|
| 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 |
9.64 |
103.8 |
181 |
400 |
118 |
260 |
299 |
660 |
31 |
8.96 |
0 |
0 |
| Aspect
ratio: |
23.29 |
| Airfoil: |
Wortmann FX 67-K-170/150 |
| Structure: |
all-metal monocoque fuselage and single-spar, multi-stringer stressed skin wing; elevator and rudder fabric covered |
| Engine: |
|
Comment:
The 1-35 was designed to 15 m. racing class
rules; however it was not fully competitive with
its glass fiber contemporaries. The 1-35 was
produced in successive, slightly differing,
models. The retractable gear versions carry up
to 145 kg./ 320 lb. Of water ballast while the 1-
35C had a fixed gear and no provision for
ballast. All use flaps for performance and
approach control with οΎ–8 to +32 degrees for the
former, and up to 82 degrees for the latter.
Specifications are for the 1-35C. The first 1-35
serial 001, belongs to the National Soaring
Museum. ATC. |
|
