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3d printing?I have no clue. Not sure it'd be worth making the huge mold tooling it'd take, plus the large autoclaves, just for ~75 parts.
3d printing?I have no clue. Not sure it'd be worth making the huge mold tooling it'd take, plus the large autoclaves, just for ~75 parts.
Wasn't there also an LAP study/proposal? Basically high speed, low altitude flight, similar to what the B-1B was supposed to do?
Edit: found it, although I could have been sure I read somewhere that it was supposed to be supersonic
View attachment 777885
Current automated composite layup process is actually very similar to 3D printing. Still need to cure the polymer resin under heat and pressure for strength though...3d printing?
You could maybe 3d print the mandrels to lay the composites onto, but the layup and giant autoclaves would still be needed.3d printing?
B-52 is currently planned to stay on till early to mid 2050s. A 10 year EMD and 15-20 year overall program for a 'second bomber / long range strike aircraft' is a reasonable assumption. That means that a future LRS aircraft would need to enter EMD around the late 2030s after 5-10 years of technology development. Depending on what sort of long range planning and analysis of alternatives is done for the 2050-2100 long range strike portfolio we could be looking at a very different set of attributes than a long range payload truck (B-52). I would not rule out long range hypersonic strike as a potential source of investment for a 2050+ fielding timeframe.Probably better, but that would require a new design program starting now. More or less.
I'm sorry to hear that, boss.Just pondering on the possibility of IR lamps and curing the skin on the wing itself but completely forgot the proessure side of the process.
I am in the end of life process with my cat tonight so possibly a bit distracted.
Sorry folks.
In fairness though, if that's the case, it's in large part due to the B-21 being rather vulnerable as a large, not so agile, subsonic aircraft. So if it's primary defense mechanism is being degraded in two or three decades, it will be less survivable. But even then I could see the B-21 sticking around for a long time, just focusing even further on stand off munitions. I'd be surprised if the B-21 serves less than 40 years.It is probably too early to plan for the next bomber. USAF is already hinting that B-21 might have a limited life span.
Either it could be the enlarged version of J-36 or the stretched flying wings with 6 x WS-15 turbofans. It emphasizes, long range, stealth, large payload, high supercruise, and high survivability.
Hic Rhodus, hic salta, see https://en.wikipedia.org/wiki/Hic_Rhodus,_hic_saltaRight…then we can probably start weighing different options. JASSM-XR offers twice the range (1000nmi) but is 6m+ in length, I don’t know how expensive it will be compared with the current JASSM-ERs. Would it be better settling with a shorter standoff and a faster bomber or use larger missiles on a subsonic platform (using the extended standoff to guarantee safety). Compatibility with larger missiles also enables better capacity for potential hypersonic weapons. Doing supersonic dash is also really, really bad for signature management. Afterburners of Soviet bombers could be seen from orbit in the 1980s. Would the warning time to the opponent actually increase due to this discovered by space factor instead of decrease by speed…? Could extended supercruise be a better option since we might not want to engage the burners thousands of miles from the release point…? There’s probably a lot of maths to do here…
As a fellow dedicated cat servant, my sincere well wishes and condolences.Just pondering on the possibility of IR lamps and curing the skin on the wing itself but completely forgot the proessure side of the process.
I am in the end of life process with my cat tonight so possibly a bit distracted.
Sorry folks.
In fairness though, if that's the case, it's in large part due to the B-21 being rather vulnerable as a large, not so agile, subsonic aircraft. So if it's primary defense mechanism is being degraded in two or three decades, it will be less survivable. But even then I could see the B-21 sticking around for a long time, just focusing even further on stand off munitions. I'd be surprised if the B-21 serves less than 40 years.
Blackbirds demonstrated that it's really hard to intercept a bomber at Mach 3+ and 80,000ft.I fail to see how making a larger, more vulnerable aircraft is a viable alternative. People here are talking about a four engined supersonic monster; I cannot fathom how that would be a survivable option. If you are thinking that a bomber can outrun the threat, I think you are operating in the wrong century.
Missiles also get much much faster nowadays though…Blackbirds demonstrated that it's really hard to intercept a bomber at Mach 3+ and 80,000ft.
However, that comes with a side order of an IRCS the size of the rising sun. And going hypersonic makes that IRCS even worse.
It'd be an interesting discussion to see if you could do low-RCS Mach 2.2 at 70,000ft+. It'd still have issues with IRCS, but no aircraft has the ability to precisely track an IR signature at range.
The attached file shows the rather dramatic improvement in down and cross ranges you get from launching an AGM-69 SRAM at different heights and speeds.
View attachment 777975
This came from Lockheed in parts of the Blackbird development. I believe that the comparisons are against a B-52 down on the deck and a B-58 at M1.6.
Well if I am getting your point correctly… I am not trying to prove that high speed bombers are viable or unviable, just listing out the advantages and disadvantages and alternatives to it that can be analyzed together… I think analyzing this problem holistically is wayyyy too complicated for me…Hic Rhodus, hic salta, see https://en.wikipedia.org/wiki/Hic_Rhodus,_hic_salta
SAMs and AAMs not so much.Missiles also get much much faster nowadays though…
IMO speed and bombload for survivability are most useful in the naval context? If you're part of a strategic air campaign then you'll have escort, so speed is useful but not crucial.Right…then we can probably start weighing different options. JASSM-XR offers twice the range (1000nmi) but is 6m+ in length, I don’t know how expensive it will be compared with the current JASSM-ERs. Would it be better settling with a shorter standoff and a faster bomber or use larger missiles on a subsonic platform (using the extended standoff to guarantee safety). Compatibility with larger missiles also enables better capacity for potential hypersonic weapons. Doing supersonic dash is also really, really bad for signature management. Afterburners of Soviet bombers could be seen from orbit in the 1980s. Would the warning time to the opponent actually increase due to this discovered by space factor instead of decrease by speed…? Could extended supercruise be a better option since we might not want to engage the burners thousands of miles from the release point…? There’s probably a lot of maths to do here…
but RE: SR-71 survivability, it was pretty solidly in the SA-5 engagement envelope, if memory serves. I should have some graphics on my laptop.
With the speed and height the launch crews had to be perfectly positioned. The slightest turn and throttle change would put the Blackbird outside the engagement envelope by the time the missile arrived at 80,000ft.I'm on mobile and can't figure out how to insert quotes while editing, but RE: SR-71 survivability, it was pretty solidly in the SA-5 engagement envelope, if memory serves. I should have some graphics on my laptop.
I have a rather pessimistic view towards high speed aircraft avoiding infrared satellite detection though... Infrared technology came a really long way since the DSP era: using staring array instead of scanning linear array alone improves detection SNR by hundreds of folds, because each pixel on the sensor exposes for about the time of the entire frame without needing to scan across it. The advent of LEO constellations would further improve the SNR by the square of the distance reduced, potentially giving thousands of folds in SNR improvement...When it comes to slow walkers, I feel like modern engines could ameliorate that, be it through supercruise, improved fuel blends/engine design (Tu-22M/NK-25 burns very distinctly), or arcane signature management techniques.
30-60min of dash at Mach 1.5 means only 750-1500km in dash range, it seems that improving missile range by that much (JASSM-ER to -XR) might be the easier option since the launcher only needs to drop the missile and go instead of start dashing. Also Su-27 might not be a representative threat for future interceptors... Setting J-36 as the representative threat, I would expect at least F-22 level of super cruise capability with tanker support for the reach, paired with 300-400km range missiles (PL-17).In terms of the kind of fashion you're looking at, I was back of the napkin looking at like 30-60min of dash before launch, I can't remember the details but it indicated that non-barrier CAP, even with Su-27's range and speed, would struggle to intercept just on geometry. It's been a minute though.
The Earth's curvature limits the maximum line-of-sight detection range from a 40kft radar to a 40kft target to be ~700km. Any longer than that you probably have to base the sensor forward no matter how advanced the datalink is. Then the sensor becomes a huge target that can be disabled first. Of course the sensor can also be space-based, I guess war is going to be really different once both sides have all-seeing, real time targeting LEO constellations...Finally, the concern about enemy missile range is the advent of quite advanced datalinks. I'll point out that BOMARC was doing like 500-700nmi (iirc) intercepts in 1961, so these kinds of stand off aren't exactly unprecedented.
I've heard from others in the community that Shul is a PNG? On the other hand, the issue with "needs to be perfectly placed" is that you can do that more easily if you know where they're going (because you know the targets).With the speed and height the launch crews had to be perfectly positioned. The slightest turn and throttle change would put the Blackbird outside the engagement envelope by the time the missile arrived at 80,000ft.
IIRC it was Brian Shul who said that Blackbird SOP was to turn slightly and push the throttles up when the missile warning system reported a launch.
And then promptly die from sticker shock, ensuring that the proposed systems never get built.I also took that to mean that the customer thinks there is operational value in going higher than Mach 5. For me this maybe hints that in a world where everyone can see you coming, systems that require a hugely sophisticated AD network, near perfect execution and probably some non trivial luck to defend against seem like a good, if someplace obvious, place to explore solutions.
Thing is, the range and cross-range boost you get from starting a weapon comparable to SRAM at M3 and 80,000ft is such that the SA-5 base needs to be some 500nmi/1000km uprange of the target to be able to intercept the bomber before weapons separation.On the other hand, the issue with "needs to be perfectly placed" is that you can do that more easily if you know where they're going (because you know the targets).
SA-5 was designed with XB-70 as the reference threat. IIRC the envelope was fairly substantial (80-160km iirc) even for 35km and 1200m/s. It's a pretty known quantity these days, and is part of why SRs used side looking sensors and didn't overfly the USSR. The flip side is that an SA-5 site is the size of a small town, and about the same population, but it's workable.
Fully agreed here.Anyway, to stay on topic, just altitude and range aren't the magic ticket for the future. It helps, but networked Radars that can forward pass missiles and a host of other things mean that I think a mix of speed, stealth, and a big defensive tool kit are the path forwards.
I've heard from others in the community that Shul is a PNG? On the other hand, the issue with "needs to be perfectly placed" is that you can do that more easily if you know where they're going (because you know the targets).
SA-5 was designed with XB-70 as the reference threat. IIRC the envelope was fairly substantial (80-160km iirc) even for 35km and 1200m/s. It's a pretty known quantity these days, and is part of why SRs used side looking sensors and didn't overfly the USSR. The flip side is that an SA-5 site is the size of a small town, and about the same population, but it's workable.
Anyway, to stay on topic, just altitude and range aren't the magic ticket for the future. It helps, but networked Radars that can forward pass missiles and a host of other things mean that I think a mix of speed, stealth, and a big defensive tool kit are the path forwards.
Sure, SR-71/SRAM would have been quite a monster, but it's also not impossible to work up an interceptor / SAM force that could work against it. On the other hand, this is why I really want SRAM-3! Or SRAM-2-2?And then promptly die from sticker shock, ensuring that the proposed systems never get built.
Thing is, the range and cross-range boost you get from starting a weapon comparable to SRAM at M3 and 80,000ft is such that the SA-5 base needs to be some 500nmi/1000km uprange of the target to be able to intercept the bomber before weapons separation.
It forces the defender to install SA5 sites ~50km apart at something like 600nmi/1200km from the targets and fire enough missiles to ensure that one or two will still be within envelope while the Blackbird bomber makes their turns. How expensive is an SA5 site? How many missiles are needed to successfully engage like that?
What happens when you take a weapon like HACM or ARRW, that have a 1000+km range from a subsonic launch at 30-50kft, and launch them fast and high? How much range does that add? Let's be nice and say it only doubles the range, instead of being an order of magnitude improvement like with SRAM.
Now that ring of SA5 sites every 50km needs to be at least 1200nmi/2400km out from the targets to engage the bombers. Or you're reduced to shooting SA5s at individual missiles.
Fully agreed here.
Sure, SR-71/SRAM would have been quite a monster,
You mean ASALM?this is why I really want SRAM-3! Or SRAM-2-2?
You mean ASALM?
No, I mean SRAM-type, which (more or less) fits in the F-35A/C bay and could probably be a quite aggressive aeroballistic these days...You mean ASALM?
IIRC, ASALM was not significantly bigger than SRAM. It may have been wider/deeper, but it still fit into more or less the same "1/8 of a CSRL" slot.No, I mean SRAM-type, which (more or less) fits in the F-35A/C bay and could probably be a quite aggressive aeroballistic these days...
You won't get anything like the same improvement from an air-breather - and that's assuming a high speed/high altitude launch doesn't just melt the thing.What happens when you take a weapon like HACM or ARRW, that have a 1000+km range from a subsonic launch at 30-50kft, and launch them fast and high? How much range does that add? Let's be nice and say it only doubles the range, instead of being an order of magnitude improvement like with SRAM.
The A-12 family was always weird for that kind of thing, presumably in part because of classification.If it had gone into production the aircraft's tri-services designation would've been the B-12A.
SRAM didn't go on the CSRL, and I'm more interested in sticking it in the slot of a 2000lbs JDAM...IIRC, ASALM was not significantly bigger than SRAM. It may have been wider/deeper, but it still fit into more or less the same "1/8 of a CSRL" slot.
Or ASALM. Faster than SRAM with more range than SRAM 2. And also would have worked from the Blackbird.Sure, SR-71/SRAM would have been quite a monster, but it's also not impossible to work up an interceptor / SAM force that could work against it. On the other hand, this is why I really want SRAM-3! Or SRAM-2-2?
How much could the blackbird based bomber have carried?
IIRC the proposed B-12A would've carried four SRAM As.
Which is a pretty pitiful payload.