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Nakajima Kotobuki
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The Nakajima Ha-1 Kotobuki was an aero-engine developed by Nakajima. It was a radial piston developed under licence from the Bristol Jupiter.
Contents
Variants
- 2-Kai-1 - 585 hp (436 kW)
- 2-Kai-3 - 610 hp (455 kW)
- 3-Kai - 710 hp (529 kW)
Applications
- Mitsubishi A5M
- Mitsubishi Ki-18
- Nakajima A1N2
- Nakajima A2N
- Nakajima Ki-8
- Nakajima E4N
- Nakajima E8N
- Nakajima Ki-34
- Nakajima Type 91
Specifications [1]
- Type: 9-cylinder radial
- Bore: 146mm (5.75in)
- Stroke: 160mm (6.3in)
- Displacement: 24.1L (1,471.2 in3)
- Dry weight: 350kg (772 lbs)
Components
- Cooling system: air-cooled
Performance
- Power output: 550-780 hp
- Specific power:
- Power-to-weight ratio:
See also
References
- ↑ Gunston, Bill. World Encyclopaedia of Aero Engines.
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This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.cs:Nakadžima Kotobuki it:Nakajima Kotobuki ja:寿 (エンジン)
| This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Nakajima Kotobuki". |
