The Allison J102 was a turbojet engine developed as a supersonic missile engine by the Allison Engine Company.[1]
| J102 | |
|---|---|
| Type | Turbojet |
| Manufacturer | Allison Engine Company |
| First run | 1991 |
The J102-100 is an axial flow turbojet that was first run in March 1991.[2] In 1997 it was being considered for use in a sea-skimming supersonic target for the United States Navy. .[2]
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| V engines | ||
| Turbojets | ||
| Turbofans | ||
| Turboprops/Turboshafts | ||
| Propfan |
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† Joint development aeroengines | ||
United States military gas turbine aircraft engine designation system | |
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| Turbojets | |
| Turboprops/ Turboshafts | |
| Turbofans | |
| Adaptive cycle engines |
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