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The TF30 was developed as an after burner equipped turbofan. Using a 3 stage fan, the engine was chosen for the F-111 and saw service from 1964 to 1986.
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| Rated Output |
20,900 lbs thrust |
| Compressor |
6 stage low pressure, 7 stage high pressure axial flow |
| Turbine |
3 stage low pressure, 1 stage high pressure axial flow |
| After Burner |
25,100 lbs thrust depending on series |
| Commonly Used On |
F-111, F-14A, A-7A, B, C |
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