Hitači Ne-230

Hitachi Ne-230
日立 ネ-230
Title:
Name:
Hitači No-230 Hitachi Ne-230
Original title:
Original Name:
日立 ネ-230
Category:
Category:
jet engine turbojet
Manufacturer:
Producer:
株式会社日立製作所, Kabushiki-gaisha Hitachi Seisakusho, Tokyo
Period of production:
Production Period:
DD.08.1944-DD.08.1945
Made pieces:
Number of Produced:
1 (?)
a Prototype made:
Prototype Built:
DD.MM.1945
Use:
Use:
Yokosuka R2Y2-G Keiun-Kai
Nakajima Ki-201 Karyū
Technical data:
Technical Data:
 
Weight:
Weight:
810 kg 1786 lb
Overall length:
Overall Length:
3429 mm 11ft 3in
Total width / Diameter:
Overall Width / Diameter:
762 mm 2 ft 6 inches
Fuel: Fuel: of diesel oil or kerosene or gasoline or their mixture diesel fuels or kerosene or gasoline or a mixture thereof
Compressor: Compessor: Axial 7 degrees 7-stage Axial compressor
Combustion chamber : Combustors: Ring the Annular combustion chamber
Turbine: Turbine: single-stage axial Single-stage axial turbine
Performance: Performance: 
Maximum thrust: Maximum thurst: 885 kp, 8,679 cn at 9 000 rev/min 1,950 lbf at 9,000 rpm
Note:
Note:
Japanese engineers according to incomplete drawings and a few photos of the German engine BMW 003 they designed their own engine.
Fa Hitači completed probably only one prototype, which was successfully tested in the maritime center in Takahagi.
The Ne-230 was an indigenous design, but the German BMW 003 turbojet engine was a major influence.
It was completed probably only one prototype, which was successfully tested at the naval base in Takahagi.
Source:
Sources:
Famous Aircraft of the World, first series, No.76, Japanese Army Experimental Fighters, Japan Bunrin-Do Co. Ltd., August 1976
airandspace.si.edu
http://ja.wikipedia.org/wiki/
http://www.airpages.ru/eng/jp/ki2.shtml
author archive
.
URL : https://www.valka.cz/Hitaci-Ne-230-t195750#563490 Version : 0
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