Allison J102
{{Short description|Turbojet engine}}
| {{Infobox Aircraft Begin
|name=J102 |image= |caption= }}{{Infobox Aircraft Engine |type=Turbojet |manufacturer=Allison Engine Company |first run=1991 |major applications= }} |
The Allison J102 was a turbojet engine developed as a supersonic missile engine by the Allison Engine Company.{{cite web | title=Designations Of U.S. Military Aero Engines | url=http://www.designation-systems.net/usmilav/engines.html | publisher=www.designation-systems.net | date= 2008-02-22 | access-date=2009-09-19}}
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.{{cite journal | title=USN poised for supersonic target | journal=Flight International | page=18 | date= 1997-06-04}}
References
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{{Allison aeroengines}}
{{USAF gas turbine engines}}
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Category:1990s turbojet engines
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