The cost of the F-22 is 146.4 million dollars apiece (2009), the maximum weight is 34571 kg, the price is 4235 dollars per kilogram.
Its entirely Impossible to answer to that question today.More expensive than FCAS from France & Germany?
This...Or maybe it's a bullshit metric, and people should stop trying to sound smart.
The cost of the F-22 is 146.4 million dollars apiece (2009), the maximum weight is 34571 kg, the price is 4235 dollars per kilogram.
Its entirely Impossible to answer to that question today.
You know, I think you're right about the greater volume.... and GCAP will be lot more affordable. Might even be produced in greater volume.
F-22 went from first flight in 1997 to IOC in 2005, 8 years. That's strictly the F-22, not counting YF-22 development on the grounds that prototypes of the F-47 have already flown. YF-22 first flew in 1990, so 15 years from the fly-off to IOC.How long will it take for the F-47 to become operational, given that next year will mark 10 years since the T-7A first flew and the IOC deadline has been set for fiscal year 2027 after many delays (and will likely be postponed again)?
Plus however many GCAPs get sold to other buyers, like Australia, Saudi, etc.
The Saudis have already approached GCAP office about buying in, though.Australia and Saudi Arabia, if they purchase 6th gen, will almost certainly purchase American. That is a political decision first and foremost, and their relationship with the US is more important than with the UK, Italy, or Japan.
I suspect that Israel would rather buy F/A-XX than F-47, since the F/A-XX actually has a designed in long-range strike mission. Or FCAS, since we know the French will design it as primarily a striker.Same with Israel, the UAE, and Qatar.
India is still more closely linked to Russia than UK.India is a possibility for GCAP, as India is not as close with the US.
Like UAE and Qatar, I suspect that which plane they want depends on what capability they want primarily. I think Poland in particular is going to want air superiority more than strike.Some European nations, like Poland, might be a tossup.
Assuming 1:1 replacement of Typhoon, UK and Italy would equal that, and assuming 1:1 replacement of F-15J you're looking at a total run of nearly 500, just for the 3 prime partners. Plus however many GCAPs get sold to other buyers, like Australia, Saudi, etc.
And in the case of the F-15, it was less than four years between 1972 and 1976....F-22 went from first flight in 1997 to IOC in 2005, 8 years. That's strictly the F-22, not counting YF-22 development on the grounds that prototypes of the F-47 have already flown. YF-22 first flew in 1990, so 15 years from the fly-off to IOC.
True but those early F-15s were extremely limited in capabilities, I understand.And in the case of the F-15, it was less than four years between 1972 and 1976....
The A models were also replaced almost immediately by the C model. All A essentially went to Guard units as C's were delivered.True but those early F-15s were extremely limited in capabilities, I understand.
There's nothing wrong with a joint CATOBAR/CTOL platform, just leave the damn STOVL out of it this time.This is starting to sound like another joint platform. I may be wrong
There's nothing wrong with a joint CATOBAR/CTOL platform, just leave the damn STOVL out of it this time.
Except that the two services want different design focuses. Just like the F-111. Well, inverse desires for the branches: this time the USAF wants the monster air superiority fighter while the Navy wants a heavy striker. But those are still two very different, incompatible design focuses.There's nothing wrong with a joint CATOBAR/CTOL platform, just leave the damn STOVL out of it this time.
That would be ideal if it can actually fit LREW in a weapon bay. Only then would we have something with a NEZ comparable to the longest range PLA missiles.assuming 6x LREW at 1000lbs each and 2x AMRAAM/JATM at ~375lbs each
I'm assuming that the F-47 was designed to be able to fit LREW length-wise into the bays, just like I'm assuming the FAXX will be designed to fit AIM-174Bs into the bays.That would be ideal if it can actually fit LREW in a weapon bay.
I would assume LREW is no longer than JASSM.... I doubt that the internal carrige of AIM-174Bs is a hard requirement for FAXX.I'm assuming that the F-47 was designed to be able to fit LREW length-wise into the bays, just like I'm assuming the FAXX will be designed to fit AIM-174Bs into the bays.
Poor example, F-111 was a bomber, you can't easily make it a naval air superiority fighter.Except that the two services want different design focuses. Just like the F-111.
The end of the Cold War ended a lot of funding.Not if the platform is supposed to be a no-compromise air superiority fighter. The last time they tried this (ATF/NATF), it didn't go well.
It is ridiculous. How much does software weigh??I'm amazed that cost per kilogram is now a useful metric for determining aircraft usefullness.
Or maybe it's a bullshit metric, and people should stop trying to sound smart.
Hmmm...really?But land-based aircraft cannot be navalized!
The examples you gave are all propeller planes or early jet planes. Why did the F-111B fail? Why did the JSF project rely on carrier-based requirements from the beginning? Why are ATF and NAFT so different? Considering the geographical environment of the United States, the navy is much more important than the air force! In addition, the USAF has a history of directly using Navy aircraft.Hmmm...really?
Sea Gladiator, Sea Hurricane, Seafire, North American FJ Fury series...
There is absolutely an argument to be made that the F-111 mostly failed due to the Navy simply not wanting it.The examples you gave are all propeller planes or early jet planes. Why did the F-111B fail? Why did the JSF project rely on carrier-based requirements from the beginning? Why are ATF and NAFT so different? Considering the geographical environment of the United States, the navy is much more important than the air force! In addition, the USAF has a history of directly using Navy aircraft.
Also, there are many USAF aircraft that have no equivalent in the USN - e.g. heavy bombers, large transports, etc etc. So again your arguments are flawed unless one uses an extremely narrow focus.Considering the geographical environment of the United States, the navy is much more important than the air force!
And arguably it gave what was originally asked for.There is absolutely an argument to be made that the F-111 mostly failed due to the Navy simply not wanting it.
My point also briefly explains why modern land-based warfare cannot be easily navalized! Please answer my question directly!My point was simply to counter your blanket statement that "land-based aircraft cannot be navalized".
So now you are adding in the "easily" qualifier. What's next?My point also briefly explains why modern land-based warfare cannot be easily navalized! Please answer my question directly!
The Navy has C-2, A-3/A-5/A-6. In particular, the A-6 earned the title of the small B-52 in the Vietnam War due to its high efficiency. How will the Air Force develop its role when all the front-line bases are destroyed by China?Also, there are many USAF aircraft that have no equivalent in the USN - e.g. heavy bombers, large transports, etc etc. So again your arguments are flawed unless one uses an extremely narrow focus.
Because I didn't expect you to use propeller fighters and early jets as examples, how ridiculous. The fighters of the 21st century are neither propellers nor early jets.So now you are adding in the "easily" qualifier. What's next?
That's a long discussion already addressed elsewhere eon this forum. Besides, as written above, one could argue that it didn't fail against what was originally asked from it. However, requirements changed.Why did the F-111B fail?
Well, if you are designing a new platform from scratch, as was the case with the F-35, of course you are going to include all the requirements from all key the users. That is a different from the argument you are trying to make re converting Air Force designs.Why did the JSF project rely on carrier-based requirements from the beginning?
Studies were done for navalized Typhoon too.Mig-29, Su-27, Gripen. Was the KN-21 and J31 designed as carrier fighters initially?
As a Chinese, I can tell you very clearly that the J-35(older model J-31) is originally a naval project, and the PLAF chose to join it only after seeing the success of the Navy.Mig-29, Su-27, Gripen. Was the KN-21 and J31 designed as carrier fighters initially?
Are the requirements for F/A-XX and NGAD the same? Each F-35 (except the F-35B) needs to carry two 2,000-pound bombs, each F-35 must be equipped with EOTS, and the approach speed requirements for the F-35C are all proposed by the USN. If modern fighters were so easy to navalize, France would not have withdrawn from the EF-2000 and made its own Rafale fighter. I think you are familiar with the naval design of the Typhoon fighter. I think you are also familiar with how difficult it is to operate the Su-33 on an aircraft carrier.That's a long discussion already addressed elsewhere eon this forum. Besides, as written above, one could argue that it didn't fail against what was originally asked from it. However, requirements changed.
Well, if you are designing a new platform from scratch, as was the case with the F-35, of course you are going to include all the requirements from all key the users. That is a different from the argument you are trying to make re converting Air Force designs.