A pre-research study conducted on the next-generation medium airlifter that would succeed the Y-8 (codenamed Y-8X) from all the way back in 2005. This Y-8X would eventually evolve into the Y-15 that we know of today.
It should be noted that certain performance parameters laid out by this paper may have been modified/adjusted during the development process of the Y-15.
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@OedoSoldier on Weibo.
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oh yes, I still remember reading about Y-8X project and having high hopes of it (this is pre-Y20, so a 30t transport was like the dream for PLA fans) and then getting disappointed by Y-9. But now having looked back, Y-9 was quite important as the special missions platform and they really had no need for Y-8X.
Comparing these numbers to A400M
141t max takeoff, 50t internal fuel and 78.6t empty weight. 4x 8MW turboprop
30t payload with 4500km range
20t payload with 6400km range
3300km at max payload (37t)
Now C130J
34t empty weight and 70t max takeoff, 21t max payload, 4 x 3.45MW turboprop
Range is 3300km at 15.4t
Y-9
4x3.8MW turboprop
I thought the only difference of the (few) KJ-500As is the refueling probe? The first image is a close-up of the KJ-500's radome, and the second is a close-up of the KJ-500A's radome—you can clearly see the distinct differences in their structure:
www.sinodefenceforum.com
if we remember this where fuel was 17.8t, max payload is 23t?
if we assume using 4x5MW turboprop here, then max takeoff for Y-15 would be around 100t.
If we assume latest lightweight technology can keep empty weight to 45t. Then you could have 30t fuel and 30t max payload.
25t payload would allow you to still fly with 30t fuel. That would be pretty good range.