| Name:Name: | Išikawadžima Cu-11 | |
| Original title: Original Name: | 石川島 ツ11 | |
| Category: Category: | motokompresorový engine | |
| Manufacturer: Producer: | 石川島播磨重工業株式会社 Ishikawajima Harima Jūkōgyō Kabushiki-Kaisha, Tokyo | |
| Period of production: Production Period: | DD.MM.1944-DD.MM.1945 | |
| Made pieces: Number of Produced: | a small amount of/ small numbers | |
| a Prototype made: Prototype Built: | DD.MM.1944 | |
| Use: Use: | Yokosuka P1Y1 15-Shi - only for tests Yokosuka MXY7 Ohka 22 Yokosuka MXY9 Shuka | |
| Technical data: Technical Data: | ||
| Weight: Weight: | 200 kg | |
| Overall length: Overall Length: | 2202 mm | |
| Total width / Diameter: Overall Width / Diameter: | 640 mm | |
| Fuel: Fuel: | gasoline | |
| Compressor: Compessor: | Axial flow single stage stage | |
| Combustion chamber : Combustors: | Ring | |
| Turbine: Turbine: | single-stage axial | |
| Performance: Performance: | ||
| Maximum thrust: Maximum thurst: | of 1.7 kN at 9 000 rev/min | |
| Note: Note: | For the drive of the compressor was used inline four-cylinder Hitači Ha-11-12 Hacukaze, this piston engine spinning at 9 000 rpm single stage aviální compressor. The channel for the compressor were injected fuel to the four burners, the resulting mixture of air and fuel after ignition of the rapidly expanded and expanding gases acting through the nozzle out of the engine to create forward thrust. The diameter of the impeller of the compressor was 540 mm, height of the blades 96,5 mm | |
| Source: Sources: | Robert C. Mikesh, Kikka, Monogram Aviation Publications, 1979, ISBN 0-914144-19-7. www.enginehistory.org http://ja.wikipedia.org/wiki/ airandspace.si.edu author archive | |
URL : https://www.valka.cz/Isikawadzima-Cu-11-t186604#543892Version : 0
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