| J102 | |
|---|---|
| Type | Turbojet |
| Manufacturer | Allison Engine Company |
| First run | 1991 |
The Allison J102 was a turbojet engine developed as a supersonic missile engine by the Allison Engine Company.
Operational history
The J102-100 is an axial flow turbojet that was first run in March 1991. In 1997 it was being considered for use in a sea-skimming supersonic target for the United States Navy.
References
Notes
- "Designations Of U.S. Military Aero Engines". www.designation-systems.net. 2008-02-22. Retrieved 2009-09-19.
- ^ "USN poised for supersonic target". Flight International: 18. 1997-06-04.
| Allison Engine Company aircraft engines | ||
|---|---|---|
| V engines |  | |
| Turbojets | ||
| Turbofans | ||
| Turboprops/Turboshafts | ||
| Propfan | ||
| † Joint development aeroengines | ||
| United States military gas turbine aircraft engine designation system | |
|---|---|
| Turbojets | |
| Turboprops/ Turboshafts | |
| Turbofans | |
| Adaptive cycle engines | |
 |
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