trajan
ACCESS: Confidential
- Joined
- 23 October 2020
- Messages
- 149
- Reaction score
- 266
ANOTHER MIG25 momentsU.S. House to open questioning session on Air Force on December 27th(
HELL!WHY NOW!
ANOTHER MIG25 momentsU.S. House to open questioning session on Air Force on December 27th(
HELL!WHY NOW!
de Havilland too?Trijets had some history. Some of it was overwater. But there was also United's "Denver rule": the ability to reach either coast out of Denver on a hot day. East was just a long way and a heavy take-off, West was minimum safe altitude over the Rockies if you lost an engine.
As for this thing... could be a lot of reasons.
Well is it more of a YF-22 or first EMD flight of F-22 in 1997? it looks like the latter to me just by the radome alone. Just as with the J-20/J-35 there will be many tweaks and mods they will do to it as testing and maturation happens before they settle on a final designI wouldn't bet on it being a tech demonstrator. J-10 and J-20 were both prototypes reasonably close to production configuration.
That statement really is not aging well...
what is the source for that?U.S. House to open questioning session on Air Force on December 27th(
HELL!WHY NOW!
Me too. Three holes at the back = Foz thinking.
What were the arguments/reasons for trijets?
Dual mains and nose like the Su34, so I suspect it's more of a striker than an air-to-air monster (Su27/F-15 analogue).
Agreed.wing area 95 m2
volume 75 m3
volume of weapon bay 16.3 m3 (20%)
3 RD-33 x 9500 kgf = 28500 kgf
maximum take-off weight 45 tons
the most likely role is a front-line bomber, an analogue of the Su-34
Yes, it's pretty clear that there's 3 engines on that beast.Could the top intake be for the middle engine? A more advanced engine might still be in development and the third engine will only be used for the demonstrator? I don't think this is likely as it would require a redesign of the internal structures and would likely negate whatever data that was gathered in the test program.
This thing should be nicknamed Mothra.
I would not want to go anywhere near Guam in a plane with all the defenses there.I think we can agree on cruiser; I am just not seeing why air targets would justify such a long ranged design. That would be a lot of effort to kills some E-2s, or alternatively pick a fight with tankers near Guam. Why would range be necessary over Japanese or Philippine islands, let alone Taiwan?
That was a very non-useful design, the bomb tended to get carried along in the wake of the plane, for an unpredictable distance. While that can be addressed with guided bombs these days, it's very clear that the plane has 3 engines.
It's easier to add an engine than get more thrust (reliably) developing a new engine. New engines always have teething problems. So if they are just looking for more thrust on a short timeline, it's relatively easy to produce three engines that are mature than tie yourself to new engine production if it isn't ready.The 3 engines deal is really puzzling, is it because two engines are not powerful enough? Why is the nose so thick, is it a side by side cockpit like the su-34? Are those glass pieces windows? Or sensors??
That's one hell of a redesign, though...It's easier to add an engine than get more thrust (reliably) developing a new engine. New engines always have teething problems. So if they are just looking for more thrust on a short timeline, it's relatively easy to produce three engines that are mature than tie yourself to new engine production if it isn't ready.
Might have started with a twin and said, that won't cut it and we don't want to wait until engine-X is ready. Let's keep the bays for 1 & 3 sized to fit engine-X if it's ready, and in the meantime, let's start producing it with three of these engines we're comfortable with.
That's my guess anyway.
Here's a nice counter argument for you guys:Dual mains and nose like the Su34, so I suspect it's more of a striker than an air-to-air monster (Su27/F-15 analogue).
There may be other advantages. Like the ability to "distribute" air intakes along the top and bottom of the plane, thus reducing RCS for each in general.It's easier to add an engine than get more thrust (reliably) developing a new engine. New engines always have teething problems. So if they are just looking for more thrust on a short timeline, it's relatively easy to produce three engines that are mature than tie yourself to new engine production if it isn't ready.
Might have started with a twin and said, that won't cut it and we don't want to wait until engine-X is ready. Let's keep the bays for 1 & 3 sized to fit engine-X if it's ready, and in the meantime, let's start producing it with three of these engines we're comfortable with.
That's my guess anyway.
size of intakes does not scale relatively to RCS as long as the engine is well hidden. Having breakage in your skin will hurt surface radar waves management and contribute to larger RCS. You want all your intakes to be either all below or above depending the operating altitude so that the smooth skin surface can be shown to enemy radars.There may be other advantages. Like the ability to "distribute" air intakes along the top and bottom of the plane, thus reducing RCS for each in general.
The Boeing 988-123 is detailed in a NASA report linked to in this thread. You will find it is designed to be a highly manoeuvrable strike aircraft designed for a joint force customer (USAF and USN).
Given how all stealth ultimately aims for hopeless diamond (while hopefully be still flying), VLO world will be probably about as diverse as world of WW1 bolt action rifles.Incredible that if we remove one engine and cut off the "neck" of the SAC J-XD planform, we can arrive at this design that Boeing thought out... 20 years ago! Convergent engineering indeed.
View attachment 753832
The air intakes are mysterious too why go to F-22 style intakes when the J-20 has the F-35 intakes? I wonder also if the new aircraft features S-shaped ducts to hide the engines? I suppose only time will tell.
Yep. Ultimately SAMs and radars and whatnot works the same way for everyside, so the method for avoiding detection stays the same.Given how all stealth ultimately aims for hopeless diamond (while hopefully be still flying), VLO world will be probably about as diverse as world of WW1 bolt action rifles.
With the strake / LERX above then a F-35 or J-20 style DSI intake simply wouldn't work because it diverts the boundary later in two directions but the top one of them is blocked off here, so the flow would end up being ingested by the intake. Hence a more traditional Super Hornet style double diverter Caret intake.The air intakes are mysterious too why go to F-22 style intakes when the J-20 has the F-35 intakes?
Maybe the DSI has a bleed area somewhere along the bump?With the strake / LERX above then a F-35 or J-20 style DSI intake simply wouldn't work because it diverts the boundary later in two directions but the top one of them is blocked off here, so the flow would end up being ingested by the intake. Hence a more traditional Super Hornet style double diverter Caret intake.
But then now you run into problems at low speed being just a flying wing with no horizontal or vertical tailsBrute force supercruise? But then why not make it longer and more slender?
My gut feeling is this is something conceptually like the Sukhoi T-60 but designed with a greater understanding of stealth, but then I can't see the need for three engines. T-60 made do with 2 AL-31F for 60,000kg class aircraft. Maybe 3 x WS-19?
View attachment 753834
That perfectly describes what SAC design is now.But then now you run into problems at low speed being just a flying wing with no horizontal or vertical tails
I believe the Xi’an thing turn out to be AWACS Y-20 that flew earlier today. Since I heard the original rumour stated that XAC will fly something, just not what people expected. With how excited people for H-20 this would fit the bill*spills drink ...AGAIN* What ?! 3 of them? Is that was Xian was rumoured from knowledgeable folks to fly too? Mao almighty...
Check ngad thread, everything is here.Them side looking radars kinda point to air to air role
As for 6gen we haven't got any definition as to what defines 6th gen .
Huitong on J-XDS (Shenyang)During the 2000s a medium size/medium range supersonic stealth fighter bomber concept (JH-XX? Project 176?) was studied by the 601 Institute. It featured a tailless swept wing design with a twin seat cockpit. A mock-up (head section?) was constructed at SAC during 2013. A recent rumor (August 2022) suggested that the JH-XX project might have progressed into the prototype manufacturing stage at SAC. The latest images suggested that another new 6th generation fighter prototype besides J-36 (see above) flew for the first time on December 22, 2024 over the sky of Shenyang. The aircraft appears more like a multirole stealth fighter (J-XX) rather than a traditional fighter bomber. It features tailless "lambda" shaped swept wings with two movable tail fins with adjustable slant angles, depending on the flight situations of the aircraft. This "adjustable tail fin" design has two main positions: the "horizontal" position allows J-XX to achieve maximum stealth and minimum drag, while the "vertical” position allows J-XX to achieve maximum maneuverability. J-XX also features two DSI engine intakes underneath the wings with an internal weapons bay in between. An EOTS is installed underneath the nose. The aircraft could be powered by two WS-15 turbofans, but it is unclear whether they have TVC nozzles or not. Compared to J-36, J-XX appears slightly smaller but is also capable of flying various air-to-air and air-to-ground missions. Currently it is unclear whether J-36 and J-XX will enter the service with PLAAF together or they will compete against each other.