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kcran567 said:I think the fact the F-35 is not really that good looking of a fighter is a valid reason to replace it.
A good troll isn't so obvious.
kcran567 said:I think the fact the F-35 is not really that good looking of a fighter is a valid reason to replace it.
kcran567 said:I think the fact the F-35 is not really that good looking of a fighter is a valid reason to replace it.
SpudmanWP said:kcran567 said:I think the fact the F-35 is not really that good looking of a fighter is a valid reason to replace it.
Count yourself lucky we did not end up with the F-32
Dragon029 said:Source on the faster and more manoeuvrable?
Foo Fighter said:Perhaps the ideal would be to cut the electives out of the equation, have instead a department like DARPA who have a remit to have the required product at the best possible cost.
SpudmanWP said:Not to mention that the final design for the -32 was never tested (normal wing/tail, not delta)
kcran567 said:There were a couple sources saying that the x-32 had better "up and away performance" not to mention the big wing and thrust vectored nozzle.The reason I ask is because the only public study I've seen done into the two put the X-35 ahead: http://www.dept.aoe.vt.edu/~mason/Mason_f/JSFWeisman.pdf
That analysis indicates that the X-32 would have been a better dogfighter, but would also have been slower and had a lower range.
The direct lift solution has always been less powerful / efficient and always more prone to hot gas reingestion as on the Harrier.As far as the x-35 having better VTOL, so what! The x-32 used perfectly good direct lift like the Harrier did for 40 years,
It seems a bit silly to compare a <1 year tech demo test program against that of a production aircraft. If a design has trouble doing the basics, your margins are tighter and it becomes harder to deal with any weight gains, etc.much simpler (cheaper) and less complicated than the x-35s fan-shaft system. As far as any difficulty during fly off, it was nothing compared to boondoggle development of f-35.
Fuel is always important for maritime / naval strike; having a greater T:W also just simply means more futureproofing. The X-32 was a neat design, but it's performance margins were simply too tight.It's not like the F-35b is lifting much more than a few sdb's or jdams anyway. Is the f-35b really going to be lifting much larger loads than the x-32 was expected to?