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Aichi M6A Seiran (Mountain Haze) |
 | | One Aichi AE1P Atsuta 30 or Atsuta 31 twelve-cylinder inverted-vee liquid-cooled engine, rated at 1,400 hp for take-off, 1,250 hp at 1,700 m and 1,290 hp at 5,000 m, driving a constant-speed three-blade metal propeller (M6A1 prototypes). |
 | | One Aichi Atsuta 32 twelve-cylinder inverted-vee liquid-cooled engine, rated at 1,400 hp for take-off, 1,340 hp at 1,700 m and 1,290 hp at 5,000 m, driving a constant-speed three-blade metal propeller (M6A1 production aircraft and M6A1-K prototypes). |
 | | One Mitsubishi MK8P Kinsei 62 fourteen-cylinder air-cooled radial, rated at 1,560 hp for take-off, 1,340 hp at 2,100 m and 1,190 hp at 5,800 m, driving a three-blade constant-speed metal propeller (E16A2 prototype). |
| www.combinedfleet.com /ijna/m6a.htm (220 words) |
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