Of course they receive the same missile, but isn’t the only thing they really benefit from the kinetic advantage of IRIS-T as compared to the Sidewinder (Which ones do they use by the way? AIM-9M?)?
I suggest you take a look at the link provided by KKM57P in post #102.
Its in German, but the pics speak for themselves.
The last 2 pics show the area where the analog IRIS-T can be locked to a target (in red) compared to digital use with helmet. Thats the only advantage.
(Note the pink area, in analog use the missile stays locked there)
The F-35 is built remarkably heavy for its size. That’s a lot of beefed up structure there.
I think its fairly light. Show me another 12-13 ton plane carrying more than 8 tons of internal fuel, internal weapons bay for 2000kg+ and internal targeting sensors.
Compare that to the F-15 and the F-35 looks quite ok. 😉
Reminds me of the LCA somehow…
Anyway, what the F-5 really needs is not a new wing, but stronger engines.
In the first one the commentator mentions that there is another 20% improvement in turn rate “in the pipeline”. Does anyone know how this will be achieved?
I dont think the EF was cleared for the full flight envelope in 1998. So it might just be an FCS related improvement.
It might. It might not. It might a whole lot of different things. Going on what things might is a very slippery slope that just invites a lot of speculation (and trouble). The Typhoon might go M4 and run on butterflies and kisses. 😉
The Rafale actually reached Mach 2 in test flights but max. operational speed is still given as M1.8.
I think its the same with the Gripen.
Do I believe the manufacturer’s figures – validated by the customers’ independent Typhoon Structures Team, or do I prefer the uninformed prejudice of some anonymous French spotter on an internet bulletin board……?
Now let me think…… 😉
I hope that wasnt directed at me. Theres no need to get insulting by naming me French. 😉
(Sorry to all French posters, just joking. 😀 )
But dont you question how BAE thinks to manage the weight increase on a design never intended for carrier use better than others who designed planes for carrier use from the start? Do they know someting the rest of the world does not know?
Its a typical manufacturers claim. History has shown theyre typically not worth the paper theyre printed on.
Serious planning
BAE have done at least two full studies into the “marinisation” of Typhoon. The first of these was, to my certain knowledge, validated by the users’ Typhoon Joint Structures Team. This is far from being ‘fantasy figures’ – there are detailed drawings and carefully worked out figures (down to sink rates, proportion of carrier landings, impact on airframe life, allowable GPS timing errors (25 ms!) – everything you could think of), as the drawings (which are the tip of the iceberg) would indicate. There are detailed drawings showing four or more main undercarriage variations and the associated structural changes to the wing, for example.Fantasy figures
According to the “Phase 3 Eurofighter Navalisation Study (July 1998)” the weight penalty for ski jump was 340-kg and for catapault launch 460-kg.“How can you know the weight penalties or the cost?”
I know the weight penalties because I have the document.I know the broad costs because I’ve spoken to people who know.
Those are exactly the kind of exaggerated figures I was talking about. Sounds all nice on paper if you want to sell stuff. Even the Rafale M gains more than that compared to the C so…
I would take that data with more than a grain of salt.
The Russians pulled it through with the Su-27/33, teh MiG-29 and the Su-25 all these were develloped simultaneously! BAE got it right with the Hawk>Goshawk… I dont see why the Eurofighter would be any harder… But it would sure be another BIG nail into the Rafale’s export possibility coffin…
Regards,
Hammer
The Russian planes were designed with rough field performance in mind and still they gained a considerable amount of weight.
The Goshawks weight increased too, affecting performance but still enough for a trainer.
Actually, though there would be penalties (the weight penalties are surprisingly low), and though there are ways in which a Rafale M would be a better carrierborne aircraft, the cost of completing some or all of UK Tranche 3 to Typhoon (N) standards would not be all that high, and the unit price might well be lower than the final price of Dave-B.
How can you know the weight penalties or the cost? At this stage where theres no serious planning, any fantasy figures provided by the manufacturer are useless. 5 to 10 times more than that is probably right. 😀
Besides, such modifications have proven to be very costly in the past.
ELP, the North Dakota ANG was the last operator of F-16ADF and they retired them earlier this year.
You think the EF can fly from carriers as-is? LOL
It probably can.
Landing will be more of a problem though. 😀
Use of ski jump plus “restraining device” (dont know the proper word) should even allow for some decent load, like on Russian carrier.
The Tornado struggles to keep altitude and speed with a tanker at medium altitude when loaded with external stores (which it always is). Better put that pod under something else if you want high-alt recce. Why not EF?
I never got that actually, looking at posts in f-16.net, the ratio is about fifty-fifty.
Unfortunately, theres no f-15.net. I bet the ratio there would be around 100 to nil. 😀
The air to ground stuff for the F-16 is practiced by the F-16C groups, not the ones with the National Guard which are flying upgraded F-16As. The air to ground stuff is also practiced by the F-15s that are either Strike Eagles, or any Eagle updated with the multi-role APG-63V1.
USAF doesnt fly F-16A anymore. The F-16A and C units tasked with air defence often didnt have the secondary A-G role, true, but I dont think theres any A-A only F-16 unit left.
No F-15C unit does A/G, regardless of radar model.
One problem occurring with the F-15 groups is that the plane is aging, and the more it ages, the more training restrictions are placed on it, including allowable G limits. An F-15C group may get more BFM practice than an F-16C group, but the latter may probably push the edge of their aircraft more during those practice times, like hitting 9G.
True, there are speed limits and some engine models are detuned though I’m not aware of any g limits.
But remember 9g isnt that important in bfm. Think about the F-18.
Several countries did and do research about a stealth fighter. The problem left is, that it becomes prohibitive expensive, when built in a small number only.
See the B-2 example about that. Second question-mark is about the development of new sensors dealing with stealth. Life-time of advantages is limited in time.
It doesnt matter if its stealth or not if built in small numbers, see F-2.
On that model, besides the awful canopy arrangement, the intakes look rather small.
You’ll want to note that’s a -132 powered F-16.
I noticed now. 🙂
That must be the hottest F-16 around.
But the 132 engine gains most of its additional thrust from its afterburner, so it doesnt matter much.