| Name: | Mitsubishi Ne-330 | Mitsubishi Ne-330 | ||
| Original Title: | Original Name: 三菱 ネ-330 | |||
| Category: | jet engine | turbojet | ||
| Manufacturer: | Producer: | 三菱重工業株式会社 - Mitsubishi Jūkōgyō Kabushiki-Kaisha, Kobe | ||
| Period of production: Production Period: | DD.MM.1944-DD.08.1945 | |||
| Units produced: Number of Produced: | Only unfinished prototypes / Only unfinished prototypes | |||
| Prototype produced: Prototype Built: | DD.MM.1945 | |||
| Use: | Use: Yokosuka R2Y2-G Keiun-Kai Yokosuka Tenga | |||
| Specifications: | Technical Data: | |||
| Weight: Weight: | 1197 kg | 2640 lb | ||
| Overall length: Overall Length: | 4010 mm | 13ft 1.87in | ||
| Overall Width/Diameter: Overall Width / Diameter: | 1180 mm | 3ft 10.5in | ||
| Fuel: Fuel: | diesel fuel or gasoline or a mixture thereof | diesel fuel or gasoline | ||
| Compressor: | 7-stage Axial compressor | 7-stage Axial compressor | ||
| Combustion chamber : Combustors: | Annular | Annular combustion chamber | ||
| Turbine: [02COL1: | Single-stage axial | Single-stage axial turbine | ||
| Performance: | ||||
| Maximum thrust: | 1,297 hp, 12,722 kN at 7,600 rpm | 2,860 lbf at 7,600 rpm | ||
| Note: Note: | All outputs are calculated only. The engine was not completed, the prototypes under construction were destroyed in an air raid. | All performances are counted only. The development of this engine has not been completed. | ||
| Sources: Sources: | Famous Aircraft of the World, first series, No.76, Japanese Army Experimental Fighters, Japan, Bunrin-Do Co. Ltd., August 1976 http://www.airpages.ru/eng/jp/ki2.shtml http://ja.wikipedia.org/wiki/ http://www.airpages.ru/eng/jp/ki2.shtml author's archive | |||