Entry Into service
1941-04-02
Maximum Take-Off Weight
12.86 t (paragliders: kg)
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Mitsubishi G4M |
12.86 |
2852 |
Similar airplanes
All data (25 fields)
- Name
- Mitsubishi G4M
- Manufacturer
- Mitsubishi Aircraft Corporation
- Description
- 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
- 1939-10-23
- Entry Into service
- 1941-04-02
- Production End
- 1945-01-01
- Service End
- 1945-01-01
- Designer
- Kiro Honjo
- Type
- Medium bomber/Torpedo bomber
- Length (m)
- 19.97
- Height (m)
- 4.9
- Cockpit Crew
- 7
- Max Speed (km/h)
- 428
- Cruise Speed (km/h)
- 315
- Min Speed (km/h)
- 120
- 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
- National Origin
- Japan
- Number Built
- 2435
- Powerplant Description
- 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/Mitsubishi_G4M
- Flat Wing Span (m)
- 24.89
- Flat Wing Area (m²)
- 78.125
- Number of Engines
- 2