The Allison J102 was a turbojet engine developed as a supersonic missile engine by the Allison Engine Company.[1]
J102 | |
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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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