Mitsubishi G1M

Length
15.83 m
Flat Wing Span
25 m
Height
4.53 m
Flat Wing Area
75 m²
Max Speed
265.5418 km/h
Max Ceiling
4600 m
Number of Engines
2
Aircraft Engine
First Flight
1934-04-01
Number Built
1
Maximum Range
4407.993 km

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Aircraft Weight Variants

Aircraft Maximum Range (km)
Mitsubishi G1M 4407.993

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All data (20 fields)
Name
Mitsubishi G1M
Manufacturer
Mitsubishi Aircraft Corporation
Description
The Mitsubishi G1M was a long-range twin-engined attack bomber built by Mitsubishi for the Imperial Japanese Navy in the 1930s.
First Flight
1934-04-01
Designer
Mitsubishi Aircraft Corporation
Length (m)
15.83
Height (m)
4.53
Cockpit Crew
5
Max Speed (km/h)
265.5418
Max Ceiling (m)
4600
Armament
2× flexibly mounted 7.7 mm machine guns (one mounted in the nose and one in dorsal position)
National Origin
Japan
Number Built
1
Powerplant Description
2 × Hiro Type 91 water-cooled W12 engine, 485 kW (650 hp) each
Status
Prototype only
Wikipedia Article (URL)
en.wikipedia.org/wiki/Mitsubishi_G1M
Flat Wing Span (m)
25
Flat Wing Area (m²)
75
Aircraft Engine
Hiro Type 91
Number of Engines
2