|
| 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. |
| 9.86 |
32.35 |
10.91 |
117.5 |
107 |
235 |
86 |
190 |
193 |
425 |
17.69 |
3.63 |
0 |
0 |
| Aspect
ratio: |
8.9 |
| Airfoil: |
NACA 4412 |
| Structure: |
2-Strut-braced, 2-spar, constant chord, wood/fabric wings; metal/fabric tail; steel-tube/fabric fuselage |
| Engine: |
|
Comment:
The BG-6 was introduced in 1939 and produced in
both complete and kit form. It has no devices for
glidepath control. A few factory-built ships were
used as training gliders in World Was II. |
|