|
| 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. |
| 18.29 |
60 |
21.49 |
231 |
476 |
1050 |
181 |
400 |
657 |
1450 |
30.61 |
4.85 |
0 |
0 |
| Aspect
ratio: |
12.88 |
| Airfoil: |
NACA 4301 2A |
| Structure: |
all metal |
| Engine: |
|
Comment:
Only one 2-25 was built and was flown in the
1954 World Championships at Champhill, England
and 1956 World Championships at St. Yan, France
in the multiplace category. Stan Smith and
R.Kidder fininished 3rd in 1954, and Kempes
Trager and Gene Miller were 4th in 1956. It has
triple spoilers (2 on top, 1 on bottom of each
wing). The sole example was donated to the
soaring program at the U.S. Air Force Academy
and later presented to the National Soaring
Museum. It is presently on loan to the U.S. Air
Force Museum at Wright Patterson FB, Dayton, OH. |
|
