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Rogožarski Brucoš
 
Rog-Brucos
 
The Rogožarski Brucoš (Freshman, Serbian Cyrillic: Рогожарски Бруцош) was a single-engine, two-seat, low wing monoplane aircraft designed as a trainer in Yugoslavia in 1940. It was designed and built in the Rogožarski aircraft factory in Belgrade. Only one prototype was built.
 
Engine: 1 × de Havilland Gipsy Major I, 96 kW (129 hp)
Propeller: 2-bladed
Wingspan: 10.00 m (32 ft 10 in)
Wing area: 16.00 sq.m (172.2 sq ft)
Length: 8.10 m (26 ft 7 in)
Height: 3.10 m (10 ft 2 in)
Empty weight: 615 kg (1,356 lb)
Gross weight: 872 kg (1,922 lb)
Maximum speed: 185 km/h (115 mph; 100 kn) 210 km/h at sea level
Range: 840 km (522 mi; 454 nmi)
Service ceiling: 4,000 m (13,123 ft)
Rate of climb: 2.54 m/s (500 ft/min)
Crew: 2
 
Rog-Brucos-ld
 
 
 



 
 
 
 
 
 


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