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Engine was developed for the Lockheed P-80 Shooting Star. Engine was in production from 1949 thru 1955.
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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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