Maximum Take-Off Weight
5.664 t (paragliders: kg)
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Zmaj R-1 |
5.664 |
1000 |
Similar airplanes
All data (24 fields)
- Name
- Zmaj R-1
- Manufacturer
- Zmaj aircraft
- Description
- The Zmaj R-1 () was a twin-engined prototype bomber produced by Zmaj aircraft of the former Yugoslavia, designed in the 1930s.
- First Flight
- 1940-04-24
- Service End
- 1941-01-01
- Designer
- D.Stankov
- Length (m)
- 12.78
- Height (m)
- 2.5
- Cockpit Crew
- 3
- Max Speed (km/h)
- 450
- Cruise Speed (km/h)
- 320
- Max Ceiling (m)
- 10000
- Rate of Climb (m/s)
- 5.55
- Armament
- 2x 20 mm Oerlikon cannon, and 4x 7.9 mm machine guns; 1600 kg of bombs carried internally
- National Origin
- Yugoslavia
- Number Built
- 1
- Powerplant Description
- 2 × Hispano-Suiza 14AB 14-cyl. air-cooled radial piston engine, 552 kW (740 hp) each
- Primary Users
- Yugoslav Royal Air Force
- Status
- retired
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Zmaj_R-1
- Flat Wing Span (m)
- 14.4
- Flat Wing Area (m²)
- 33.8
- Aircraft Engine
- Hispano-Suiza 14AB
- Number of Engines
- 2