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Dobi-I
From PlaneSpottingWorld, for aviation fans everywhere
| Dobi-I | ||
|---|---|---|
| 300px | ||
| Description | ||
| Role | Sportplane | |
| Crew | One | |
| First Flight | July 1922 | |
| Ended Service | 1 December, 1925 | |
| Dimensions | ||
| Length | 4.5 m | |
| Wingspan | 7.9 m | |
| Wing area | 7.5 m² | |
| Weights | ||
| Empty | 167 kg | |
| Loaded | 200 kg | |
| Powerplant | ||
| Engine | 1x Haacke HFM-2 (30HP) | |
| Performance | ||
| Maximum speed | 175 km/h | |
| Cruise speed | 130 km/h | |
| Service ceiling | 3.8 km | |
Dobi-I is a plane designed by Lithuanian aviator Jurgis Dobkevičius and first airplane of Lithuanian design [1]. Jurgis Dobkevičius started designing and building Dobi-I in 1921, and it was first tested by designer in July 1922. Soon new models Dobi-II, and Dobi-III followed. Single prototype of Dobi-I was damaged in accident beyond repair on 1 December, 1925.
References
See also
Template:Lithuania-stub Template:Aero-1920s-stub
| This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Dobi-I". |
