 | This article needs additional citations for
verification. (November 2013) |
| 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).
Applications
Specifications (XF5-1)
General characteristics
- Type: afterburning turbofan
- Length: 3 m (120 in)
- Diameter: 61 cm (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
Comparable engines
Related lists
References
Wikimedia Commons has media related to
Ishikawajima-Harima F5.
- ^ Policy evaluation report (summary)
-
^
"Archived copy" (PDF). Archived from
the original (PDF) on 2017-03-22. Retrieved 2021-07-02.
{{ cite web}}: CS1 maint: archived copy as title ( link) -
^
"Archived copy" (PDF). Archived from
the original (PDF) on 2013-02-03. Retrieved 2021-07-02.
{{ cite web}}: CS1 maint: archived copy as title ( link)
| This article needs additional citations for
verification. (November 2013) |
| 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).
Applications
Specifications (XF5-1)
General characteristics
- Type: afterburning turbofan
- Length: 3 m (120 in)
- Diameter: 61 cm (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
Comparable engines
Related lists
References
Wikimedia Commons has media related to
Ishikawajima-Harima F5.
- ^ Policy evaluation report (summary)
-
^
"Archived copy" (PDF). Archived from
the original (PDF) on 2017-03-22. Retrieved 2021-07-02.
{{ cite web}}: CS1 maint: archived copy as title ( link) -
^
"Archived copy" (PDF). Archived from
the original (PDF) on 2013-02-03. Retrieved 2021-07-02.
{{ cite web}}: CS1 maint: archived copy as title ( link)