Given its need to get low, it does not surprise me that it has so many flare dispensers.
Wrong thread mate. This is the “USAF NOT F-35 Thread”
That one may be a USAF bird, but here is one where you can clearly see “VF-14”

Here is info on the USAF bird
’57th FIS F4E 66-0304 that took off, flew and landed safely with wings folded, August 1, 1978. PIlot: Capt. Greg Harrison; WSO: Capt. Denny Dawson. Photo taken with an Instamatic by WSO lst Lt. Jim Uken flying in 66-328. The F4 became pitch sensitive at 205 kts, so Harrison landed at 230 kts. Wing fold locking nuts retracted, lock indicator pins fully extended. But the F4 had just been painted gray & the pins, which should be red, were also painted gray no one noticed they were extended.’

To end the OT digression
My bad for helping to lead the topic off point.
communication and netcentric capability
Um, those are not sensors and they won’t help you if it’s you that is out at the pointy end of the spear.
A properly designed AESA system is not overweight so are you saying that is what’s keeping it out of the Mig-29?
The point is that
Everything from increased range, increased number of targets tracked, vastly increased scan rates, sidelobe reduction, inherent LPI qualities, inherent jamming, increased A2A/SAR/ISAR resolution, simultaneous functionality (scan vs track, A2A, A2G, data link, SAR, etc), increased reliability, etc…
You’re right, those are just “modest” gains.
Since radar remains the primary sensor on an aircraft, it most certainly is relevant to the discussion.
Look closer..
The slope actually starts in the early 2000’s with much more than 1600 where you see F-15,16, and 117 numbers coming down as F-35 starts up.
Cutting the annual buy is more harmful to the program than just cutting the same number off the end of the program.
I always wondered why fighters do not have an in-hub electric motor for the front wheel so that they can more themselves around using either battery power or the IPP.
I have NEVER said that there is not an issue.
What I and the accident report have said is that the issue and it’s workaround was known but not properly taught & followed.
3. SUBSTANTIALLY CONTRIBUTING FACTORS
a. Procedural Guidance/Publications
Neither publications nor guidance and training were adequate for the circumstances surrounding
this incident. IPP and engine start issues with a tailwind were known prior to the incident.
However, the publications were written and communicated in such a way that the F-35A pilot
community had only vague awareness of the issue. This vague awareness led to inadequate training
for engine starts with a tailwind. Training also resulted in complacency and an over-reliance on
aircraft automation. Thus, the MP was not trained adequately and was not as ready for the abnormal
engine start and resulting fire as he could have been. Preponderance of evidence shows if there
had been an expectation of engine startup problems with a tailwind, the MP may have relied less
on aircraft automation, and may have identified an abnormal engine start earlier.
http://www.airforcemag.com/AircraftAccidentReports/Documents/2017/09232016_F35_MOUNTAINHOME.pdf
You don’t need a shelter and the issue was know.
The problem was that the specific issue parameters and workarounds were not disseminated correctly.
When was the last time you heard that?
Earlier this year IIRC.
I’ll try and find the link to the quote.
I think the issues was with a direct tail-on tailwind. Changing the angle just 5-10 degrees should help as will proper training.
but the low segment of the hi-lo mix is still being well served with mechanical arrays
Multiple services are upgrading their 4th gen assets to AESA like the US (F-15C/D/E, F-16, B-1B, etc), Taiwan, South Korea, Rafale, Eurofighter, etc. It’s a budget thing more than a capability thing.
They do not plan to replace 1 for 1
This is an older chart but you get the point.
