And add 2 external AIM-9Xs and 1) the enemy plane can detect the F-35 from significantly further, 2) the extra drag of the missiles and pylons prevent the F-35 from supercruising at all and it needs to use its afterburner extensively to compete with its supercruise capable opponent. Let’s be honest, it is one hell of a smart design!
Apparently there is no indication that they are going to fix the rear visibility issue with the huge helmet. This problem should have been identified a long time ago and the fix should already be in production.
Kind of mind boggling… but we’re used to that kind of c*** now…
In the case of the US, but surely F35B is capable of carrying ASRAAM internally? Could be an interim solution for the US too.
The ASRAAM has no datalink and no thrust vectoring, so I am not sure it would be sufficiently good.
They had a lot of time during all those years to figure out a way to launch the 9X from inside the bays, and they didn’t do it.
I am still convinced that the original a2a specs were insufficient. The specs should have been 4 AMRAAMs + 2 internal 9Xs in side bays. The JSF was going to be the primary fighter of many air forces, so it needed really good a2a armaments. Originally the USAF was going to get a lot of F-22 so the it could afford the JSF to be a somewhat subpar, but as soon as F-22 production was stopped at the beginning of 2009, the F-35 a2a capabilities should immediately have been accelerated, with 6 internal AAMs including 2 9Xs.
The F-35 might not be very maneuvrable, but what is much more important is the off boresight capability. The DAS should help significantly to achieve quick locks, but the problem is that the AIM-9X has to be carried externally, which is detrimental to stealth obviously. AMRAAMs cannot match the WVR performances of the 9X.
Being forced to carry the 9X externaly is a **** poor specification.
On a strike mission, if the F-35 doesn’t carry external 9Xs to keep its stealth maximal, it doesn’t even have 9Xs at all, and its opponents of course will have off boresight missiles. Good luck with that..
And the F-35 won’t have a real WVR capable missile that can be carried internally before a good 10 years.
The Block 1 upgrades rely partly on development work that P&W carried out for a demonstration in autumn 2013 for the navy’s XTE68-LF1 project. This focused on demonstrating a capability for higher operating temperatures in the F135’s turbine and introduced a variety of new technologies into the engine’s high-pressure turbine (HPT) module. These improvements, which Kenyon described as “advanced cooling technologies”, included new casting technologies for metal- alloy parts; new, highly temperature-resistant HPT materials; new thermal barrier coatings for HPT blades and vanes; more temperature- resistant oils for lubricating and cooling; and a new main shaft bearing. He said P&W’s XTE68-LF1 demonstration in autumn 2013 was “tremendously successful” – so successful that it recorded “the hottest-ever temperature in a production engine”.
They absolutely have to have this upgrade available if they build 450-500 planes in 3 years from 2018. Ugrading existing engines would cost a significant amount. What would be the point of lowering the cost with a massive production plan if some of the saving is almost immediately lost in upgrades.
It’s the same for some of the other upgrades. Ideally block 4 should only add new functionalities without modifiying existing systems, or add new software for new weapons and such.
I am sure they would like to accelerate the block 4 upgrades, but of course with LM patience is a virtue.. Money is a virtue too lol..
The single engine requirement from the USAF was the single largest driver to the overall shape of the F-35.
Having one large engine vs two skinnier ones forced the bomb bays down and out. The lift fan has little overall effect as the bays cannot move up even when it’s not there.
I don’t see how the single engine requirement affected the position of the bays. However, the STOVL requirement forced the engine to be sufficiently close to the lift fan, so the engine had to be placed like between the rear of the bays. That forced the bays to be separated by a significant width, unlike on the F-22, where the bays are right next to each other.
Without the STOVL requirement, the bays would have been placed right next to each other with the engine ( or 2 engines ) right behind them. The plane would have been longer, so would have been designed more in length than width.
My readings suggest that the F-35 would’ve been a more slender fighter if the Navy requirements weren’t there. I believe the carrier recovery is the primary reason why LM abandoned canards on their design. I believe for a given overall length, a canard aircraft can have a longer fuselage length. Also, USAF and USMC both only required 2 x 1000 lb bombs instead of the 2 x 2000 lb bomb the Navy desires.
One can question indeed the requirement for the 2000lbs JDAM. The JSF was going to be about 2/3 the size of the F-22 and the bays were forced to be larger. The requirement for 8 SDBs was right because it gave the plane enough firepower in stealth mode but there is a significant width difference between the SBDs on the rack and a 2000lbs JDAM. They should have kept the bay optimized for the box size of the SDBs+BRU-61, and built a large bomb that would have used all the space available. The bomb would have weighted about 1500lbs but would have been designed with a higher explosive content to have about the same power.
The STOVL variant also forced the plane to be wider. Just look at a pic from below and you’ll see that the lift fan did impact the width.
A large fuselage cross section is not that bad for subsonic, but in transsonic and supersonic the F-35 is significantly slower than it could have been. So basically they traded the supercruise capability for the 2000lbs JDAM and the STOVL variant.
Nobody complains because they were not 7 years late.
They need one that can capitalize on the MLD capabilities.
No, it is too bulky and if you look at the seat on the F-35, you can see that it has a large and wide headrest to help support that thing. Using the MLD like DAS is feasible and LM has claimed that it has that capability. It would require some extensive software mods(not easy with the Raptor), however. The new helmet study does mention that very possibility though:
The Scorpion HMD has been floated one possible option, was shelved, and has re-emerged as the leading contender to be integrated:
http://www.gentexcorp.com/scorpion-helmet-mounted-cueing-system
If the scorpion can do the trick they’ll probably chose it, even though it is less capable than the F-35’s helmet. It should have the ability to tell the pilot where to look when the MLD has detected a threat. I doubt it would be that hard to display an icon on the visor when the MLD detects a target in a certain direction.
US air force considering new 2,000lb rocket-propelled penetrating weapon
Background Here
Could this weapon enable to have significantly smaller internal bays on the LRS-B? The B-2s could be reserved to use the GBU-28s/MOPs, etc… the LRS-B could be made smaller, lighter and cheaper.
Has there been studies to integrate the F-35’s HMD on the F-22? The HMD could display the video stream coming from the MLD sensors and give the F-22 better night/day SA and a 360deg capability. The MLD has a lower definition than the DAS but I would guess it is still good enough to warn the pilot of incoming threats.
Double kills are relatively rare in air combat, so maybe 3 missiles would be sufficient for most sorties to kill one or maybe 2 planes. A 9 tons plane with a 13 tons engine would probably be feasable. I take it such a plane would make use of advanced datalinks to attack in packs.
The missiles could be located in side bays like on the F-22, one missile per bay, plus maybe one extra missile behind the cockpit in a dorsal spine bay. Keep it small.
They are planting various species of native trees. They start with fast growing trees to create a canope, then plant smaller trees below.
They are planting various species of native trees. They start with fast growing trees to create a canope, then plant smaller trees below.