Allison J102
Turbojet engine
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]
Operational history
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]
References
Notes
- ^ "Designations Of U.S. Military Aero Engines". www.designation-systems.net. 2008-02-22. Retrieved 2009-09-19.
- ^ a b "USN poised for supersonic target". Flight International: 18. 1997-06-04.
- v
- t
- e
Allison Engine Company aircraft engines
- VG-1410
- V-1710
- V-3420
- J33
- J35
- J71
- J102
- AE 3007
- AR.168R†
- TF32
- TF41
† Joint development aeroengines
This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them. |
This article about aircraft engines is a stub. You can help Wikipedia by expanding it. |
- v
- t
- e