FighterJock
ACCESS: Above Top Secret
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Wonder how soon is soon if the in service date is sometime in the 2030s for the F/A-XX?
CR's are temporary. If you are suggesting that we will be in continuous CRs for the rest of the decade then that is really not something that is going to happen. CR's cause delays and mess up new starts and other programs have to wait to ramp up as they can only be funded to previous FY levels when under CR. That doesn't mean that as administrations submit their budgets they have to honor FYDP funding profiles stated in their previous budgets. As I wrote earlier, if admin or service wishes to prioritize something based on where it is at in its analysis, it can dramatically alter the funding profile in the FYDP relative to what might have been in the out years as per the last 2-3 budget docs.Happy to be corrected but I think continuing resolutions mean no funding increase can occur and the previously agreed budget just carries forward. It also limits the ability to start new programs or change funding limits and levels.
I was thinking more in terms of a lower cost / less risky propulsion EMD program that is based on more mature technologies from a tech and mfg. readiness level. So a new clean sheet engine, just not one that blows budgets and assumes a lot of risk with untested or relative immature technology. Though certainly adapting something off the shelf could be an option. It really depends how big FA-XX will be and what the Navy wants in terms of performance.What are you thinking, a further enhancement of the F414 or perhaps another in service engine such as the F135? The F135 feels maybe not quite big enough as a single and two likely too big for a carrier capable aircraft.
NAVY $22.7 billion in research and development funding, you can find 1 billion for FA/XXTell me about this “black budget” you speak of
No I'm not expecting CRs but I am expecting that there will be a continued cap on defence spending similar to the Fiscal Responsibility Act.CR's are temporary. If you are suggesting that we will be in continuous CRs for the rest of the decade then that is really not something that is going to happen. CR's cause delays and mess up new starts and other programs have to wait to ramp up as they can only be funded to previous FY levels when under CR. That doesn't mean that as administrations submit their budgets they have to honor FYDP funding profiles stated in their previous budgets. As I wrote earlier, if admin or service wishes to prioritize something based on where it is at in its analysis, it can dramatically alter the funding profile in the FYDP relative to what might have been in the last 2-3 budget docs.
While that is probably the lower risk approach I feel like the requirement for range makes an AETP derived engine a better option. The other issue is cost. Your suggestion is likely lower cost and we know the XA100/101 were not cheap and 102/103 likely the same. Even if GE or PW started today on a clean sheet new engine the timeline would be very close for IOC of the aircraft so timeframe might also be difficult.I was thinking more in terms of a lower cost / less risky propulsion EMD program that is based on more mature technologies from a tech and mfg. readiness level. So a new clean sheet engine, just not one that blows budgets and assumes a lot of risk with untested or relative immature technology. Though certainly adapting something off the shelf could be an option. It really depends how big FA-XX will be and what the Navy wants in terms of performance.
What I want to say is with a budget of 22.7 billions of research the Navy can find one billion for the FA/XX program, if they are in source selection they have the idea of want they want and how to fund it.$1 billion for F/A-XX dark sidius? Is that for the overall program?
Spending CAP's are on topline. Within that topline, the department and services are free to prioritize as they see fit. If the very top of the USN leadership is speaking about source selection and competition with follow on development, they would at least be willing to make the necessary changes to fund those wishes including seeking civilian approval. Or their program is less ambitious and requires significantly less funding through EMD compared to a high end 6th gen PCA the air force might have been considering.No I'm not expecting CRs but I am expecting that there will be a continued cap on defence spending similar to the Fiscal Responsibility Act.
Agreed, however in that context it would be the AF trying to explain to Congress why this is a bad idea (for all the reasons you stated). The Navy wouldn't be in that position, they can say "This platform best suits our requirements, and if the AF were to increase the buy, that would be fine with us." Because I don't think that Congress would merge the programs, but would instead force one service to buy the same fighter that the other one did, and the Navy's trying to get out ahead of that while Kendall tries to figure out exactly what it is he wants.If Congress tries that, the Navy gets to say "With all due respect, Senator, the only time that worked is when the USAF bought aircraft designed for the Navy. USAF needs a lot more range, our airfields move and theirs don't. But we also have pretty hard limits on how big a plane can be and still take off and land from a carrier."
And then gets to say that FAXX is limited to ~85,000lbs MTOW and a landing weight with full weapons and minimal internal fuel of ~55,000lbs. While the USAF's published wish list for range means an aircraft that is closer to 105,000lbs max takeoff.
The Black Budget is great for small, relatively cheap, relatively discrete projects - a few RQ-180s, 59 F-117As, etc. but also comes with drawbacks and limitations. (Look back to why the originally 'black' PWIII didn't fit the 'black' F-117A's weapons bays).Thanks dark sidius, the Black Budget and it's mysterious ways of operating. That is where the NGAD F/A-XX should belong like the F-117A Nighthawk back in it's early days when it was classified as a SAP Level 1 program.
Why does the USAF not do a Joint program with the US Navy in the first place and share some of the technology that would go into the NGAD F/A-XX designs, if the Air Force is getting serious about saving money then that could be the way forward. A common design with shared technology would be beneficial for both services, at least that is what I am currently thinking about right now.
Can the Air Force make its next-gen fighter jet cheaper than the F-35?
The Air Force wants to keep its next-generation fighter jet affordable without sacrificing capability. Some analysts warn it can't be done.www.defensenews.com
I expect that this will end up similar to the F-22 and F-35 dynamic. For NGAD to really be 6th gen it has to push some boundaries, similar to what the F-22 did. Then a few years later the F-35 came along and used all the lessons learned to make an affordable platform that in many respects is superior to its 5th gen sibling.Can the Air Force make its next-gen fighter jet cheaper than the F-35?
The Air Force wants to keep its next-generation fighter jet affordable without sacrificing capability. Some analysts warn it can't be done.www.defensenews.com
I mentioned this once before, but at some point the DOD will build a super AI for research and development. It will be trained on centuries of military procurement history. As such, it will determine that the only sensible thing to do is to stop all new system procurement indefinitely, as by the time any new system comes out, there is already new research that can be used for new systems. The AI will recommend that we complete all possible research and development first, and build the ultimate weapon once there is nothing else to learn about the universe.At some point though, I do agree with the notion that you have to stop analyzing and just build a damn aircraft before the concept is studied to death. And if nothing else, I think that we should not allow the propulsion systems to stagnate.
I mentioned this once before, but at some point the DOD will build a super AI for research and development. It will be trained on centuries of military procurement history. As such, it will determine that the only sensible thing to do is to stop all new system procurement indefinitely, as by the time any new system comes out, there is already new research that can be used for new systems. The AI will recommend that we complete all possible research and development first, and build the ultimate weapon once there is nothing else to learn about the universe.
USN can get what it wants in time by measuring it's wishlist.
Making sorta twin f-35 with long loiter/dash, more range and decent oversized/bringback capability is not too dissimilar from f-18e program though.USN asked for a stealth fighter for Xmas, got the F-18E.
Let's be realistic about what the Navy asks for and what it actually gets.
Makes sense with their funding issues and priorities to down select to a single vendor. Perhaps more risk given earlier selection and all three primes competing have indicated they won't sign fixed price contracts so there is wiggle room ahead for whoever wins.The FAXX funding profile with an early down-select for the base contract may be feasible within the Navy near-term budget realities. Under this plan, the big $$$ ramp-up for EMD is deferred until FY27 and beyond.
An evolved F-35 was always one of the options for F/A-XX but I am inclined to believe it will be more than that. I couldn't see NG staying in if they believed an evolved F-35 was viable given it will cost a lot less than what Boeing and NG would have to build. If it is an option makes you wonder if LM will propose two options, an evolved F-35 and an all new airframe?No time for major engine or advanced avionics development in this scenario, so it seems reasonable to assume that FAXX will be wrapped around F-35 Block 4+ and utilize a derivative turbofan, not NGAP.
I'm thinking less "F-35F Super Lightning" and more "new airframe using most of the F-35 avionics and a pair of F135 engines"An evolved F-35 was always one of the options for F/A-XX but I am inclined to believe it will be more than that. I couldn't see NG staying in if they believed an evolved F-35 was viable given it will cost a lot less than what Boeing and NG would have to build.
I think the range demands are too high for FAXX, but if the USN is stupid enough to make a stretched F35 an option they're going to get it.If it is an option makes you wonder if LM will propose two options, an evolved F-35 and an all new airframe?
At what point though does the aircraft become too big to land on the carrier? If I read it correctly the Advanced Arrestor gear on the Ford class is capable of up to 70k lbs landing weight and the Mk7 was around the 60k lbs mark. Super Hornet had a max landing weight of 42k lbs so there is clearance for the F/A-XX to increase in size if necessary. I think the F-14 was the heaviest fighter to land and that was maxed at 54k lbs.I'm thinking less "F-35F Super Lightning" and more "new airframe using most of the F-35 avionics and a pair of F135 engines"
The oft mooted delta winged F-35E postulated here may have the range required but perhaps not the rest of the package needed to make it a 6th gen aircraft. Might also have a very high landing speed.I think the range demands are too high for FAXX, but if the USN is stupid enough to make a stretched F35 an option they're going to get it.
If a current in service engine then reusing the F414 in the EPE variant makes sense. Navy already knows and is very happy with the engine, it is significantly lighter than the F110 and I expect they will be able to, with five years of concerted dev effort, get the thrust and durability close to the F110-129. Would also be a good export market for GE given that engine size has been popular on non US fighters.Perhaps an aircraft designed around two F110 derivatives may be more appropriate in size, especially as the base engine is quite mature and currently in production which reduces risk and cost, and can also leverage commercial CFM56 developments to improve performance and efficiency. Such a engine would not be optimized for supercruise speeds that the F-22 was designed for, but the Navy has traditionally placed a greater emphasis on loiter, so it may not be too big of a concern.
Twin f-119 projects (NATF, A/F-X, evolved tomcats) were norm, and they were by no means borderline. Maybe even swing wing, haha.A low risk approach that makes use of F-35 Block 4 mission system components (radar, EW, etc.) would make sense, but I think an airframe using two F135s may be too large.
Did somebody say twin F135s?if USN satisfied off-the-shelf components, just need bigger stealth aircraft. There is a possibility for F135 X 2 engined stealth fighter-bomber.
Did someone say "isn't there meant to be a radar in the nose?"Did somebody say twin F135s?
IIRC the catapults max out at 85-90k, and I was assuming that ~55k is the effective max for the arresting gear. Because most of the USN carriers are still Nimitz class, so we need to design to those limits, not the Ford limits.At what point though does the aircraft become too big to land on the carrier? If I read it correctly the Advanced Arrestor gear on the Ford class is capable of up to 70k lbs landing weight and the Mk7 was around the 60k lbs mark. Super Hornet had a max landing weight of 42k lbs so there is clearance for the F/A-XX to increase in size if necessary. I think the F-14 was the heaviest fighter to land and that was maxed at 54k lbs.
Did someone say "isn't there meant to be a radar in the nose?"
I suspect that there is an AESA radar in there, gone are the days of the big radome nose on traditional fighters.
It got coal for Xmas that year.USN asked for a stealth fighter for Xmas, got the F-18E.
Let's be realistic about what the Navy asks for and what it actually gets.
Agree but I expect there is some fat so close to 60k for the Mk7 should be doable.IIRC the catapults max out at 85-90k, and I was assuming that ~55k is the effective max for the arresting gear. Because most of the USN carriers are still Nimitz class, so we need to design to those limits, not the Ford limits.
Was thinking though if you are going F135 size why then go F135, you might as well use the XA100/101. More expensive again than the F135 but you would design the platform to make full use of the adaptive advantage. That is a step change in range. The timeframe to productionise that engine would be suitable for F/A-XX.But a pair of F135 engines means that the T:W ratio is dang close to 1:1 at takeoff. (where's the evil grin emoji on this forum?)