Ishikawajima-Harima J3

Last updated
J3
Ishikawajima-Harima XJ3 turbojet engine left front view in Yamato Museum May 6, 2019 02.jpg
Type Turbojet
National origin Japan
Manufacturer Ishikawajima-Harima
Major applications Fuji T-1
Kawasaki P-2J

The Ishikawajima-Harima J3 was a Japanese turbojet aircraft engine. It was the first jet engine designed and built in Japan after the Second World War and was used to power the Fuji T-1 trainer and as a booster engine in the Kawasaki P-2J patrol aircraft.

Contents

Design and development

Development of the J3, the first Japanese post-war jet engine, [1] intended to power the Fuji T-1 jet trainer, was begun in 1955 by the Nippon Jet-Engine Company, with Ishikawajima-Harima Heavy Industries (IHI) being designated prime contractor in 1959. [2] [3] The resulting engine was a small, simple axial-flow turbojet.

The first pre-production engine began flight testing in a Curtiss C-46 testbed in February 1960, with production deliveries beginning in April 1962. [4]

Operational history

While the J3 was designed to power the Fuji T-1, it was not ready in time and the first version of the T-1 was powered by imported British Bristol Orpheus engine. The J3-IHI-3 version of the engine equipped the later T-1B version. [4] A more powerful version of the J3, the J3-IHI-7 was used to re-engine the T-1Bs and as booster engines for the Kawasaki P-2J maritime patrol aircraft. [5]

Variants

J3-IHI-3 01.jpg
J3-1
Nippon Jet-Engine Company prototype. [3] [6]
J3-IHI-3
Initial production version for Fuji T-1B trainer. 11.8 kN (2,645 lbf) thrust. [4]
J3-IHI-7
More powerful version used as auxiliary engine in the P-2J and to re-engine T-1B trainers. 13.7 kN (3,080 lbf) thrust. [5]
J3-IHI-7C
13.7 kN (3,080 lbf) for take-off.
J3-IHI-8
15.19 kN (3,415 lbf) for take-off.
J3-IHI-F
Aft-fan variant, 16.7 kN (3,750 lbf). [4] — the later Ishikawajima-Harima F3 turbofan engine began flights in 1985. [7] [8]

Applications

Specifications (J3-IHI-7C)

Data from Jane's All The World's Aircraft 1976–77 [5]

General characteristics

Components

Performance

See also

Related lists

Related Research Articles

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References

  1. Flight International 9 October 1976, p. 1150.
  2. Flight International 28 June 1962, p. 1012.
  3. 1 2 Taylor 1966, p. 492.
  4. 1 2 3 4 Taylor 1966, pp. 492–493.
  5. 1 2 3 Taylor 1976, pp.735–736.
  6. Bridgman, Leonard, ed. (1959). Jane's all the World's Aircraft 1959–60. London: Sampson Low, Marston & Co. Ltd. p. 512.
  7. Hamada, T., Akagi, M., Toda, D., Shimazaki, H., & Ohmomo, M. (1989). T-4 Inlet/Engine Compatibility Flight Test Results. Presented at the AIAA/ASME/SAE/ASEE 25th Joint Propulsion Conference, Monterey, CA: American Institute of Aeronautics and Astronautics.
  8. Wilkinson, Paul H. (1964). Aircraft engines of the World 1964/65 (20th ed.). London: Sir Isaac Pitman & Sons Ltd. p. 192.

Further reading