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Worlds first engine in the 10,000 thrust class. Produced in 1953 through 1970. Designed to have low fuel consumption due to dual rotor compressor.
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| Rated Output |
10,000 lbs thrust |
| Compressor |
Dual-rotor axial flow |
| After Burner |
16,000 lbs thrust Depending on series |
| Commonly Used On |
B-52, F-100, F-101B, RF-101C, RF-101H, F-102, TF-102, F4D-1, SM-62, U-2A, KC-135A, F-8, 707, 720, DC-8 |
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