|
| 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 |
14.29 |
153.8 |
224 |
465 |
116 |
255 |
340 |
750 |
23.79 |
4.87 |
0 |
0 |
| Aspect
ratio: |
15.75 |
| Airfoil: |
NACA 63-618 |
| Structure: |
all metal |
| Engine: |
|
Comment:
Only one 1-29 was built and has subsequently
been presented to the National Soaring Museum.
It consists of a modified 1-23G fuselage and
tail with the addition of a constant chord,
laminar-flow airfoil wing and balanced dive
brakes. The wing ribs are indentical, made from
one master die to help ensure laminar flow. It
has flush, counter-sunk rivets, and the heavy,
deep spar helps to reduce elastic wing
deflections and minimize skin oil-canning. |
|
