That is rather a wordy way of saying you don’t have a source isn’t it?
Nope, it means how it reads.
I am failing to understand why showing that the F-35 has performance characteristics on par with the F-16 is a great thing.
F-16, whilst a fantastic jet, has been surpassed by many designs now. Just comparing performance and results from exercises with F-22’S, Typhoons, Rafales etc.. prove it isn’t that special anymore. End result, it is at a disadvantage.
With the F-35 having similar, it is at a disadvantage as well. F-16 comparable is not a strength but a weakness.
But the F-35 has a lot of strengths other jets do not, that is where to take the argument of ‘superiority’.
hoppy do you get it?
(still swear you are Scooter)
So at the first sign of a threat the Eurofighter drops its stores, wasting them, and failing in its mission….
An F-35 in that same scenario, and with the benefit of its stealth and huge kinematic superiority over a strike configured 4th generation aircraft would likely simply avoid the threat and see its mission through to completion.
Could a Typhoon get to M1.4 while carrying that load? Perhaps… but it would be a very strange scenario that would see it attempt to do so.
Check: BVR shot kinematics.
How likely do you think a sortie would be planned with knowledge that the jets may be attacked AND then not give additional support? escort whatever…
The whole point behind an aircraft having to drop its stores is a total surprise threat.
Again, would an F-35 (full int load) keep the extra weight when a surprise hostile threat emerges? God knows, but the planned idea is that it would not encounter such a threat and if there was a probability, additional support in whatever form would be given.
BTW here I’m not trying to compare ground attack, The F-35 has that sowed up.
Why don’t you share with us your source stating the load an F-35 can carry while pulling 9 Gs. (The speed and altitude requirement is true of all aircraft.)
I don’t have one. Do you think it can sustain 9G with full internal fuel and weapons at speeds >400ktas or alt >30kft? Does it need to, considering the systems it has? Would it be useful if it bleeds kts like the F-18E/F? When would it even find itself in a position of full load and 9g manoeuvring? hmmmm
, you must be going slow to perform high AoA maneuvers. Sometimes pilots find themselves slow, in those situations it is nice to be able to perform high AoA maneuvers. :rolleyes:
hurray! My point, of course completely missed, what pilot would want that situation? If your there at high AoA you are like an asthmatic airborne penguin, the pilot has generally f-ed up in the first place. You are dead most of the time no matter what jet you have.
Given that the F-35 and Typhoon have similar installed thrust, they can expect similar endurance in combat with the same internal fuel load. Thus a Typhoon with 100% internal fuel is carrying the same fuel load as an F-35 at 60% fuel.
That is a belter.
Why don’t you share with us your source stating the load an F-35 can carry while pulling 9 Gs. (The speed and altitude requirement is true of all aircraft.)
hoppy, I give up. You lack common sense, realisation of modest sarcasm and a strong ability to completely miss a point.
Just so much wrong, or ‘honest confusion’ in one place. I just wanted to see how small a piece of bait could catch a giant tuna like you.
I am not even going to try to address all the various points raised here.
phew.
think we can all agree that the F-35 was not designed with an emphasis on prowess in BFM exercises, nor was it designed as a high-fast interceptor.
Nice, you are learning.
said, it is a 9G capable aircraft with the ability to go to 50 degrees AoA (compared to the Rafale or Eurofighter at 29 or 25 degrees).
Yes, one version with a small load can maintain? 9G at a certain altitude and speed. Pilots love to get slow with high AoA, especially in slower accelerating jets.
will have a thrust to weight ratio in excess of 1:1 in an air to air configuration with 50% or less fuel (a fuel load that corresponds to roughly 100% fuel load for a Rafale or Eurofighter) and by all accounts has excellent handling characteristics and strong acceleration at speeds where WVR occurs.
An A380 at 50% internal fuel has >15 times F-35 max fuel load. Not sure of your point. If it is range, well that is a different, complex debate. F-35 WVR is all about it’s systems, they are world class.
together the F-35 will clearly be a dangerous foe even in WVR combat. Will it be the absolute top aircraft in the world at BFM exercises? Probably not… but in the real world and combined with the F-35’s other advantages (sensors, stealth, networking) there is every reason to believe the F-35 will be effective. I guarantee you there isn’t a pilot with a brain that would relish the thought of having to fly against a LO adversary armed with Meteor or AIM-120D.
Correct. Promote the advantages it has, accept the weaknesses, then you can have a credible jet that you do not allow the enemy to exploit the weakness.
Also, are you Scooter? You seem like Scooter with an A-level or two.
…and you know this how?
It takes only a small amount of intelligence to understand the context of his speaking, and understand the different permutations of conclusion. I will explain it to you though.
As stated,
CHAIR: Let the Air Vice Marshal finish his answer, then proceed.
Air Vice Marshal Osley : If we compare those two, the legacy aeroplane with fuel tanks and weapons on it, if we take a fourth generation fighter, typically an F16 or an F18, in that configuration it would take substantially longer than 63.9 seconds. If you took a 4½ generation aircraft it actually could not accelerate to supersonic in any time over that 0.8 to 1.2 range with a combat configuration of external tanks and weapons. The point I made originally was that we need to talk apples and apples between legacy fighters and the F35 on manoeuvrability and performance capabilities.
Well of course NO highly loaded typhoon/rafale could go supersonic with this, additional weapon parameter limitations.
The F-35 can, though the time to do this is not mentioned, and hence fuel consumption may put a full stop to this regardless, never mind maintaining above mach flight.
The fact it can do it does not mean it adds value. Why burn a **** load more fuel, increase IR sig and reduce manoeuvring capability for such a small increment in flight velocity? Not much.
Then the argument of a threat (Note, not typhoon vs F-35).
Typhoon just drops the stores and is able to use the much higher kinematic performance available to it. Say the F-35 does not, it’s performance is even poorer than usual and in all likelihood getting rid of a few $100k of internal stores is needed to give the F-35 a slight increase in ability and prevent the loss of pilot and $mils of the jet. The scenario I am describing is uber simplistic and pretty much fictional with all the over support available, however it is a case that the typhoon just drops the stores and then it has far better kinematic performance than the F-35.
Now, if you can show me the F-35 can usefully go through the barrier and obtain M1.3+, with full internal load, without it compromising critical fuel levels and make it into a meaningful advantage I will retract my argument.
And finally when he states no transonic performance with external tanks and weapons, typhoons blast past M1.4+ with 2 tanks and 8 ata missiles. So you have to ASSUME he is talking about heavy atg loads with restrictive flight parameters.
Simple.
[I][B]
But would any of the Typhoon assembly lines still be open by the time that Typhoon started defeating the F-35 in various circumstances?
good question and i certainly cannot answer it with any credibility.
[QUOTE=FBW;2094533]Someone should inform the Australian parliament that the Vice Air Marshal lied in front of a committee for the quote is from him, not mine (if you had read the link). First, the key is similarly configured, take that for what it is worth. I rather agree with you that there are few aircraft that would be able to match a Typhoon in trans-sonic acceleration when carrying four semi-recessed missiles.
I did read it, he didn’t lie. He chose his words wisely (ambiguously) that could fool someone not very clued up on differing sortie profiles. His statement is reference to full atg loads, i.e. full gas bags, 4-6 lgb’s/smart bombs and the ata fit. There no aircraft with MAX.external weapons can go supersonic (well there are a few) where as the F-35 technically can, kudos F-35 it would seem. The question is, for what use? As I said, any danger and the stores are dropped. An F-35 ingress at (1.0-1.2)M gives little advantage vs .8-.9M. What’s the point of burning tons of fuel to stay in transonic drag hump, especially fully loaded god only knows how long the F-35 would actually take to get there. He just chose his words wisely.
I agree with what you say about DACT. My point is really stressing, I think the only force structure to allow ‘fully exploited weapons potential’ would be the UK armed forces between the F-35 and typhoon, determining real vulnerabilities of both aircraft etc…No ‘sensitive’ information can really be given away when its in the same force. Multi-national, as we all know, exercises are a different matter all together regarding actual capability demonstrated. However IF the typhoon starts defeating the F-35 in various circumstances, thats gonna be one hell of a marketing point for Eurofighter to have. The question here is IF weaknesses were found in the F-35, it’s also not in the UK’s interest to start telling everyone and anyone where the F-35 is most vulnerable. Unique set of circumstances present within the UK regarding the F-35.
Is this after the destruction of everything of any consequence in the inevitabe nuclear war or….?
😉
If you took a 4½ generation aircraft it actually could not accelerate to supersonic in any time over that 0.8 to 1.2 range with a combat configuration of external tanks and weapons
A fully bombed up rafale/typhoon would never need to go >.9M. The stores would we ditched. The F-35 pilot could keep his own if he wanted, >.8M performance would just be ****er than usual and any ‘engagment’ or a simple bank would have the F-35’s G-limit between 1-2.
In AtA configs with tanks, well documented (go and educate yourself if needed, not from marketing brochures but words spoken form pilot’s mouths) rafale and typhoon toast the F-35, significantly w.r.t typhoon. Typhoon can SC, for a useful period, >1.25M, 6-8 AAM, 2 Tanks. Again I will not waste my time finding common knowledge for users.
Lets all wait till the RAF and RN start doing some DACT. Should be quite a time when REAL F-35 performance can be evaluated.
As a point. I think the compromise of the F-35B is, with all the constraints outside of the technically feasible at present, an aircraft with fantastic potential.
F-35C raises questions, USN will need to spread its risk there.
The USAF and all the other customers are the biggest losers here-F-35A. They wanted one thing and and all the evidence points to that they’re gonna be getting something different. Not necessarily bad different, but not what was ideally asked for, promoted and guaranteed.
The power of marketing.
Having nuclear ICBM.SLBM capability gives far more than obvious offensive/defensive arguments. Think political and reputation. The world has much greater volatility than ‘surface’ relations represent. Idealism vs. reality.
Not in a million years will the UK quit trident. Anyone who proposes that needs a serious reality check.
Scotland has a fortunate postion, if their ‘independence’ actually got anywhere, any real territorial threat to Scotland is a threat to England, nuclear or otherwise.
silly times.
‘Independent’ with the £.
You are welcome. Pictures were taken at Decimomannu yesterday 27th of November. Now BAE and other sources have released further images and a press release: http://www.baesystems.com/article/BAES_163539/typhoon-flight-tests-with-storm-shadow-missile-started
With Stormshadow’s integration beginning, is there any emphasis on conformal tanks yet?
I’m not clued in on range/tank capacities with stormshadow, but as of now, if only the central tank may be used, surely the typhoon in this role is not competitive?
To be ‘attractive’, true penetration range must be a factor. Then again, the middle east is a small place when you have a decent standoff capability within the missile itself.