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| |Crew||colspan="2"|Two | |Crew||colspan="2"|Two | ||
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| |First Flight||colspan="2"| |
|First Flight||colspan="2"|October 1923 | ||
| |- | |- | ||
| |Ended Service||colspan="2"|], ] | |Ended Service||colspan="2"|], ] | ||
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| !bgcolor="#87CEEB" colspan="3"|Powerplant | !bgcolor="#87CEEB" colspan="3"|Powerplant | ||
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| |Engine||colspan="2"|1x ] ( |
|Engine||colspan="2"|1x ] (200 hp) | ||
| |- | |- | ||
| !bgcolor="#87CEEB" colspan="3"|Performance | !bgcolor="#87CEEB" colspan="3"|Performance | ||
Revision as of 20:03, 2 October 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 (200 hp) | |
| 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
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