Engines like this are asstonishing, They could've been used on airplanes wings to VTol, for wide wing airlines, private jets etc, by just assigning them in the bottom front & rear top of the wings width rim, across the elongate path row, without the front shield vector flap needed, since it can now balamce on a front and back, of rear pivit boosters thrusted down. like feet stands, made of air levitation propulsion
She's reading a script and doesn't remotely explain principals discussed and clearly doesn't know anything of her own accord .. typical corporate ad dumbed down and coated with sugar .. placed in a venue of engineering minds who want real information
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The F135 originated with Lockheed Corporation Skunk Works, with efforts to develop a stealthy STOVL strike fighter for the U.S. Marine Corps under a 1986 DARPA program. Lockheed employee Paul Bevilaqua developed and patented[4] a concept aircraft and propulsion system, and then turned to Pratt & Whitney (P&W) to build a demonstrator engine.[5] The ground test demonstrator used the first stage fan from a F119 engine for the lift fan. The engine fan and core from the F100-220 were used for the core of the demonstrator engine, and the larger low-pressure turbine from the F100-229 was used for the low-pressure turbine of the demonstrator engine. The larger turbine was used to provide the additional power required to operate the lift fan. Finally, a variable thrust deflecting nozzle was added to complete the "F100-229-Plus" demonstrator engine. This engine proved the lift-fan concept and led to the development of the current F135 engine
