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Savoia-Marchetti S.84 ✕ Mitsubishi G4M ✕
Manufacturer Savoia-Marchetti Mitsubishi Aircraft Corporation
Description 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. The Mitsubishi G4M was a twin-engine, land-based medium bomber manufactured by the Mitsubishi Aircraft Company, a part of Mitsubishi Heavy Industries, and operated by the Air Service (IJNAS) of the Imperial Japanese Navy from 1940 to 1945.
First Flight 1936-01-01 1939-10-23
Entry Into service 1941-04-02
Production End 1945-01-01
Service End 1945-01-01
Designer Savoia-Marchetti Kiro Honjo
Type Twin-engined airliner Medium bomber/Torpedo bomber
Length (m) 19.8 19.97
Height (m) 4.9
Cockpit Crew 4 7
Max Seating 18
Max Speed (km/h) 354.0557 428
Cruise Speed (km/h) 315.4314 315
Min Speed (km/h) 120
Max Ceiling (m) 7798.003
Rate of Climb (m/s) 9.17
Armament 1× 20 mm Type 99 cannon (tail turret), 4× 7.7 mm Type 92 machine gun (nose turret ×1, waist positions ×2, top turret ×1); 1× 858 kg (1,892 lb) Type 91 Kai-3 (improved model 3) aerial torpedo or 1× 800 kg (1,764 lb) bomb or 4× 250 kg (551 lb) bombs or 1x 1200 kg (2,645 lb) Yokosuka MXY-7 Ohka suicide bomb
Capacity Description 18 passengers, 594 lb of baggage and 1144 lb of cargo and mail
National Origin Italy Japan
Number Built 1 2435
Powerplant Description 2 × Gnome-Rhône 14Krsd 14-cylinder air-cooled radial piston engines, 671 kW (900 hp) each 2 × Mitsubishi MK4A Kasei 11 14-cylinder air-cooled radial piston engines, 1141 kW (1530 hp) each
Primary Users Imperial Japanese Navy Air Service
Wikipedia Article (URL) en.wikipedia.org/wiki/Savoia-Marchetti_S.84 en.wikipedia.org/wiki/Mitsubishi_G4M
Flat Wing Span (m) 24 24.89
Flat Wing Area (m²) 78.125
Number of Engines 2 2