- Source: Savoia-Marchetti S.84
The Savoia-Marchetti S.84 was an Italian twin-engined airliner developed in Italy, from the three-engined Savoia-Marchetti S.73; only the prototype was completed and the designation was re-used for the Savoia-Marchetti SM.84.
Specifications (S.84 prototype)
Data from Italian Civil and Military aircraft 1930-1945 General characteristics
Crew: 4+
Capacity: 18 passengers, 269 kg (594 lb) of baggage and 519 kg (1,144 lb) of cargo and mail
Length: 19.8 m (65 ft 0 in)
Wingspan: 24 m (78 ft 9 in)
Empty weight: 5,987 kg (13,200 lb)
Gross weight: 9,480 kg (20,900 lb)
Powerplant: 2 × Gnome-Rhône 14Krsd 14-cylinder air-cooled radial piston engines, 670 kW (900 hp) each
Performance
Maximum speed: 350 km/h (220 mph, 190 kn) at 2,000 m (6,560 ft)
Cruise speed: 315 km/h (196 mph, 170 kn)
Range: 999 km (621 mi, 540 nmi)
Service ceiling: 7,798 m (25,584 ft)
Time to altitude: 4,000 m (13,120 ft) in 18 minutes
Notes
References
Kata Kunci Pencarian:
- Alitalia
- Don Juan de Austria
- Savoia-Marchetti S.84
- Savoia-Marchetti SM.84
- SIAI-Marchetti
- Savoia-Marchetti S.55
- Savoia-Marchetti S.56
- Savoia-Marchetti S.72
- Savoia-Marchetti SM.89
- Savoia-Marchetti S.66
- Savoia-Marchetti S.65
- Savoia-Marchetti S.71