Engineering:Romano R.120
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| R.120 | |
|---|---|
| Role | Bomber |
| National origin | France |
| Manufacturer | Chantiers aéronavals Étienne Romano |
| Designer | Etienne Romano |
| First flight | 1938 |
| Primary user | French Air Force (intended) |
| Number built | 1 |
The Romano R.120 was a twin-engine 4-seat bomber aircraft designed by Etienne Romano in the 1930s.
Specifications
Data from Aviafrance: Romano R.120[1]
General characteristics
- Crew: 4
- Length: 16.1 m (52 ft 10 in)
- Wingspan: 21.1 m (69 ft 3 in)
- Height: 4.25 m (13 ft 11 in)
- Wing area: 58 m2 (620 sq ft)
- Empty weight: 4,800 kg (10,582 lb)
- Gross weight: 9,100 kg (20,062 lb)
- Powerplant: 2 × Hispano-Suiza 14AA 14-cylinder two-row air-cooled radial piston engine, 730 kW (980 hp) each
Performance
- Maximum speed: 520 km/h (320 mph, 280 kn)
- Range: 1,400 km (870 mi, 760 nmi)
- Service ceiling: 9,000 m (30,000 ft)
Armament
- Guns: **2 x 7.5 mm (0.295 in) MAC 1934 in the nose turret
- 1 x 7.5 mm (0.295 in) MAC 1934 in a ventral position
- 1 x 20 mm (0.787 in) Hispano-Suiza HS-404 in a dorsal turret
- Bombs: 1,000 kg (2,200 lb) of bombs
References
- ↑ Parmentier, Bruno (30 November 2001). "Romano R-120" (in Fr). Paris. https://www.aviafrance.com/aviafrance1.php?ID=9402&ID_CONSTRUCTEUR=1116&ANNEE=0&ID_MISSION=0&MOTCLEF=. Retrieved 2 March 2019.
External links
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