Dobi-II

Dobi-II

Role	Reconnaissance aircraft
National origin	Lithuania
Manufacturer	Dobi
Designer	Jurgis Dobkevičius
First flight	October 1923

The Dobi-II is a second airplane 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.

Specifications

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-cyl. water-cooled in-line piston engine, 150 kW (200 hp)

Performance

Maximum speed: 248 km/h (154 mph; 134 kn)
Cruising 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 (29,528 ft)

See also

Wikimedia Commons has media related to Dobi.

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