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

  1. ^ "Designations Of U.S. Military Aero Engines". www.designation-systems.net. 2008-02-22. Retrieved 2009-09-19.
  2. ^ a b "USN poised for supersonic target". Flight International: 18. 1997-06-04.
  • v
  • t
  • e
Allison Engine Company aircraft engines
V engines
  • VG-1410
  • V-1710
  • V-3420
Turbojets
  • J33
  • J35
  • J71
  • J102
Turbofans
  • AE 3007
  • AR.168R†
  • TF32
  • TF41
Turboprops/TurboshaftsPropfan
† Joint development aeroengines
  • v
  • t
  • e
United States military gas turbine aircraft engine designation system
Turbojets
Turboprops/
Turboshafts
Turbofans
Adaptive cycle engines
This aircraft engine article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.


Stub icon

This article about aircraft engines is a stub. You can help Wikipedia by expanding it.

  • v
  • t
  • e