About next generation engines, there is one non VCE project with max ab thrust of around 200KN, TIT 2400K and 15% better fuel efficiency as the less ambitious option. There is also a VCE project with TIT close to 2600K(?)
That diagram showing a 2400K engine with 17.97% more thrust than f119, turns out it used a ridiculously high source of f119 thrust in itts references, so final thrust should be around 200KN
That diagram showing a 2400K engine with 17.97% more thrust than f119, turns out it used a ridiculously high source of f119 thrust in itts references, so final thrust should be around 200KN