Do you realize that as early as 2000/2001 the clock was tickling hard toward this tech in open source ? That today some countries have flying assets with thousands of hours in a vast array of speed, weight, range and alt ?
And what are you adverting, an Eu R&D financed project whom most are sink holes to R&D budget (I still remember one of this guy laughing all his guts out in front of the assembly when we where remarking that all the project that he was presenting where alrdy fielded the very same day the RFP was published : “You’ve got to get in contact with us before, uh uh uh”….)
Oh yes. 10 years on,after a gamut of cocktails, “committee” and whatever comes after, something will fly… 20 years on from now, we will discover that most of the cap are dubious or the gains are marginal and so goes the story…
Great ! Errare humanum and bladibladabla
By the way,
might it not be possible to disrupt a plasma sheath at range with a highly-steered radar beam? Things might get quite awkward if your intakes start getting differential airflow, or one wing becomes more draggy than the other.
Are you really re-singing that old song: Plasma/Stealth does not deserve nothing ?!! 😡 (re-read the above)
Let’s wait for it to be tunnel tested or some CFD view release
@Rii:
I think you are wrong here. The ATD-X is a capacitor. It keep a momentum of decision on the JAF commender. Just like the F1 and the F2 were.
With “F3” the JAF will be able to follow in theory whatever policy they want and that makes them less predictable. It’s good for Japan… And good for the US.
Capacity wise, the F3 is not as sophisticated as the 35. It’s looks like to be an offensive AirSup platform at range. A modernized F15 with light first day strike cap added.
Are Orange Amplification known for having their products to be, well… Orange? Yes.
Pretty obvious what it states, Nic. *Sigh.*
Don’t be that angry EE, your thoroughbred is well positioned in the “new race” thx to its cte positive cross section variation.
The real question is: Since there is no 35 nor 22 nor PakFA… What for do we have to go to the static display at Farnborough ? Well free fish&ships someone ?
Separately, Eurofighter is also updating its aerodynamics, promising to improve the combat aircraft’s subsonic turn rate by 15%. By year-end it expects to make is final proof-of-concept test flight on an aerodynamic modification kit including leading edge root extensions and extended trailing edge flaps. The kit also features reshaped side-of-cockpit ILS antennae covers, turning them into 70° delta strakes.
Laurie Hilditch, head of future capabilities at Eurofighter, says the modification kit should give the aircraft the sort of “knife-fight in a phone box” turning capability enjoyed by rivals such as Boeing’s F/A-18E/F or the Lockheed Martin F-16, without sacrificing the transonic and supersonic high-energy agility inherent to its delta wing-canard configuration.
From FlightGlobal as of Today…
Yes. It’s a clever move. They have asserted the threat and build something ard that fits 95% of their needs. A duper 15 with a massive AirSup potential and light first strike cap (my guess only).
What I wonder is: is this the first 3D AESA scan radar because that strange thing in the open nose (see Deino’s picture) looks weird for a planar antenna ?
It certainly seems like “some” of the future capability will be high and fast. I can’t see strikes against moving ground targets happening from up there though, maybe slow moving or static high value assets.
High altitude and fast looks like the pattern for LM’s recent patents though. Propulsion designed for 150kft altitude for speeds up to Mach 10, and there’s been quite a bit of focus on geo-navigational systems that use stars as reference points, which really does make sense if you’re flying at such high altitude, unjammable, consistent and highly accurate due to the very short wavelength of light.
Yes you are right. I just wanted to add my 2 cents to you excellent debrief.
I have been talking so much nearly alone abt that subject that it’s strange to see my old rat hole transformed in a matter of a day into a new Plasma-mall with glowing advert signs everywhere etc.. 😉
Shiny it is said…
PS: high is also where you can find “free” plasma… and to get there you’d need to be fast 😉
So now, ppl can understand why the future is high up and fast.
they have to pick and choose what functions they want and not want, says Lennart Sindahl
I thought it deserve its own post. I do agree however that this is not the right thread 😉
Lockheed, Boeing and Northrop (from memory) all seem to have worked out how to use plasma for aircraft applications and how to negate the downsides associated with its use. In 2005 and 2006, around the time when all 3 companies were submitting their patents for hypersonic propulsion systems (the recent SR-72 announcement prompted the search for this information), there was also a whole bunch of technologies patented for using plasma systems in conjunction with electromagnetic aircraft surfaces to negate drag.
Lockheed’s patent claimed to be able to actually use the skin of the aircraft to generate additional propulsion and it removes the need for moving control surfaces on aircraft by controlling the airflow using plasma produced at the leading edges. They also claimed to be able to enhance and control airflow into irregularly shaped inlet ducts. From memory Boeing had plans to use plasma with helicopter rotors.
Will be quite a game changer for aircraft considered by many to be “un-aerodynamic” if these companies have turned the laws of aerodynamics on their head.
Someone mentioned the effects on plasma on radio communications and radar. Don’t remember if it was Boeing on NASA, but there was another patent for technologies to locally negate the effects of plasma. The context of the technology was for eliminating radio blackouts for re-entering spacecraft.
Thank you very much for the debrief. Would you be kind to link some of the patent ?
Also, it would be nice to hve a similar topo on the Russian side. Just for the comparison.
Great one!
While the saying goes mever say never, I doubt there is something behint the CFTs only with AMK claim. While it’s said that the AMK smoothes integration of heavy stores like Storm Shadow or Taurus it’s apparently not a must. Consider that the CFTs run along the fuselage and are in fact closer to the CG than the stand-off missiles. Furthermore the CFTs are split in three main sections with a transfer tank in the middle. Like the internal fuselage tanks the CFTs can shift fuel from the front to the rear section and the other way round. In other words it sounds like a hoax to me.
Concerning Brimstone we’ll see. It might well be that the customer requires not more than 12 Brimstones which is already plenty. From a technical point of view I see no limitation here that would prevent carriage and employment from the centre wing stations.
Just my 2ct
Scorp,
The prob with CFT is that you have to fight while carrying it. For a fighter that means Alpha*. In the order of +25 – +35 nowadays to stay credible. We known that the Typhoon is alpha sensitive thanks to choice made during the design. If those things restrict the bird bellow 20, then they are useless. That’s how I see things.
You won’t re-establish an aft fleeting CG by transferring 1/3 rd of the fuel carried (when in fact you’d better have those empty before engaging in a fight).
*I have a hard time thinking that supersonic drag is the concern.
Well I tried, but since we will continue to talk about MRAAM’s, might as well have a bit of fun 🙂
Fantastic vid. Thx for posting.
We can see there that getting the proper clearance was one of the most critical factor.
Radio buzz
Banjee leader: Understand th.. crrrrkk clear to k… crrrr
…
…
Awac : Clear to kill clear to kill leader
“Tuuut” constant tone ring on the RWR
Centric connection will alleviate this expending the WFO bubble closer to that of the sensor.
I disagree with any 3D printing on board a fighter being useful. There is no weight savings from 3D printing. In fact you will absolutely carry more weight because of the weight of the 3D printer will add to the plane in addition to anything it makes. The smaller the printed item is the larger the weight penalty of the 3D printer will be. The potential advantage of space saving is also negated because you need a internal bay to do the printing and that negates compactness of 3D printing. That only leaves ability to tailor UAV and Munitions to potential targets and in that case you really should just plan your missions better.
Doesn’t that printed UAV looks like an RQ47?!!! 50 years of engineering just for BAe to rebuild Ryan 😉
[…] reduction of the transition between boundary layer. But only on very high value aircrafts.
🙂