Zahid
Junior Member
Hmm ... if that can possibly be the case for the Mach-2 claim, it would support my argument that there might be some structural changes to Block-llls. My argument was that since the first two blocks were 50 aircraft each (unless that has changed). That Block-lll would most likely have structural changes which would go along the lines of F/A-18Cs to F/A-18Es. Greater wing surface area (more hard points) and redesigned DSI (Mach-2 speed). Considering that Block-llls will be produced to the tune of 100-150 aircraft. Then such a structural design change is justifiable.
But that's just my view and I can be wrong. I thank Zahid, Plaworlf, Deino and Sinosoldier for your analysis. Much appreciated, guys.
1. I can not talk about engine issue. But do expect a change. I will not divulge the information until the bird flies. My guess (not confirmed info) is that the changes would change both endurance & power, but it would be an incremental change. I do not expect Block-III to cross Mach 2. The DSI penalty would be too huge to climb over with marginally more power, unless the design changes.
2. I do not know about the structural changes apart from inclusion of more composites.
3. EO pods may function as a substitute for IRST.
4. The philosophy of the design would not change with incremental changes (composites, engine power, etc...).