Trident said:
http://www.aviationweek.com/aw/blogs/defense/index.jsp?plckController=Blog&plckScript=blogScript&plckElementId=blogDest&plckBlogPage=BlogViewPost&plckPostId=Blog%3a27ec4a53-dcc8-42d0-bd3a-01329aef79a7Post%3a22abe2fc-0087-4e1e-a82d-04d19b25d322
More stuff on the ATD-X, including a first look at its XF5-1 engine. Apparently the demonstrator will be Gripen-sized and possibly not a direct prototype of a service version. So the paddles for TVC and the weird cockpit might yet disappear if it is ever developed into a production airframe. Regarding said cockpit, I'm with starviking's first explanation here (and it is a demonstrator, afterall) - I struggle to see how such a pronounced hump would improve aerodynamics when bubble canopies are apparently detrimental. Or perhaps the JASDF has indicated preferrence for a twin-seat design? The similarity to a tandem twin-seat Flanker with its elevated rear cockpit is undeniably striking.
Another interesting issue is how large a series production variant would be. It seems pointless to invest large sums of money into an engine sized for a Gripen-class demonstrator if the final design is supposed to be substantially larger, requiring either foreign engines or a new indigenous design.
1. The cutaway model of the XF5-1 appears to depict a far higher bypass ratio than one might expect? Am I incorrect?
2. Does the model depict an afterburner, because the info card doesn't seem to? Can anyone who reads Japanese glean any relevant specs from the below attachment?
3. I don't know whether modern jet engines are as readily "scaleable" as one might hope, but assuming that this project is indeed nothing but a scaled down demonstrator, is it in any way feasible to scale up the entire design for a far larger production standard aircraft, engines included?