Well sadly that’s all we’ve really got for these two. From the looks of the post I quoted, I’m not the only one who registered similar claims by the French.
Dead link. The wiki statement of M1.82 references Ayton, Mark. “F-22 Raptor”. AirForces Monthly, August 2008, p. 75. Retrieved: 19 July 2008. The source for the Pentagon paper stating M1.76 I saw on f-16.net.
The 2009 SAR report gave the baseline estimate Vmax/optimum alt. in mil power as Mach 1.76. There most likely is some variation in those numbers due to engine life allowances, gross weight, vagaries over optimal altitude (optimal for what?).
All the things i’ve read about F22 vs Rafale dogfight in 2009 at the “Air Tactical Leadership Course” was: 6 dogfight, 1 win for the Raptor and 5 draws. I never saw someone serious with reliable source said 7/1 for the Rafale, the famous video of a Rafale that shoot down an F-22 is considered a draw because the rules of engagement was not respected.
This vague quote lifted from Air & Cosmos posted over at F-16.net about the F-22 “winning” , is silly. First, who cares? By now, both the Rafale and the F-22 have most likely lost simulated engagements to each other and quite a few other aircraft.
Second, whatever the numbers (and I have a suspicion who made the 7-1 claim in favor of the Rafale, a certain blogger with as much credibility as those posting Youtube analysis), a “guns only” DACT exercise is about as reflective of respective combat capability of the two aircraft as a competition between the Household mounted Cavalry and the Governor General’s horse Guards to compare the UK and Canadian Armies. Those types of DACT exercises are to hone pilot’s ACM skills.
Too much emphasis is put on the DACT results vis a vis: the Rafale, F-22, Typhoon. (DISCLAIMER- EVERYTHING BELOW IS OPINION, based on anecdotal evidence and the few specifics released):
I have little doubt that the Rafale and F-22 are very much a match for each other low and slow, the Raf holding a bit of an energy advantage at those speeds with the F-22 being able to counter with it’s high alpha controllability (the Typhoon is a bit lacking in this particular regime other than acceleration)
At traditional dogfight speeds (mach .65-.8), I doubt that any hold a decisive edge. Both the Rafale and Typhoon likely hold a bit of an edge in sustained turning, with the F-22 having slightly better instantaneous rate and acceleration.
From what has been stated about the design criteria for the F-22, both the engines and airframe were optimized for supersonic performance. I would expect F-22 to hold the advantage high and fast over the other two with the Typhoon a close second.
Yes and not, a F-15C w/o conformal tanks weight less, a F-15E with them more.
But given that any stealth plane have to carry all fuel and a part of weapon load internally I’ll call them apples and oranges.
No, the F-15C. The original empty weight figures of 28,600lbs are 30 years old. The F-15C has added AESA, structural modifications, the MSIP II upgrades that started in 1985 (internal EW, countermeasures, JTIDS). The “C” has gained enough weight over the year that the c.g. of the aircraft shifted leaving the F-15C a bit nose heavy (hence studies commenced in 1991 to remove some of the 250lbs of ballast in the nose). The F-15C’s empty weight has crept up to nearly 31,000lbs.
its nearly the same size as the f-16, but weighs more than the f-15. check it out yourself the empty weight.
the chinese j-31 is what the f-35 should’ve been.
Based on what? The wikipedia pages? No, the F-15C currently weighs more than a ton more.
even 1sqm rcs will be detected at hundreds of kms. a competent rival can plan accordingly. 4ET has weight of 7tons. 2ET will be 3.5tons.
Another operative example that this guy has not idea what he is writing about. 2 US 610 gallon EFT weigh in excess of 4.4 tons (fuel+EFT-more with pylons, as the F-22 does not carry them without EFT)
each engine of EF has 6400kg non afterburning thrust supporting airframe of 11.5tons. F-22 has practically twice the weight without twice the non afterburning thrust. AAM semi-recessed does not add that much drag. you can see this thing in airshows where F-22 use full afterburner thrust at low altitude. you wont see that much flame from Su-35 at low altitude.
Wrong again, The Typhoon has 27,000 lbs of dry thrust and and empty (operational) weight of 24,200+
The F-22 has an empty (operational) weight of 43,430lbs and an estimated 47,000+lbs of dry thrust (the F119 thrust figures are still classified, commentary has put the dry thrust between 23,000 and 26,000. Have seen 23,500 mentioned more than once).
Dry-empty thrust to weight ratios are nearly the same.
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The bump after the intake is present in the Gripen C as well, but it looks like it is longer. The intakes have the same shape as well (don’t really look much bigger from that angle).
The most noticeable changes are the IRST, the APU inlet at the base of the tail, and two sensors where the canard meets the inlet on the side. Wider aft fuselage- less noticeable area ruling (could be angle).
Regarding the Danish evaluation
Does the document state why 34 EF-2000 or 38 F-18E/F would be acquired? Why the different numbers? The document states the difference in performance/parameters is marginal.
Two reasons are given: airframe life 6,000 hour vs 8,000 hours and this: “identified a need for 28 Joint
Strike Fighter airframes, 34 Eurofighter airframes and 38Super Hornet airframes, respectively, in order to perform the same portfolio of tasks”
Thus they assuming that considering the 30 years time period, some of the EF and SHornets will reach the end of their fatigue life so attrition replacements are most likely figured in. It also appears that they feel more of the other two are needed to meet fulfill the mission requirements as opposed to the F-35.
Ongoing readiness issues, not surprising considering: average fleet age 27+ years old, fighter fleet ~22 years old (without A-10C counted), tanker fleet 40+ years old, bomber fleet average ~39 years old.
Those interested in average age for each type:
http://www.airforcetimes.com/story/military/2016/01/19/worn-war-birds/78860920/
Errh..no , Andrea Nativi, Pietro Bonsignore, Fabio Coniglio and a lot of other serious professionals on field of italian defense publishing.
And no, the continuation of F-35 development made a lot of sense just because the introduction of some counter stealth technologies, not sufficient at all to negate the huge advantage of VLO planes but surely enought to force a reconsideration about tactics and modus operandi of said planes when they have to face them.
For the rest, it was not that development of what would become the F-22 started in 2005 or even in 1998 when the F-117 shootdown happened: it started much more earlier.
So when they became fully aware of the problem and it took some time for it even after Kosovo war, the project was near to completion so what would they have done, in your opinion? Scrap all the program?
Or instead keep on trying to find some feasible solution or at least try to salvage something from the project?
They chose the second one, and in the end they obtained not the Air Dominance Fighter they dreamt on at the beginning but almost an excellent 5th gen Air Superiority Fighter able to confortably operate on high altitudes that the F-15C would even find difficult to reach.So , let’s say that it ended way better than the great majority of those wunderwaffen programs they carried on during the last phase of the cold war and even more during Bush sr and Clinton presidencies that ended regularly in big money for nothing.
I cannot stress this enough, your rationale for why the F-22 program was curtailed is flawed. It had nothing to do with:
1. advances in counter stealth technologies
2. not having a credible mission- the USAF reiterated the “minimum acceptable risk” at 240 F-22, several officers ruined their careers publicly advocating this to the ire of Gates
3. The design features of the aircraft (with a caveat)
It had everything to do with: Gates claiming “next war-itss”. Basically sacrificing the F-22 to meet his requirement for increased drone funding and MRAPS (great investment in overproduction-we are giving them away now). He shut his ears to anything that was not of immediate use in the war on terror. The F-22 also has two great design weaknesses, it is very expensive and time consuming to upgrade the software code, and upgrading early software/hardware blocks is equally expensive and difficult. Just bringing the 140 or so PAI and BAI and attrition aircraft up to increment 3.2 has cost billions, now the fleet is undergoing RAMMP to fix structural issues inherent in the abbreviated production run (early blocks that would have been used differently or for less hours are part of the combat coded fleet). All told, 11 billion spend that could have gone into building block 40 and beyond have to be spent to bring early blocks into commonality due to insufficient numbers. The Raptor had two clear failings, software modularity and politics, not the points you are harping on.
$400bn for 2,450 aircraft is equivalent to a unit procurement cost of about $160 mil. Not cheap but far from scandalous. The 4 year rightward ‘reset’ of the timeline too, while a PR nightmare for the program is hardly a ‘scandal’, especially relative to other fighter programs around the world. Similar case for the development cost (its over budget by 30%).
Applying the same logic to the three major European fighter offerings would further this point:
Consider total program cost of the Rafale- development cost, rebuilding the early production M F1 variants, the expensive upgrade to F3, now F3R= PAUC equivalent of 160+ million in 2011 dollars (based on 286 aircraft operated for 40 years). To meet that procurement total, the total Rafale production will have to nearly double.
True to a point, unfortunately they are also less important from financing standpoint. Most politicians don’t care what happens 10 years in the future: they’ll rather save 1 billion for next budget year, than 2 billion for budget year decade in the future. Hence, if and when the total procurement numbers are cut, most likely it is done by cutting production RATE rather than production SPAN. This is not a thought exercise, that’s how it has happened with nearly every military aircraft program over last 30 years.
True, this has already occurred with the F-35. This has been eased somewhat by the addition of orders from non-partner nations and cost saving measures initiated by L-M. I don’t think that the USAF production will reach the planned 80 per year. However, if the cost curve continues to drop as it has, then a rate approaching 60+ for the USAF per year and a total buy in the range of 1,300- 1,500 F-35A for the USAF is plausible.
Oh no, that is not how politicians handle things :p What good it does for a politician struggling with BY2022 to consider what happens 10 years in the future? No, they whip out the cheese slicer and cut little bit right away – like they have done elsewhere in same situation, and what they indeed already have done with F-35…
Again, final numbers produced are NOT as important as the ramp up for driving down the costs F-35 partner nations will pay. It may impact FMS buyers costs, but not significantly enough to drive away buyers (as we’ve seen). If the F-35 approaches the peak production numbers originally planned, the affordability will drive up final production numbers as well. Considering the order book to date and the addition of customers (Japan, Korea) not originally included, I’d say that regardless of who the buyers are, the F-35 will reach somewhere near the planned 3,000 in the 20+ years it will be in FRP.
No one with a sane mind and with some rudamentry understanding on economics scale believe that US will produce that many F-35’s.
1763 is a wild stretch. There are allready dire reports that the F-35 will have to be upgraded in the not so distant future to stay in the game.. guess what, that will cost moar $$$.
And with the current status of F-35 program.. well McCain did mention something about over budget and delays.. can’t remember what he said, probably nothing important to worry about.
t.. right Jessmo23?
The F-35A program of record stands at 1763, let’s stick to facts. Where are the Dire reports you are referring to? Like some hinting that an aircraft expected to be in production for the next 20+ years will need to upgraded to stay relevant? Color me shocked! I assumed that manufacturers designed a basic airframe and avionics and built it until obsolescence. After all isn’t what they’ve done with the F-16, Rafale, Su-27? Oh, what….
Well that’s fair enough but even having heard some of these variables, I still find their numbers incomprehensible.
MAWS does the same as DAS as regards missile warning, it just isn’t passive on the other aircraft. Is AAQ-40 any better than G4? It’s a lot smaller. If Storm Shadow were the case, then surely the F-18F has JASSM, both of which are launched from outside SAM range.
PIMAWS would be similar in some functionality. It is not the actual AN/AAQ-37 IR cameras that make the system so capable, it is the processing behind it. Besides the missile warning, countermeasure deployment, navigation, and blue force red force tracking, and has shown capability for ground fire detection and classification, and as NG has stated that they’ve only begun to scratch the surface of what future applications of the DAS system will be. Considering the advances in shape recognition software there may be some functionality for that already included or planned.
As we hear often here on this forum, “what so special about DAS, EOTS, the APG-81. X or Y aircraft have something like that”. It isn’t just the inherent capability of the hardware (FoV, resolution, T/R modules, and on and on), the processing power behind the sensor and level of integration make one system comparable to another.
That is exactly what was done. In the report, the segments where they discussed specific capabilities to justify the scores have all been scrubbed from the document.
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In regards to overall evaluation approach for the survivability and effectiveness.
Yes I get it, I’ve read it several times through. The redacted sections on mission effectiveness and survivability are quite short for each. The Swiss report, by comparison, explained the rationale behind the score on each section, assessed the strengths and weaknesses of each candidate in meeting mission requirements. I’m not saying that the results are incorrect but rather incomplete and lacking in specifics on why the aircraft were scored as they were. In my opinion, it would lend credibility to the evaluation if there were indications that there was a separate classified annex detailing specific threats modeled and what criteria led to scoring the effectiveness in DCA, for example.
Why are there calls for restarting F-22 production if F-35 is said to be so capable in the A2A role? I don’t see the point.
Because there is no one mission set in the A2A role. The F-35 can be very well capable of defeating current and projected threats and still not meet the needs of the USAF in an expeditionary role. The F-22 brings several superlatives to OCA missions that the F-35 lacks; high speed persistence and with it the ability to provide air cover over a larger area, APG-77 is a larger, more powerful radar, and magazine depth (8 missiles vs. 2 [eventually 4; maybe 6 someday])