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Lift Jet Engine, JR100 FREE

[+] Author Affiliations
Masakatsu Matsuki, Tadao Torisaki

National Aerospace Laboratory, Tokyo, Japan

Kaneichiro Imai, Kiyoto Miyazawa

Ishikawajima-Harima Heavy Industries Co., Ltd., Tokyo, Japan

Paper No. 71-GT-75, pp. V001T01A075; 12 pages
doi:10.1115/71-GT-75
From:
  • ASME 1971 International Gas Turbine Conference and Products Show
  • ASME 1971 International Gas Turbine Conference and Products Show
  • Houston, Texas, USA, March 28–April 1, 1971
  • Conference Sponsors: International Gas Turbine Institute
  • ISBN: 978-0-7918-7982-5
  • Copyright © 1971 by ASME

abstract

As part of the program for developing VTOL craft, the National Aerospace Laboratory (NAL) of the Japanese Government installed two JR100 lift jet engines on their Flying Test Bed, following upon the successful outcome of tests on the Height Control Tower with other JR100 engines. These JR100 engines were developed in a joint effort between NAL and IHI. Five engines in three successively modified version have been produced, and the aggregate number of runs has already reached 1700, recording accumulated operating time of more than 200 hrs. The engine which has a 6-stage compressor, an annular combuster and a single-stage turbine, produces 3350 lb thrust and weighs 340 lb.

Copyright © 1971 by ASME
Topics: Jet engines
This article is only available in the PDF format.

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