Not sure how legitimate this is, but here are some documents posted on a . The documents ask for engineering studies and test samples of various parts and systems that point to a new transport being developed. Given the nature of these systems, I think this plane could be a new heavy transport in the same class as the or the .
Corrections and critiques are welcome.
1) (Performance Simulation of Hydraulic Control System for a Large Nose Cargo Door):
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2) (Engineering Samples/Demonstration of Nose and Rear Cargo Door Seals):
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3) (Demonstration/Simulation of a for a High-bypass Engine):
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4) (I believe this is a call for engineering samples/test pieces for a foldable/retractable partition system separating the upper and lower decks of the fuselage. The system is to be of metal/composite construction. Dimensions are 1.72m x 2.45m x 3.28m):
A paper on numerical simulation of the aerodynamics of a large strategic transport. Filing it here for record keeping, since there have been signs of China working on a large transport in the same class as C-5 and AN-124. Of particular interest is that the paper examined the aerodynamics of an early warning variant mounting an impressively large radome.
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this research paper indicate, this project could be in research/development phase. exploring different ideasFigured it's be better to reply to the paper separately.
The general dimension of the aircraft given in the paper is pretty much similar to the now-destroyed An-225.
As for the engines - The 569 kN max thrust per engine value sounds outright bogus. An An-225-sized airlifter won't need 4x 569 kN-class engines when 4x 350-400 kN-class engines is already sufficient.
Figured it'd be better to reply to the academic paper separately in separate threads.
The general dimension of the aircraft given in the paper is pretty much similar to the now-destroyed An-225.
As for the engines - The 569 kN max thrust per engine value sounds outright bogus. An An-225-sized airlifter don't need 4x 569 kN engines when 4x 350-400 kN-class engines is already sufficient.
For reference, the An-225 is powered by 6x 230 kN engines.
To be fair, an-225 was almost exclusively designed as a barely flying AKS(space launch system) carrier, which for most of it's career didn't do it job. It isn't a good example of proper military transport.For reference, the An-225 is powered by 6x 230 kN engines.
They want An-225 but with austere field capability thenFigured it'd be better to reply to the academic paper separately in separate threads.
The general dimension of the aircraft given in the paper is pretty much similar to the now-destroyed An-225.
As for the engines - The 569 kN max thrust per engine value sounds outright bogus. An An-225-sized airlifter don't need 4x 569 kN engines when 4x 350-400 kN-class engines is already sufficient.
For reference, the An-225 is powered by 6x 230 kN engines.