|
| 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. |
| 14.12 |
46.3 |
11 |
118.4 |
210 |
463 |
130 |
287 |
340 |
750 |
30.91 |
6.33 |
0 |
0 |
| Aspect
ratio: |
18.12 |
| Airfoil: |
Wortmann FX-60-17A11-182, root; FX-60-126, tip |
| Structure: |
all metal, except fabric covered rudder |
| Engine: |
|
Comment:
The Solo, which first flew in 1992, is a
flapless sailplane designed to the OSTIC World
Class sailplane specifications for the early
solo/club pilot. Construction follows Blanik
practice with all metal surfaces and flush
rivets. It has top surface only Schempp-Hirth
airbrakes. The fixed main wheel has an oleo-
pneumatic shock absorber. ATC |
|
