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. [1]
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]
This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
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. [1]
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]
This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |