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Revision as of 13:44, 1 September 2006
| 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 Waeight | 1240 kg | |
| Powerplant | ||
| Engine | 1x Benz Bz.IV (200HP) | |
| 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 aircrafts 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.
See also
 | This Lithuania-related article is a stub. You can help Misplaced Pages by expanding it. |
 | This aircraft-related article is a stub. You can help Misplaced Pages by expanding it. |
 | This military aviation article is a stub. You can help Misplaced Pages by expanding it. |