Kid, don’t troll/LOL
How old do you think I am? I presume you were born in 1973? You keep saying kid, and you know nothing about my background.
It says AG attack and I’ve shown you the list of AG configurations, all of which are significantly heavier than anything F35C can carry internally.
Now, if I was you, I could go ahead and troll about EF doing this on internal fuel only, since the text nowhere says, that EF uses tanks for those ranges, does it?
Very few missions are flown with the max load out, so it’s a bit daft to think that the combat radius given coincides with the maximum possible payload.
In theory an F-16 can carry 15,800lbs of stores, but it’ll never do that in practice.
Anyway, all this is immaterial since you lost the argument as early as on mission profile, so even if we assume the EF somehow carried similar loadout (it’s not possible to arm EF so poorly, though) to F35C, it’ll outrange F35 by even a larger margin, with tanks.
Which mission profile of the Typhoon has a combat radius over 900nm?
The cruising altitudes are unlikely to be below the stated combat altitude which is given with 35k ft in the slide. And for that matter internal carriage doesn’t protect your loads/structure from g-loads. Where is the prove that the F-35 will be able/cleared to pull 9 g when loaded with internal AG stores?
Carrying the weapons internally, and nearer the center of gravity, means that there’s less inertia to overcome for one, which is why LM/USAF says that a combat loaded F-35 is more agile than a clean F-16.
Source-
http://www.airforce-magazine.com/MagazineArchive/Pages/2009/July%202009/0709Fighter.aspx
With a full internal load of fuel and weapons, the F-35 is as agile as a βcleanβ F-16 carrying no weapons
So I think that answers the question about G loads.
[quote]
I agree that the F-35 don’t need ETs to achieve a similar range, but the fact that the F-35 don’t offer a significantly greater range while carrying more fuel and not being constrained by external stores is telling, if these data are true! And that’s the point here, the Typhoon wasn’t designed as a deep striker! [quote]
The question is which one is going to have the higher degree of survivability, or ability to operate in less permissive environments?
40 nm less range at lower cruise altitudes and with fewer fuel? Sounds a little bit odd don’t ya think so?
It also has less weight and drag though, and without a true apples to apples comparison, I’d hesitate to draw to many conclusions about which numbers were right.
LOL…
http://typhoon.starstreak.net/Eurofighter/tech.php
http://www.airpower.at/flugzeuge/eurofighter/technik-daten.htm
Weapon loadouts…
http://www.eurofighter.com/et_sr_mc_sw.aspLOL, Wrightwing. Just as I thought and wrote in my previous post.
Reread attack profile paragraph of my last post, although I don’t imagine it’ll make much difference since you obviously didn’t understand it, the first time…
I mean, this is getting funny, watching you trying to “interpret” the figures for us. π
Seriously man, you don’t have a clue…
I’m not saying the Typhoon can’t carry all that. I’d just like to see where it says that 750nm combat radius is with that particular load out.
Well thanks for the link, though I know this document. You have to take into account that:
1.) This is a very old document and that the aircraft hasn’t demonstrated that range, so it’s at best an estimation.
2.) It’s the combat radius for the F-35C, we discussed the A.We can just wait and see what the real figures are as I’m certain there will be more information available in the future. I could well imagine that the F-35 will offer a not to dissimilar range to the Eurofighter with ETs, but we have to take into account that this just includes 1000 l tanks for the Typhoon. Full internal plus external fuel for the Typhoon results in a total fuel load of just 7230 kg. If you take into account that these range figures are with external tanks in comparison to the F-35 with ~8300 kg of internal fuel and being clean, the Typhoon doesn’t fare bad! In other words a Typhoon with ~10% less fuel 1/3 of which is carried in ETs still offers a similar range to the F-35, while the later is clean!
Edit:
And as Cola said the F-35s combat radius is with a hi-hi-hi profile, in comparison to the Typhoon’s hi-lo-hi.
Again, these were prior to weight reduction, and we don’t know what the cruising altitudes used to ascertain those numbers were. The important thing is that the F-35 doesn’t have to use EFTs, to still be competitive, and has no G restrictions due to external stores(or RCS penalties). In more permissive environments, the F-35 can also carry EFTs, and additional stores.
Wrightwing, EF’s AG radius is 750nm, BUT on a high-LOW-high profile and full weapon loadout (6-8 AAMs and 2-4 AG weapons plus 2 tanks).
F35C computer game’s radius is 768nm, BUT for a high-HIGH-high profile and 2 AMRAAMs and 2 JDAMs.
EF is M1.3 capable in QRA (2 tanks) configuration, on dry power alone.
You don’t even have an idea, of what you’re talking about, do you?
What matters in your little world, is that F35C’s (F35A’s imaginary friend) figure is 18nm larger than EF’s, doesn’t it?? π …seriously, go learn anything about planes. π
I’d love to see the source for 8 AAMs and 4 A/G weapons, and achieving that range. That’s 18nm further on internal fuel, than the Typhoon on internal fuel, and 2 EFTs. Even the F-35A isn’t much different(728nm, and that includes a low altitude leg, and cruise at 25k feet- I suspect that at 35-40k+ you could squeeze even more range).
As for the F-35’s capabilities on dry thrust, I wonder if you’d share what that figure is for us, bearing in mind that the F-35 can reach high subsonic at less than 50% dry thrust(Code One Magazine 2007).
That is a very old document, I would like to see something more recent to take it serious.
You’re right. That’s pre-weight reduction, so that’ll throw the results off.:D
LOL Wrightwing, so how did you figure, F35 has longer range on internal fuel than EF with tanks, from this document? π
The Typhoon’s combat radius is ~750nm with 2 tanks, so it’s close.
@Wrigthwing
And this is based on what? Your wishful thinking? According offical data the F-35A has a range of just 2222 km on internal fuel, while the Typhoon has a range of 2600 km on internal fuel. While I think it’s reasonable to assume that the F-35s range actually exceeds 3000 km, your claim definitely doesn’t hold water, nor can you back it up.
http://www.nps.edu/Academics/Institutes/Meyer/docs/Joint%20strike%20fighter.pdf
Check out slide 13
It depends on how you look at it. An example – imagine a test with F-35 carrying two dummy bombs, fueled at 15% and accompanying F-16C fueled at 90%. Duing the acceleration phase the pilots find out that the F-16 is not quite able to cope with the F-35 in that conditions. Beesley reports that to LM and their PR decided to use it.
So they let Beesley say: a loaded F-35 can out-accelerate a clean F-16C Block 50.
Is he lying? Technically he isn’t. What he says is true. He just doesn’t say the important details which change the whole picture.
Ask yourself this question- what information would LM be able to determine from a flight test under those conditions? If one wishes to go to irrational lengths in order to argue the F-35 doesn’t perform well, they can come up with all sort ofs what ifs, yet claims from other manufacturers are accepted at face value. That doesn’t fly with me(no pun intended:cool:).
If however you look at the examples where LM mentions flying with a full load of fuel and 5500lbs of simulated ordinance, and performing well, you’ll get a better idea than imagining the above scenario being likely.
More data from material you examined long ago and under copyright?
Wrightwing, cmon and be a sport…just leave this board.
Sorry to disappoint you. I’ve already posted links in the past, which I’ll go back and find, seeing as how you can’t trouble yourself to do so.
You may want to look at pages 38-41 a little closer. There are 3 hardpoints under each wing(6), plus the internal hardpoints, and the hardpoint for the gun.
^^^^^^^^^^^^^^^
The range of the F-35 on internal fuel is already greater than a Typhoon with EFTs. Now add EFTs on the F-35 on top of that.
As for hypothetical avionics upgrades, well I suppose anything’s possible if the countries are willing to spend the $$$$ in R&D and integration. Of course the F-35 will continue to get upgrades too.
Well the figures on page 42 were what I was pointing out, where the comparisons of RCS were listed.
Well considering an F-15’s RCS is more like 8-10m^2, and not 405m^2, I think one can draw their own conclusions about how accurate the methodologies used are.
F-35-
internal carriage- ~5500lbs
external carriage ~15000lbs(and the F-35 doesn’t have to waste pylons for things like targeting or ECM pods)
Sensor fusion-
Saying that all sensor fusion is the same is like saying a Ford Mustang and a Porsche 911 Turbo are both cars. Not only are there different levels in the sensors that are being fused, but in the level of integration of the fused information.