How does the turn rate of the F-35A/C compare with that of the F-16 and the F-18 respectively? I've read some very negative articles about the F-35 and how it compared with its predecessor models but I have no idea whether of not any of that has any merit. Obviously after reading Air Power 101 and DACT, I understand that specific instances of elder air-frames beating their replacements does not entail the end of the world for the newer fighter.
It can depend on the configuration of the aircraft. Say both aircraft are clean (that is to say, no pylons/external stores such as drop tanks, missiles etc), then there could be scenarios where say the F-16 might be at a turning advantage to the F-35. However, the reality of the situation is that this is not how air to air combat works - see, the F-16 has to bring along external stores to do its job. So everything from its turn rate to acceleration to everything else is going to be affected by the fact that, in an air-to-air configuration, it's probably going to be carrying 2-4 AMRAAM missiles, a pair of Sidewinders, and most likely a 2-3 drop tanks of fuel. All of this is carried externally, and as I said, all of it will affect the performance of the aircraft.
On the other hand, the F-35 will be capable of entering a similar situation with a much greater internal fuel load than the F-16, thus minimising the need for external tanks, along with an internal carriage capacity of 4 AMRAAMs (and I believe there's a plan to increase this capacity to 6). So the F-35 will enter the engagement with similar fuel and weapon loads, only without having to carry external stores and thus negatively impact performance. So yes, a clean F-16 might out-turn a clean F-35, but the difference is a clean F-16 is significantly limited in what it can actually do, while the F-35 can maintain performance while also carrying a useful payload.
Honestly these days it's the performance of short-range missiles that is becoming the deciding factor in any kind of dogfight. Missiles like AIM-9X and ASRAAM are moving at Mach 3.5+, and are capable of turns in excess of 40 Gs. When you consider most manned fighters are limited to 9 Gs by default, and that in a turning fight a manned fighter is certainly not going to be moving anywhere near the speeds achieved by modern missiles, "winning" really becomes a case of who shoots first, which naturally follows who sees who first. In that particular competition, I'll put my money on the aircraft with cutting edge sensor fusion and wide band signature management, regardless of who can out-turn the other. We live in an age of helmet mounted missile sights and lock on after launch capability - you don't have to get on their tail, just make sure you see them first, and let your missile do all the hard work.
This is a pretty low-quality video, but it should give you an idea of what we're talking about with these missiles, and what's called "high off-boresight" capability.
https://www.youtube.com/watch?v=KpBpzuDRt0A
I am also curious about the maximum altitude of the F-35 and how it compares to the F-16 and F-18.
Additionally, I was wondering if anyone on this thread had any information on the performance of the P&W F135 vs the GE F110 vs the F404 engines.
These questions purely pertain to the specifications and capabilities of each of the these systems.
Thank you for your time, have an excellent day.
-Guardian52
I'm not sure of the specific performance differences between the engines mentioned, though I'm sure someone on here could help. As far as maximum altitude goes for a given platform, I would be careful with publicly available numbers as I'm quite sure they're inaccurate. For example, back in the days of the F-22 fever, when it seemed as though no other aircraft would possibly do for any country looking to replace their combat jets, there were some people in the public debate who made a big deal of the F-22's publicly quoted operational ceiling of 50,000 feet. The idea was that a supercruising Raptor at this altitude could "loft" its AMRAAMs further than the F-35, which was not designed to attain supercruise and had a publicly quoted flight ceiling of (I believe) 40,000 feet.
However, a little bit of research would be quickly revealed that flight at 50,000 feet wasn't some magic trick reserved only for the F-22. In fact operational combat jets have been capable of reaching 50,000 feet for decades - the F-4 Phantom is one example, and I believe there were examples of F-8 Crusaders getting up that high. The MiG-25 and MiG-31 interceptors would have had no problem whatsoever attaining 50,000 feet, and I'm sure an appropriately equipped F-15 could do it while barely breaking a sweat.
Of course, the big difference would be the performance of the various aircraft types while at that altitude. I'm sure if you put together a series of exercises to undertake at high altitude, the results for the F-4, the F-15 and the F-22 would all look very different. How
effectively would an F-4 operate at 50,000 feet? I don't know. All I know is that the aircraft has attained that altitude repeatedly during its service life.
That was a really long winded way to say:
a) don't take publicly available figures on altitude (or anything else remotely sensitive such as missile range) as gospel.
b) context is important - there's a difference between attaining an altitude and operating effectively at that altitude.
c) I suspect the F-35 will be quite comfortable operating at higher altitudes than prior generation aircraft, regardless of information in the public domain.
d) with such a comprehensive sensor fit and the ability to deploy weapons targeted via offboard datalink, I think the F-35 will do quite a lot of its air-to-ground mission at a higher altitude than previous generations of combat aircraft. One could perhaps draw a parallel to the P-8 Poseidon, which is capable of undertaking the ASW mission at altitudes that are, compared to its predecessors, truly staggeringallel to the P-8 Poseidon, which is capable of actively pursuring the ASW mission at altitudes so far in advance of its predecessors as to be staggering.