Design
The F136 produces 18,000 lbf (80.1 kN) of lift thrust in STOVL configuration. Combined with thrust from the LiftFan (20,000 lbf/89.0 kN) and two roll posts (1,950 lbf/8.67 kN each), the Rolls-Royce LiftSystem produces a total of 41,900 lbf (186 kN) of thrust. This compares with the maximum thrust of 23,800 lbf (106 kN) for the Harrier's Rolls-Royce Pegasus engine.
Read more about this topic: General Electric/Rolls-Royce F136
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