|
| 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 |
263 |
580 |
208 |
458 |
471 |
1038 |
44.86 |
9.17 |
0 |
0 |
| Aspect
ratio: |
21.4 |
| Airfoil: |
Wortmann mod |
| Structure: |
fiberglass |
| Engine: |
|
Comment:
The LS-3 was a 15 meter racing class sailplane
with full-span flaperons instead of the more
usual flap/aileron combination. The flaperons
are coupled with dive brakes to reduce approach
and landing speeds. The LS-3a version has
separate flaps and ailerons. All οΎ–3 series use a
fuselage similar to that developed for the
Standard Class LS-1f, which features a front-
hinged canopy and a fixed stabilizer on a T-
tail. The LS-3-17 version was offered with a 17
m. wing with no change in gross weight. ATC |
|
