Short description: 2010s Japanese turbofan aircraft engine

XF5

Type  | Turbofan
National origin | Japan
Manufacturer  | IHI Corporation
Major applications | Mitsubishi X-2 Shinshin

The Ishikawajima-Harima Heavy Industries (IHI) XF5 is a low bypass turbofan engine developed in Japan by Ishikawajima-Harima Heavy Industries for the Mitsubishi X-2 Shinshin (ATD-X).

## Contents

* 1 Applications
* 2 Specifications (XF5-1)
* 2.1 General characteristics
* 2.2 Components
* 2.3 Performance
* 3 See also
* 4 References

## Applications

* Mitsubishi X-2 Shinshin

## Specifications (XF5-1)

XF5-1 engine undergoes performance testing

Data from [1][2][3]

#### General characteristics

* Type: afterburning turbofan
* Length: 3 m (120 in)
* Diameter: .6 m (24 in)
* Dry weight: 644 kg (1,420 lb)

#### Components

* Compressor: axial, 3 stage fan, 6 compressor stage
* Combustors: annular
* Turbine: 1 stage high pressure turbine, 1 stage low pressure turbine

#### Performance

* Maximum thrust: 49 kilonewtons (11,000 lbf)
* Overall pressure ratio: 26:1
* Turbine inlet temperature: 1,600 °C
* Thrust-to-weight ratio: 7.8

## See also

Related development

* Ishikawajima-Harima F3
* IHI Corporation F7
* IHI Corporation XF9

Comparable engines

* GTRE GTX-35VS Kaveri
* Ivchenko-Progress AI-222
* Honeywell/ITEC F124
* Rolls-Royce Turbomeca Adour

Related lists

* List of aircraft engines

## References

1. ↑ Policy evaluation report (summary)
2. ↑ https://www.mod.go.jp/j/approach/hyouka/seisaku/results/21/jigo/sankou/16.pdf
3. ↑ https://www.mod.go.jp/trdi/research/R3-2p.pdf

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