Cruise Speed
333.3597 km/h
Entry Into service
1942-01-01
Maximum Take-Off Weight
8.184 t (paragliders: kg)
Maximum Range
2544.648 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
Maximum Range (km) |
|
Nakajima J1N Gekkō |
8.184 |
1700 |
2544.648 |
Similar airplanes
All data (25 fields)
- Name
- Nakajima J1N Gekkō
- Manufacturer
- Nakajima Aircraft Company
- Description
- The Nakajima J1N is a twin-engined heavy fighter designed and produced by the Nakajima Aircraft Company.
- First Flight
- 1941-05-01
- Entry Into service
- 1942-01-01
- Production End
- 1944-01-01
- Service End
- 1945-01-01
- Designer
- Nakajima Aircraft Company
- Type
- Heavy fighter, night fighter
- Length (m)
- 12.77
- Height (m)
- 4.562
- Cockpit Crew
- 2
- Max Speed (km/h)
- 507.4476
- Cruise Speed (km/h)
- 333.3597
- Rate of Climb (m/s)
- 8.7
- Armament
- 4× 20 mm Type 99 cannon, two upward- and two downward-firing, :::or 2× 20 mm Type 99 cannon, firing upward only :::or 3× 20 mm Type 99 cannon, all three firing upward
- National Origin
- Japan
- Number Built
- 479
- Powerplant Description
- 2 × Nakajima NK1F Sakae 21 14-cylinder two-row air-cooled radial piston engine, 843 kW (1130 hp) each
- Primary Users
- Imperial Japanese Navy Air Service
- Status
- Retired
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Nakajima_J1N_Gekk%C5%8D
- Flat Wing Span (m)
- 16.98
- Flat Wing Area (m²)
- 40
- Number of Engines
- 2