Rogožarski R-313
Rogožarski · Yugoslavia · first flew 1939 · fighter
The Rogožarski R-313 was a two-seat twin-engined monoplane designed as a fighter, light bomber and reconnaissance aircraft in Yugoslavia before the Second World War.
Recognition (WEFT)
| W — Wings | Low-mounted, straight |
|---|---|
| E — Engines | 2 × piston, wing-mounted |
| F — Fuselage | 11 m fuselage |
| T — Tail | Conventional |
WEFT is AircraftIQ's four-point recognition method — how it works.
Spot it by:
- Two-seat twin-engined low-wing monoplane
- Two inverted V-12 piston engines driving three-bladed propellers
- Armed with a 20 mm cannon and a 7.9 mm machine gun
It is a twin-engined low-wing monoplane with two Walter Sagitta inverted V-12 engines.
Specifications
- The Rogožarski R-313 has a length of 11 m (36 ft).
- It has a wingspan of 13 m (43 ft).
- Its maximum speed is 460 km/h (286 mph).
- Typical crew: 2.
Figures are for the representative variant described above; marks differ. See how AircraftIQ sources figures.
History
It was designed and built at the Rogozarski factory in Belgrade and did not get beyond the prototype stage.
Variants
Only one was built, so there were no production variants.
Where you'll see it
Abandoned in April 1941, it was repaired by the Croats and flown in May 1942.
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