Dobi-II
| Dobi-II | |
|---|---|
 | |
| Role | Reconnaissance aircraft |
| National origin | Lithuania |
| Manufacturer | Dobi |
| Designer | Jurgis Dobkevičius |
| First flight | October 1923 |
The Dobi-II is the second airplane designed by Lithuanian aviator Jurgis Dobkevičius in 1922. It was tested in October 1923. After two landing accidents plans for mass production of Dobi-II were abandoned.[1]
Specifications
Data from Lithuanian Air Museum[1]
General characteristics
- Crew: 2
- Length: 6.1 m (20 ft 0 in)
- Wingspan: 14 m (45 ft 11 in)
- Wing area: 22.44 m2 (241.5 sq ft)
- Empty weight: 840 kg (1,852 lb)
- Gross weight: 1,240 kg (2,734 lb)
- Powerplant: 1 × Benz Bz.IV 6-cylinder water-cooled inline piston engine, 150 kW (200 hp)
Performance
- Maximum speed: 248 km/h (154 mph; 134 kn)
- Cruise speed: 190 km/h (118 mph; 103 kn)
- Stall speed: 90 km/h (56 mph; 49 kn)
- Range: 1,000 km (621 mi; 540 nmi)
- Service ceiling: 9,000 m (30,000 ft)
- Time to altitude: 34 min to 7,000 m (23,000 ft)
- Landing speed: 85 km/h (53 mph; 46 kn)[2]
References
- 1 2 "Dobi-II". Retrieved 27 January 2017.
- ↑ Serryer, J (13 March 1924). "Les avions Dobkevicius". Les Ailes (143): 2–3.
See also
 |
Wikimedia Commons has media related to Dobi. |
This article is issued from
Wikipedia.
The text is licensed under Creative Commons - Attribution - Sharealike.
Additional terms may apply for the media files.