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Engine was developed for the Lockheed P-80 Shooting Star. Engine was in production from 1949 thru 1955.
All photographs and text copyright Arizona Aerospace Foundation, 2009 and may not be used in any way without express written permission.
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| Rated Output |
4,600 lbs thrust |
| Compressor |
1 stage Centrifugal |
| Turbine |
1 stage axial |
| Dry Weight |
1,795 lbs |
| After Burner |
Water/Alcohol injection 5,400 lbs thrust |
| Commonly Used On |
P-80/F-80, T-33A, TV-2, T2V-1, F9F-4 |
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