| Manufacturer |
Mitsubishi Aircraft Corporation |
Savoia-Marchetti |
| Description |
The Mitsubishi G7M was a proposed twin-engine long-range bomber designed for use by the Imperial Japanese Navy in 1941. |
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. |
| First Flight |
|
1936-01-01 |
| Designer |
Mitsubishi Aircraft Corporation |
Savoia-Marchetti |
| Type |
|
Twin-engined airliner |
| Length (m) |
20 |
19.8 |
| Height (m) |
6.09 |
|
| Cockpit Crew |
7 |
4 |
| Max Seating |
|
18 |
| Max Speed (km/h) |
544 |
354.0557 |
| Cruise Speed (km/h) |
|
315.4314 |
| Max Ceiling (m) |
5000 |
7798.003 |
| Armament |
:: 6x 13 mm Type 2 machine guns ::2x 20 mm Type 99 Mark 2 machine gun (classified as machine guns by the IJN); up to 800 kg of bombs |
|
| Capacity Description |
|
18 passengers, 594 lb of baggage and 1144 lb of cargo and mail |
| National Origin |
|
Italy |
| Number Built |
|
1 |
| Powerplant Description |
2 × Mitsubishi MK10A 18-cylinder air-cooled radial piston engines, 1491 kW (2000 hp) each |
2 × Gnome-Rhône 14Krsd 14-cylinder air-cooled radial piston engines, 671 kW (900 hp) each |
| Primary Users |
Imperial Japanese Navy Air Service (planned) |
|
| Wikipedia Article (URL) |
en.wikipedia.org/wiki/Mitsubishi_G7M_Taizan |
en.wikipedia.org/wiki/Savoia-Marchetti_S.84 |
| Flat Wing Span (m) |
25 |
24 |
| Number of Engines |
2 |
2 |