French already have it in series and are firmly commited to it with roadmap defining improved ECCM and GaN based modules.. Plus there are export orders from three other air forces.. If that’s a tick in box, then it was a damn good one.
Still using the same back end though, with no clear timescale and no indication of when electronic attack will be added. That’s what ticks in boxes are for – sales, whereas genuine capability is for domestic defence capability.
It all depends on interpretation. If your source says that Mk2 is ready by 2019 and even if we believe it, what exactly does it mean? a) Ready to be tested? b) Ready to be deployed? c) Already produced and in service? d) Produced, in service and with full capabilities? Biased fanboys like yourself tick d) without thinking but the sad reality is you don’t have a clue… currently the Mk2 is not much beyond vaporware, just like the further evolution of RBE2-AA currently developed by Thales under the PEA (Plan d’Etude Amont) program.
“Two successive releases,” implies release to service. The functionality of the Mk2 has been tested on Bright Adder for quite some time.
Mk1 has old back-end. Mk1+ is likely to have improved processing power, better resolution in SAR mode and software update. Mk2 should have new capabilities, most likely beyond the possibilities of current hardware, therefore it’s logical to expect at least a revised or even a completely new back-end.
Mk1 hasn’t been mentioned to. Only a Mk1+ grade is going to non-UK partners. Mk2 is a software update to the new architecture and linkage with DASS.
Captor-E will likely never be more advanced than RBE2-AA. Thales has some solid time advantage here – unless DGA give up commitment on further Rafale upgrades, I cannot see that happening.
Yeah right, in your dreams. Why? Thales rushed it into service and then sat back for quite some time, Captor-E development has been going on in the background all that time, in one guise or another, starting from around when the Rafale first came out. What we’ll likely see is a leap-frog situation.
No. Captor-E is largely based on Captor-D.. It isn’t a Captor-D with new antenna only because such transition is not possible – some mods to high power transmitter and processing unit are required in order to adapt them for an active phased array.
Not according to the information posted already. Both Mk1+ and Mk2 have a new architecture. It’s isn’t Captor-D with a new antenna because it’s not a tick in a box solution like the rushed RBE2-AA.
So what’s the fundamental difference between a PESA back-end & an AESA back-end?
Nic
The latter has an expanded architecture with extra processing power to run electronic attack and high bandwidth communications, as well improving detection. It’s the difference between buying a supercar and modifying a Honda Civic.
Different philosophy , different tactics , different planes and characteristics. That is why comparing A to B on fact sheet won’t bring much.
Very low fast flying ,hiding in the clutter with deceptive jamming , is another form for stealth. A Look down -shoot down capability, does not imply ability to detect and track a very low flying LO object within the clutter, not mentioning how challenging the environment is to both EM and IR seekers. Radar theoretical horizon, based on earth curvature with zero relief and no cluster nor EM interference ,is just that the maximal theoretical horizon. Add relief and EM reflection and clutter and the theoretical range deprecate fast.
Detecting and shooting down from above a fast low flying jet , is way much harder than one imagine, Kosovo experience , or even more recently in Lybia showed that even with total air superiority , AWACS and cover in the air, low flying planes evaded detection long enough , even with poor electronics.
There are of course draw backs , fuel consumption being one, exposure to hazard of low flying being another. Good mission planning is a must. Gulf war is rich of bad experiences in that domain, .Sending 2 successive waves on the same ingress route over an undetected enemy division. First wave caught division off guard and went unchallenged ,second wave was not so lucky. Or flying low ,but not low enough , like the initial tornados raids, popping up at worst possible spot to release their weapons . Some got cold feet after that !,but the blame is less on low flying than poor planning and over confidence .
I personally experienced regular pairs of fast low flying M2000 when in my summer house in a relatively flat country side. Well the expression they are gone before you hear them is pretty close to the feeling . With some getting used to, you can get a glimpse of them ,but honestly small weapons ,shoulder or short range SAM has null chances to engage, and I must have been on a hill 100 meters above the rest.
So it is risky business , as much or less I guess than flying at altitude in a VLO airframe in contested airspace . But that is my opinion.
On a side note, this obsession with an improbable extrapolation of the range for airborne launched MICA from VL MICA is getting really tiring. It was proven wrong ,and remain wrong even for low flying launch at +900 km/h ……compared to vertical launch at 0 km/h. It is borderline intellectually dishonest or worse.
Do you know low flying planes avoided detection, or was it just that nobody was around to shoot them down. Wasn’t aware of any Libyan low altitude ops when the allies were there.
How can it be less risky than flying at altitude in a VLO aircraft? The sheer number of things that can kill you at low altitude make it more dangerous. You also make it sound as if contested airspace is only contested at altitude. What’s to stop you meeting jets at low altitude, where even an attack jet like an Su-25 will have a decent chance of getting lucky with an AAM, along with the million other threats down there.
Range is vastly reduced at low altitude. An AIM-120C has a range of 5km in tail chase at low altitude, your chance of hitting anything at 40,000ft with a MICA from SL is zero. Wrt VL vs 900kph horizontal launch. One starts from rest but points the missile in the correct direction and the energy required to get from 0-900kph is minimal, relative to the energy required to get from 900-3000kph whilst climbing 40,000ft.
On the deceptive jamming issue. Completely irrelevant against IIR or laser-guided SAMs, as is RWR. Yet another reason why there’s no point in developing expensive EW suites and then putting an aircraft at an altitude where they’re useless. It’s like taking a sniper rifle into a phone booth fight. FWIW I also heard lately about a Russian MANPADS that is comms linked to a wide variety of platforms to give them a heads up when a sitting duck is about to arrive at low altitude. The mobility and quantity of threats also increases at low altitiude. It takes a fair while to set up an S-400 and they aren’t thousands of them, and missiles are limited in quantity per unit. At low altitude, smaller missiles are more plentiful and threats can move around rapidly in jeeps or small manoeuvrable platform. You could even theoretically have people firing Igla-Ss out of helicopters, or using helicopters to place them on the top of terrain. From a financial point of view, even forcing the enemy to shoot you down with a 48H6E2 is better than letting them do it with an Igla-S or a few 23mm rounds.
Could, but RN is not going to get a full carrier worth of fighters, not unless something very drastic happens,
so its going to be pocket carrier without reinforcement from RAF that will also get a couple of squadrons of F-35B,
this will when needed double fighters at RN disposal
How big are your squadrons? 80 are on order, with a possible 60 extra after that.
Are you aware that the original RBE2 was already an electronically scanned radar, because the FAF had already anticipated that electronically scanned radars were the way of the future? That it was a PESA was a transitory step to get ahead on the AESA transition because the cost/efficiency ratio of first gen AESA modules was considered too low.
It’s not like the RBE2 was a mechanical array in the first place.
Nic
No but it wasn’t an AESA in the first place either, hence why it’s limited in still having the PESA back end. The Captor-E is a ground-up AESA design built with fully matured technology.
One example that has surfaced in the press:
Heh, so basically they’ve stooped to using CIA/NSA e-puppet tactics. Referendum on independence set for 2017.:cool:
Sometimes imperial units are better, sometimes metric. Landing with metric altitude feels worse to me.
The most capable AESA will be RAF. They are already planning how to squeeze the most out of the F35/Typhoon combination and do things that they haven’t been able to do before like Electronic attack.
I expect the SA Typhoons to copy the RAF and gees will be the best Typhoons.
Not sure the Mk2 is for export.
on EF: it’s on the very top performance wise as an interceptor, and Captor E may well be the best radar to date,
it also has the sheer mass and power to be a heavy duty bomb truck,
but the customer/Germans expected to pay for upgrades and integration has other priorities, time’s up,
high operational cost also doesn’t help making it desirable or future proof.
Perhaps it is put best to use in an AF large enough to use two types, one dedicated fighter-interceptor,
and then UAV for ground targets
Where do people get these ‘high operational costs’ from? Most sources show them to be similar to the Rafale and cheaper than the Tornado. As regards progress, the UK has got tired of waiting for Germany and will go it alone. Note that the Tories have just been elected with a majority and no Lib Dems to hold them back.
The Captor-D was obviously deemed more than enough for partner nations.. The main driver for Captor-E was to have a tick in the AESA checkbox so that the Typhoon stays at least partially relevant on the export market vis-a-vis F-35, Strike Eagle, Super Hornet, Gripen-E or Rafale. Those sheiks who spend billions on new hardware buy them like they were LaFerraris and Veyrons – they were told AESA was better so they wouldn’t pick anything without it.
Not really, the tick in box was very much a Rafale goal, hence maintaining the old back end. The RAF’s intention with the Captor-E is to provide a far more advanced warfighting capability.
Don’t say.. and which airforces have ordered these?
That’s what the ukarmedforces blogspot says, which is the best source we’ve got.
Well, that’s funny. I thought a completely new back-end was more than enough physical but I guess one always learns something new, especially from people who don’t have slightest clue.
The Mk1+ has the new back end, the Mk2 is a software update.
Just a small reminder – the works on AMSAR started in 1993 and CAESAR technology demonstrator has first flown in 2007. Today, in 2015 there is still no series Captor-E flying or even being produced, not even with old back-end. But hey, now they will have series deliveries of fully capable Mk2s developed from BrightAdder in just four years.. :applause: I can’t wait..
Hence why it will be much more advanced than RBE2-AA – more development effort, rather than just throwing some front end modules into service.
Yes. I completely ignore it.
I’ve noticed.
I still think 2019 is more likely for the all-up version, given the amount of development already done and that fact that 4 years is still a pretty long time to get stuff done and the economic situation is improving.
Ok listen,a small car with a roof rack do take more fuel, say 0,2l extra per 10km. Now build a car (50 cm?) higher around it. What do you have ? A MINIVAN…. how fuel conservative are a minivan? specially at higher speeds.
Comparing the roof rack and the minivan…..Ok you save a bit, but not very much. say 0.05 to 0.1 maybe. You can have a aerodynamic skibox which helps you here maybe 0.05 to 0.1.
THE DIFFERENCE BETWEEN IS THERE ! BUT VERY INSIGNIFICANT.
What matters are the total size that pushes the air to the sides. AT higher speeds I AGREE that it makes less air resistance to be “whole” but the bigger drag commes from SIZE.
Relative to fuel fraction the minivan will still go further. And its Cd, which is relative to per unit cross-sectional area, will be lower too
On a fighter parasitic drag slows you down the faster you go. Thats one of the reasons why a bigger fighter always has more drag@ higher speeds.
Dude, you really need to read up on Cd and understand why fuel fraction is used. Everything is relative to size. More absolute drag doesn’t necessarily mean a higher Cd between 2 different aircraft and fuel fraction is also relative to overall weight/size. Therefore a bigger aircraft, with a lower Cd and a higher fuel fraction will still go further despite higher absolute drag.
Ok about the f414g again. The only thing we have, is the afterburner effect 98k and thats why everyone think we know what engine it is (f414-400). f414in has a 6 stage engine and are probably an epe/ede variant THAT ONE also has 98kn afterburner.
Find me the spot where an updated engine spec. are…. because the only thing i ever saw was that 98kn wet. NEVER the dry thrust.
Wet thrust is related to dry thrust for a given quantity of afterburning.
Higher threat activity, heavily jammed environment, the need to kill a HVT that cannot wait threats to be treated with rain of AAM and ARM, among other..
That’s a stretching scenario but even them the target would have to be outside the range of naval cruise missiles. You’re also exposing yourself to massively more risk than a F-35 sneaking in between the reduced radar coverage zones.
Beam riding isn’t exactly the best guidance method against highly maneuverable targets, unlike proportional guidance.
Furthermore, and again, ground tracking systems are subject to aircraft countermeasure and environment (weather). Visible spectrum systems won’t see anything at night or in bad weather (i.e fog) and are still vulnerable against visible spectrum flares.
If the guidance method works, it works. A laser isn’t subject to countermeasures and no current fighter has the sort of countermeasure that would be effective against IIR missiles. Relying on weather for protection is risky and most modern optical systems also work in IIR, which isn’t easily fooled by flares.
Furthermore, a configuration on which a high point has unlimited visibility are somewhat unlikely to happen, and a reactive maneuver from the targeted aircraft could allow it to switch between valleys in a relatively short amount of time.
Unlikely? Yeah, until it happens. If you know you have areas covered by radar SAMs, then that a good cue as to where you’re going to put MANPADS and SR SAMs.
Modern SATCP system are very dangerous indeed, but not uber weapons. http://foxtrotalpha.jalopnik.com/this-shoulder-mounted-sim-trains-pilots-to-evade-surfac-1702680164
Evading a fake missile doesn’t mean you can evade a real one. It also appears to be simulating older IR seeker variants.
45 kilometers.. that’s around 2 minutes for a fighter. That’s short, not mentioning such radar’s position would be well known pre-flight, or detected during flight at the worst case, updating SA immediatly and permitting the crew to rearrange their route.
Not mentioning either your calculation works on completely flat terrain, like, water. Unlikely to happen on a continental type environment.
Two minutes of risk. Now put the SAM radar on a hill or mountain, or use a higher mast.
Why would they shot them down ? It’s all about getting undetected here.. not taking stupid opportunity shots.
Also, while SL launched missile suffer from high drag at low altitude, it is the same with high altitude launched missile reaching higher density air layers when targeting a low altitude aircraft.
The missile coming down has the advantage of gravity and higher initial speed though.
Furthermore.. what do you call little speed ?
Again, typical speed for a low level run of 2000D or Rafale is between mach 0,9 and mach 1 on optimal cases (i.e egress without heavy weaponry)
But the missile has to turn upwards losing most of that energy.
.
Great news, because Mirage 2000D’s SERVAL/SPIRALE/CAMELEON systems and Rafale’s SPECTRA suite were designed with low level penetration flights in mind.
Yes but it’s completely useless at jamming the kind of SAM threats that one encounters at low altitude. It can detect the missiles after launch but that about it, excluding the use of flares against last gen IR SAMs. Factor in a modern short-range SAM and they’re both as good as dead and the likes of a 23-35mm AAA will down them in a hail of bullets with zero warning from out of nowhere.
@Lukos
NOT!
I’m only going by what sources are indicating. I don’t see it being left to the early 2020s because that just too late from many perspectives.