|
| 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. |
| 7.92 |
26 |
8.36 |
90 |
79 |
175 |
79 |
175 |
158 |
350 |
18.9 |
3.89 |
0 |
0 |
| Aspect
ratio: |
7.51 |
| Airfoil: |
Northrop mod. |
| Structure: |
metal, wood and fabric |
| Engine: |
|
Comment:
The V-1 is a scaled down version of the bomber
and transport flying wing prototypes. Which were
produced by Northrop near and shortly after the
end of World War II. It differs from these by
the addition of a vertical tail surface. Control
of both pitch and roll is accomplished by
rotating wingtips which make up 0.61 m. / 2 ft.
of the span. The pilot is located in a prone
position within the wing root. |
|
