but surely a low RCS aircraft will be as difficult to detect using such a passive system as it is using normal AD radar systems anyway?
You taking the p**s?
X-band = 8-12 GHz
Medium wave radio = 0.5 – 1.6 MHz
Don’t forget the old mantra “there is nothing invisible to radar below 2 GHz”.
Has anyone ever actually claimed, that Stealth aircraft are undetectable to radar ?
Very different from being able to mount an effective defense against them.
Here is an article claiming that defence against stealth is just around the corner
There are numerous means of effective defence against VLO aircraft.
Just because the stealth-mafia on here don’t realise it, doesn’t make it any less factual.
F-14 is not a viable fighter for today. it is too heavy with tiny fuel capacity relative to its size. It has to be completely redesigned.
No it doesn’t.
Its range, speed:range and payload:range are all more than adequate for its primary job – guard the fleet.
Indeed, its range, speed:range and payload:range are all far superior than its supposed ‘replacements’.
You can argue WVR maneuverability – however, if the USAF and USN are going to stack the deck toward BVR with F-35 (and to a much lesser extent with F-22), then why does the F-14 not fit in?
At BAESYSTEMS the replacement RMPA studies started on the very late 80’s. By 93-94 the favoured solution was FLA (A400M) which was expected to be given the go ahead in 95. But even this was not going to be available in RMPA form until 2005. So the MR2’s had to be O/H to span the gap………. A400M did not start in 95 and the RAF really liked the MR2+ O/H ……….and that’s how MRA4 started.
Ah – I suppose in hindsight, waiting for 400M would have been the right call – but not given projected timescales.
Pity the electronics weren’t of modular design that would fit into an A400M (with relatively few mods).
Its easy to say “just convert an A321” ( I was involved in this study in 92) but in reality its far from easy;
Fair enough – if you were on the study team, I’ll not dispute it as you’d have examined it in far greater depth than me.
perhaps they also got it right going jet powered C-2 instead of the A400 thats turboprop
same size, same cargo
Very different take-off field lengths.
That is not a small detail in design – its a very fundamental driver. 🙂
Is there any better upcoming tech to replace riviting in airplane manufacturing, in the future? it got alot bad caractaristics…
Oh yes.
Friction Stir Welding and Laser Beam Welding* are two big ones.
The current craze for composite wings may well become a passing fad (at least until there is production capability with Carbon Nano-Fibre infused resin). Right now – a metallic wing built with FSW or LBW would be around as light as a composite wing – without many of the associated issues.
Engine maturity is not the only reason Boeing shelved the 737RS and Airbus went with NEO. 😉
*LBW is already used on A380 – probably also on 787.
There were no off-the-shelf aircraft available at the time except refurbished P3s.
I think that Aardvark’s point – which I agree with – is that the Comet airframe should never have been considered for the job.
Why were the systems not considered as installable items onto an A400M airframe (then FIMA) for instance? For that matter – if FIMA timescales were a killer why not just use an A320?
Increased flexibility, reduced cost and more airlifter airframes (if using the A400M option) into the bargain. Whats not to like?
This was the impetus and reasoning behind the common Support Aircraft program. The plan was to replace AEW, EA, ES, EW, IFR, COD, ASW, ASUW, etc with a common airframe that supported all the various rolls with little customization.
If you had a propfan powered lifting body in a similar (if smaller) vein to the IRKUT DOLPHIN* (albeit with folding wings); you could probably get sufficient cargo in to meet some last mile Army needs too, as well as medi-vac and possible short range civilian freighter (like a slightly bigger version of the Shorts Skyvan).
It would also be a good proving ground for blended-wing-body and propfan studies in Western aerospace.
*warning pdf
Am I the only one that thinks a real maritime SAR aircraft should actually be able to land on the water? :confused:
A modern (and probably bit bigger) take on the PBY Catalina.
Now I want some reason to support such senility and why us didn’t foster something new?
Low speed propulsive efficiency would be a big plus towards turboprop/propfan.
As others have said, endurance ranks far above dash speed for AEW requirements.
RCS is completely a non-issue – it has a honking big radar emitting (or at best, a big dirty housing reflecting) – and the Navy would rather have the enemy direct pot-shots at it than at their billion+ dollar ships.
If you want to predict the future of Navair AEW – think along the lines of turboprop/propfan UAV (or dirigible) with bigger radar than E2, that has extended loiter time relative to E2 and has significantly higher service ceiling than E2.
The data is then put through limited onboard processing before a compressed encrypted stream is sent back to the SAG/CVBG on datalinks where full processing and dissemination of information can occur.
I know Marshall’s of Cambridge offered something similar and I see them getting sub contract and conversion work but maybe this rather open ended solution from Lock-Mart is the cheapest way into a credible long range MPA and ASW type. We have the airframes and we have significant sensors in storage.
Or do people have other ideas…
No thanks.
Simply because it is Lock-Mart proposing it.
Their word isn’t even worth sh!t when it comes to cost control.
Seahawk is bang on the money.
And another nice question is, Was the Berkut used as T-50 testbed?, or the T-50s technologies were tested in the Berkut program?
I would say with absolute certainty knowledge gathered in Berkut will have been carried to PAK-FA.
It is very unlikely that many things above component level will have been carried over though.
IMHO, Airbus should have updated the A330 with GEnx engines and a 540,000lb MTOW and not even done the A350…..perhaps they can still do it since the 330 has a wing area of 3890 sq ft and the A350 is 4700, maybe they can fit different niches. IMO, an A330 with a low price and a 6,000-6,500 nm range with real payload would be a world beater.
They have talked about an A330NEO.
Talk is done in whispers though to avoid A350-800 cancellations.
They may follow through eventually, but only when A350 is in service and airlines are liking them I would think.
You are right though – they should have split their market as:
A320(family) >> 150-220 seats
[A30X >> 150-250 seats]
A330 >> 250-400 seats
A350 >> 400-500 seats
A380 >> 500+ seats
‘cos at the minute, its:
A320(family) >> 100-220 seats
A330 >> 250-440 seats
A350 >> 270-550 seats (it’d be a very cramped 550 people though)
A380 >> 500+ seats
That is a big overlap of A330 and A350… with A350-1000 essentially being a different aircraft.
By the way, where are the Japanese orders for the A380?
As far as I know, only Skymark with 4 orders is the entire Japanese A380 portfolio.
Air Japan are short haul only – and all (relatively) small twins. Air Nippon are the same.
That leaves (any more I’ve missed) ANA and JAL. JAL are all Boeing. ANA could be the one – but they’ve went down the large twin route so far – scrapping a proposed A380 buy due to weak passenger numbers.
Maybe if the Europeans would allow more Japanese car imports……..hmmmm.
Ye reckon?