
236 kg |
220 kg |
Bombardier-Rotax engine 4 cyl.
4 stroke |
912 S |
914 F |
MTOP |
100 hp |
115 hp |
MCP |
94 hp |
100 hp |
fuel capacity standard |
70 L |
70 L |
| fuel capacity long range
|
140 L |
140 L |
wing span |
18,00 m |
18,00 m |
wing span folded |
7,20 m |
7,20 m |
aspect ratio |
18,60 - |
18,60 - |
| length |
8,52 m |
8,52 m |
height |
2,45 m |
2,45 m |
landing gear |
fixed |
retractable |
main wheel |
380x150 |
380x150 |
nose wheel |
300x100 |
300x100 |
wheel track |
2,00 m |
2,00 m |
wheel base |
2,00 m |
2,00 m |
best glide ratio |
33:1 |
39:1 |
airspeed at best glide ratio |
117 km/h |
123 km/h |
min. sink rate (empty weight + 70kg) |
0,86 m/s |
0,74 m/s |
min. wing loading (empty weight + 70kg) |
38,1 kg/m² |
39,0 kg/m² |
max. wing loading |
48,8 kg/m² |
48,8 kg/m² |
max. rate of climb at MSL (with MTOP) |
4,73 m/s |
5,8 m/s |
rate of climb at MCP (with MTOW) |
4,44 m/s |
5,1 m/s |
cruising speed at MCP at MSL |
267 km/h |
280 km/h |
cruising speed at 55% MCP at MSL |
214 km/h |
240 km/h |
fuel consumption at MCP |
25,0 l/h |
25,0 l/h |
fuel consumption at 55% MCP |
14,5 l/h |
14,5 l/h |
range at 55% MCP at MSL long range version |
2,000 km |
2,300 km |
All numbers are subject to change.
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