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IHI XF9-1

IHI XF9-1 prototype low-bypass afterburning turbofan engine developed under Japan's fighter-engine technology program. Japan's ATLA describes a 15-tonne-class (at least 153 kN) afterburning prototype with approximately 4.8 m length and 1 m inlet diameter, integrating high-temperature, high-power-extraction technologies for future fighter propulsion; the record is kept at development status and does not infer a production aircraft installation.

Identity

Aliases
XF9-1IHI XF9-1XF9 prototype engine
Domains
aviation
Identity Level
model
Kind
turbofan
Name
IHI XF9-1
Status
development

Details

Description
IHI XF9-1 prototype low-bypass afterburning turbofan engine developed under Japan's fighter-engine technology program. Japan's ATLA describes a 15-tonne-class (at least 153 kN) afterburning prototype with approximately 4.8 m length and 1 m inlet diameter, integrating high-temperature, high-power-extraction technologies for future fighter propulsion; the record is kept at development status and does not infer a production aircraft installation.
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Creation Time
August 14, 2026 at 18:31:05 UTC
Updated Time
August 14, 2026 at 18:31:05 UTC

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