Length
11 m
Flat Wing Span
13 m
Height
2.68 m
Flat Wing Area
26.4 m²
Cruise Speed
376 km/h
Max Speed
460 km/h
Max Ceiling
8000 m
Number of Engines
2
Aircraft Engine
First Flight
1939-01-01
Number Built
1
Maximum Range
1000 km

Pictures

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Rogožarski R-313 1000

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All data (24 fields)
Name
Rogožarski R-313
Manufacturer
Prva Srpska Fabrika Aeroplana Zivojin Rogožarski A.D.
Description
The Rogozarski R-313 (Рогожарски Р-313 in Serbian) was a two-seat twin-engined monoplane designed as a fighter/light bomber/reconnaissance aircraft in Yugoslavia before World War II.
First Flight
1939-01-01
Service End
1942-01-01
Designer
Sima Milutinović
Length (m)
11
Height (m)
2.68
Cockpit Crew
2
Max Speed (km/h)
460
Cruise Speed (km/h)
376
Max Ceiling (m)
8000
Rate of Climb (m/s)
8.33
Armament
1 × 20 mm HS-404 and 1 × 7.9 mm FN; 4 × 106 kg
National Origin
Yugoslavia
Number Built
1
Powerplant Description
2 × Walter Sagitta inverted air-cooled V-12 piston engines, 368 kW (493 hp) each
Primary Users
Yugoslav Royal Air Force
Status
inactive
Wikipedia Article (URL)
en.wikipedia.org/wiki/Rogo%C5%BEarski_R-313
Flat Wing Span (m)
13
Flat Wing Area (m²)
26.4
Aircraft Engine
Walter Sagitta
Number of Engines
2