Vertol VZ-2
| Use attributes for filter ! | |
| Top speed | 340 km/h |
|---|---|
| Range | 210 km |
| Retired | 1965 |
| Weight | 1678 (kg) |
| Engine types | Lycoming T53 |
| First flight | August 13, 1957 |
| Date of Reg. | |
| Date of Upd. | |
| ID | 2358438 |
About Vertol VZ-2
The Vertol VZ-2 was a research aircraft built in the United States in 1957 to investigate the tiltwing approach to vertical take-off and landing. The aircraft had a fuselage of tubular framework and accommodation for its pilot in a helicopter-like bubble canopy.
