| Manufacturer |
Zmaj aircraft |
Dassault Aviation |
| Description |
The Zmaj R-1 () was a twin-engined prototype bomber produced by Zmaj aircraft of the former Yugoslavia, designed in the 1930s. |
The Dassault M.D.320 Hirondelle was a French 14-seat utility transport aircraft of the 1960s, designed and built by Dassault Aviation. |
| First Flight |
1940-04-24 |
1968-09-11 |
| Service End |
1941-01-01 |
|
| Designer |
D.Stankov |
Dassault Aviation |
| Type |
|
Utility transport |
| Length (m) |
12.78 |
12.72 |
| Height (m) |
2.5 |
|
| Cockpit Crew |
3 |
2 |
| Max Seating |
|
6 |
| Max Speed (km/h) |
450 |
500 |
| Cruise Speed (km/h) |
320 |
|
| Max Ceiling (m) |
10000 |
9000 |
| 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 |
|
| Capacity Description |
|
6 to 14 passengers depending on seating configuration or 1200 kg payload |
| National Origin |
Yugoslavia |
|
| Number Built |
1 |
1 |
| Powerplant Description |
2 × Hispano-Suiza 14AB 14-cyl. air-cooled radial piston engine, 552 kW (740 hp) each |
2 × Turbomeca Astazou XIVD turboprop engines, 686 kW (920 hp) each |
| Primary Users |
Yugoslav Royal Air Force |
|
| Status |
retired |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Zmaj_R-1 |
en.wikipedia.org/wiki/Dassault_Hirondelle |
| Flat Wing Span (m) |
14.4 |
14.55 |
| Flat Wing Area (m²) |
33.8 |
27 |
| Aircraft Engine |
Hispano-Suiza 14AB |
|
| Number of Engines |
2 |
2 |