Advanced Medium STOL Transport (AMST) and its predecessors

Not sure if this has been answered already, I've read the specs and know they both met Air Force requirements, but is there any evidence they preferred one over the other (YC-14 and YC-15)?
The C-17 evolved from the YC-15, which might be indicative.
Both were McDonnell Douglas products. It would be strange for McDD to develop the C-17 from the YC-14. (Did Boeing have a C-17 competitor?) That said, I could swear I've seen somewhere where the YC-14 was liked more, or showed itself superior, to the YC-15.
The C-17 was derived from the YC-15, and Boeing's submission for the C-X competition, the Model 1050, was derived from the YC-14.
The C-17 requirement was for a longer-legged, higher capacity airplane and I suspect that the YC-15 configuration scaled up better than that of the YC-14. Boeing's C-17 entry was awkward looking and placed a 3rd engine above the tail cargo ramp.
They should have gone with four engines above the wing like this: Maybe there would have been a drag penalty though.

 
They should have gone with four engines above the wing like this: Maybe there would have been a drag penalty though.

Agree!

Regards
Pioneer
There must have been some drawback to adding engines outboard of the existing 2 since it's the obvious approach, assuming that an engine of appropriate thrust was available. 3 engines vs 4 brings savings but I wouldn't think that alone would be sufficient to justify placing an engine in the tail above cargo operations. If we discount the MD-11 as a development of the DC-10, it may have been the last clean-sheet big tri-jet design..
 
They should have gone with four engines above the wing like this: Maybe there would have been a drag penalty though.

Agree!

Regards
Pioneer
There must have been some drawback to adding engines outboard of the existing 2 since it's the obvious approach, assuming that an engine of appropriate thrust was available. 3 engines vs 4 brings savings but I wouldn't think that alone would be sufficient to justify placing an engine in the tail above cargo operations. If we discount the MD-11 as a development of the DC-10, it may have been the last clean-sheet big tri-jet design..
Could have used four F117s, or even just four of the engines the YC-14 used. There were plenty of engine options. It's a head scratcher.
 
From Aviation magazine 1972.
 

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From Aviation magazine 1974.
 

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Just to ask, but where did you find these paintings
The source for all good things these days: Ebay.
Were they from a specific seller on eBay you could recommend? Or were they "scattered" and could only be found after doing some "digging"?
The AMST and AATS paintings came from one seller, the Hughes hot cycle painting from another, the Lockheed stowed-rotor painting from another. In all cases, they came to my attention almost through sheer dumb luck.
 
is there any design consideration in c17 or amst to prevent fod issue on engine?
At least one measure I am aware of on the C-17A is that its thrust reversers direct flow only upwards and forward, so as to mitigate any additional dust and debris from being kicked up by the reversers and ingested into the engines on rough/unprepared airstrips. Another is the nose gear doors splay open outwards almost (but not quite) horizontally to prevent any dust, gravel, etc., kicked up by the nose gear wheels from being ingested by the engines.

Here's some footage that demonstrates both features nicely.
YouTube: AiirSource Military - "C-17 Globemaster III Reverse Thrust Stunt - Short Field Landing & Backing Up"
 
From my own collection, one of the YC-14 demonstrators at its current residence at the Pima Air & Space Museum.

Picture taken in April 2022.
 

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More photos of the YC-14 (sans engines) at Pima Air Museum. One engine (GE CF6-50D turbofan) is displayed beside the aircraft
GE CF6-50D turbofan. And a single photo of the other YC-14 at Davis-Monthan AFB (AKA "The Boneyard") taken during a tour.
 

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Early concept model of what became the YC-14 recently acquired on eBay. In addition to the recontoured nose, different glazed areas and slanted inlets, the general proportions of the model seem different than for the aircraft as actually built. The tailplane seems smaller and the aft fuselage longer - I'd have thought that these dimensions would have been fixed very early in development.
 

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Your model appears to be the Boeing 953-280 AMST proposal.

Don't forget the AMST requirements were fairly loose and the proposal limited to 50 pages, like the LWF.
 
Asuka, Japan's STOL experimental aircraftAsuka, Japan's STOL experimental aircraft
View: https://www.youtube.com/watch?v=Sz-fQnAntJE

05c966ba[1].jpg
Application:STOL research machine
Classification: Research aircraft
Manufacturer: Kawasaki Heavy Industries
Operator: National Aerospace Laboratory of Japan
First flight: October 28, 1985
Number of aircraft produced: 1
Operational status: Retired
Prototype: C-1
 

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