I don’t see China as agressive in nature. The US is much more agressive, in fact. But when planning for military conflicts, you always plan for all eventualities. That’s what drives up the costs. otherwise we could all follow the route of Costa Rica and be happy with police forces only! 🙂
last sentence is exactly my point. 😀
but if the drive to prepare for all eventualities will bankrupt the state and jeopardize the economic well-being of a nation, and may be even spark war the very thing you try to prevent, then whats the point.
follow the golden rule my friend. follow the golden rule.
sorry, getting philosophical here.
Do not forget the psychological aspect of it! A new arms race has started, and there will be losers and winners. Unfortunately, the europeans seem to come out as losers out of this one, as there is no concrete 5th Gen fighter on the horizon. What a shame!
why does there need to be an arms race necessarily?
why can’t some just live in parity? or even inferiority?
China was at peace when in the past it clearly had inferior technilogocial platforms vs its neighbors.
its neighbors (or strategic competitors) do the same certainly?
How do you know that without (reliably) knowing any of its characteristics?
Let’s wait and actually find something out aside from a few pics before deciding exactly where it stands on terms of material superiority.
sorry.
I didn’t get finish my sentence and hit save button. 😀 read my post again.
This is new information for me. But still, then the F-35 simply wouldn’t be employed in the role it was devised for, namely air to ground. It will always be at a disadvantage against stealthy, fast fighters with a a high combat persistency.
To be more clear, of course the F-35 is able to shoot down enemy planes, but the notion of western air combat is to start a war with superior platforms. As already noted, numbers count. But the F-35 is so expensive. How many would Japan afford? 100? That wouldn’t be a good starting point to meddle with a china with perhaps 200 or 300 J-20…
then J-20 has acheived its intended purpose to stop wars.
who says the ‘west’ must always and can always afford to maintain military superiority vs. china?
china has lived under superior air platform of its neighbors relatively peacefully for a long time.
why can’t China’s neighbors live in peace when they are in the shadow of someelse’s superior air power platforms? 😀
Even if they do not achieve F-35 stealth levels or sensor potency, it does not make them stupid or anything similar imo.
I am not saying same level of potency as F-35’s sensors, I am saying assess the scenario where it will come up against F-35 and have appropriate requirements to ensure at least competitiveness in a2a.
I agree in regards to raw performance, but a2a is more than that. Keep in mind I am not saying F-35 definitely trumps it, but given US aero technology lead over everyone else, their stealth expertise, sensors, etc, I would not count the F-35 out as a credible, potentially better a2a opponent.
Like I said in the other thread…
J-20 started well after F-35 is well into its program. its rough tech capabilities are know. people are not going to sit there and twiddling their thumbs.
the chinese would be very stupid if they do not evulate what f-35 can do in aircombat as part of their J-20 program.
I for one have confidence that Chinese are not stupid.
And if you look back at all the air wars (WW2, Israeli-Arab, Vietnam, Iran-Iraq), speed and endurance ar two of the deciding factors for victory in air combat.
The german luftwaffe hated the P-51 for exactly those qualities!
And additionally: if you have a fast AND stealthy platform, the advantages of stealth are even more pronounced.
wrong on partial count.
Me-262 has speed advantages over any allied fighters.
numbers counts.
What basis is there for the claim that the F-35 is lesser performing than the J-20? For all we know it has significant advantages in A2A.
if it had less raw a2a performance than F-35 it would have been called H-20.
It wasn’t an LM release though, unless Aviation Week has been bought off too. It was a pretty clear, and unspinnable statement, that he made.
may be from life experiences your and mine perspectives are different. that’s all.
Why don’t bomber designers build very sleek aircraft, and then hang 50k lbs of bombs under the wings, along with EFTs? Which do you suppose would suffer a higher drag penalty?
and why did the Tu-16s have that big bulge on the wing?
and why did F-111 a rather small internal bomb bay early on and deemed fine?
and why did tornados and fencers have no internal bay at all and deemed fine for strike missions with ordinance strapped underneath their wings.
surely with out LO considerations back then they still must have known about the “higher drag penalties” have they and stuff everything inside because as you suggested hanging bombs outside would definitely suffer those “higher drag penalties” than a bigger wetted area. and to paraphrase our friend up there. You need some real gall and alot of hope if your going to start saying that engineers who designed the jets know less about the tradeoff then those who sit infront of their pc’s posting on internet forums 16 hours a day.
at end of the day it is a trade. there is no way you can say it must go one way because it doesn’t.
you know before ww2 transport and bombers were very much alike.
until performance need drove the bomber designers to get rid of big wide fuselage and squeeze all the iners as tight as possible. some even squeezed so much that their max load has to be carried on the outside… their internal volume wasn’t big enough to carry all the bombs.
You must have missed the USAF Lt. Col in front of Hank Griffith’s name, and mistaken him for a LM employee, or that it was an article in Aviation Week, and not a LM press release.
There’s gonna be a tin foil shortage soon, with all of these conspiracies be tossed about.
He is certainly part of the program. and as such he is subjected to all the PR distortion as any other program.
now I am by no means saying he is a lier. I am saying these things are often taken out of context by PR peoples. and PRized.
Perhaps if we limit the discussion to wingtip Sidewinders and conformally carried MRAAMs. It most certainly does matter when you’ve got EFTs, 2000lb bombs, sensor pods, and the pylons, etc… hanging under the wings.
why do you assume an external store is necessarily more draggy than an bigger wetted area? :dev2:
In sustained G 4 big things matter, Lift drag weight thrust.
suppose your thrust balance out your drag.
assume your airplane is not structure limited and elevator power limited. then you will reach your max alpha (fbw or not) when you pull your stick back (and beyond if you don’t have fbw limiting it). now. whatever lift generated divided by your weight, that’s your g.
now, what happens if you chunk up your weight. fuel/ bombs.etc. point mass or not.
tell me again you can reach your a/c’s max g when you have stick bombs on your structures?:dev2:
…
and whoever build their aircraft beyong its g capability + margin i.e. stress for max weight at max g where its wing can not get you the lift needed to get to the max g given the max weight, + margin, is, imho, stupid.
We’ll see. After the intense spotter activity surrounding the taxi tests and first flight I would have thought we’d get clear evidence about another flight (or an An-124 flying in), either in the shape of forum activity or photos.
an-124 flying in.
ha.
traditionally the fighters from CAC/SAC or transporters from Xian (duhhh) just fly themselves to XianYang. after assuring that the ferry flight is ok.
Wing tanks and A2G munitions hanging on a 4th gen wing greatly affect roll rate, g-limits, etc in an A2A fight.
An F-35 (in full VLO mode) that carries it’s A2G munitions internally has them very near the center of gravity and center of lift. Also by having the A2G internal stations mounted directly to the frame, they can be stresses for a full A2G load and cleared for max g load.
have you seen any literature from any one assure you of that? I would like to see it very much.
btw. The reason I asked one to consider for drag polar and wing loading is that, doesn’t matter if your structure is made out of tungsten, and your bomb is a point mas…
your wing will still need to generate more lift, given the g you want to pull. now, last time I checked the drag polar of any airplane I have seen don’t have a big flat swath.
btw, I have yet to seen an airplane that claims to be able to hit its max g, instant and sustain, everywhere in the envelope, in all wt and cgs.
now the question still stands: the F-35 guy will not let go of its a2g stores when a2a fight starts?