|
| Span |
Area |
Empty Weight |
Payload |
Gross Weight |
Wing Load |
Water Ballast |
| m |
ft |
sq.m |
sq.ft |
kg |
lb. |
kg |
lb. |
kg |
lb. |
kg
/sq.m |
lb.
/sq.ft |
kg |
lb. |
| 15 |
49.2 |
10.5 |
113 |
240 |
540 |
285 |
617 |
525 |
1157 |
50 |
10.24 |
0 |
0 |
| Aspect
ratio: |
21.29 |
| Airfoil: |
|
| Structure: |
|
| Engine: |
|
Comment:
The LS-8 is designed to Standard Class
specifications. Winglets come as standard and a
fin ballast tank is an option. Approach control
is by top surface Schempp-Hirth airbrakes.
Wingtip extensions bringing the span to 18 m.
are also an option. At the 1995 World
Championships at Omarama, New Zealand, LS-8ﾒs
scored 2nd, 4th and 5th in the Standard Class.
ATC |
|
