From Wikipedia, the free encyclopedia
| Dobi-II |
 |
|
| Description |
| Role |
Reconnaissance |
| Crew |
Two |
| First Flight |
October 1923 |
| Ended Service |
5 November 1924 |
| Dimensions |
| Length |
6.1 m |
| Wingspan |
14 m |
| Wing area |
22.44 m² |
| Weights |
| Empty |
840 kg |
| Flight Weight |
1240 kg |
| Powerplant |
| Engine |
1x Benz Bz.IV 200 hp (150 kW) |
| Performance |
| Maximum speed |
248 km/h |
| Cruise speed |
190 km/h |
| Minimum speed |
90 km/h |
| Service ceiling |
9 km |
| Range |
1000 km |
Dobi-II is a second plane from Dobi line of aircraft designed by Lithuanian aviator Jurgis Dobkevičius in 1922, tested in October 1923. After two landing accidents plans for mass production of Dobi-II were abandoned.
[edit] See also
