Looked like something from the 60’s.
What exactly about it looks like it is from the 60’s?
It looks pretty much what it is, a design from the 70’s that first flew in the 70’s.
Two things I found interesting on the Mirage 4000 was the sideways opeing canopy and the massive vertical tail.
Does anyone know what the wing sweep angle of the Mirage 4000 was?
I seem to recall the original Mirage III was 60 degrees, while the Mirage 2000 was 58 degrees.
Some pics of the Dassault stablemates:
This whole thing started with the government sniping at its own people!
They keep them in the city and then they and the Russians can say “oh well, we tried. You can’t say we didn’t try…” They will then increase the bombardment under the pretext that they gave anyone truly innocent the chance to escape.
This is a pretty absurd post, with all due respect Mrmalaya.
The BBC Effect…
Would suggest reading the actual HASC report. The impressions Breedlove gives are far different in full context than what this article suggests. Dave Majumdar uses some creative cut and paste on the actual comments of Breedlove (as is Majumdar’s habit since leaving Flightglobal).
This whole section is utter B.S.- “One area that he highlighted was the North Atlantic where the Russian Navy massively increased its activity to nearly Cold War levels.” The Soviets had around 170 submarines in 1989, today there are roughly 38 nuclear submarines (SSBN, SSN, SSGN) active, fitting out, or being re-activated. There are around 20-22 Conventional submarines in service. Yes, sortie rates are way up over the 90’s and early 2000’s. Claiming “nearly cold war levels” of deployment even in the North Atlantic is an exaggeration. This article is the typical “chicken little” piece whipping up fears for no reason.
Breedlove has gained a rather notorious reputation over the last few years for hyping stuff up.
He’s been banging his drum to a rising crescendo.
Fogh Rasmussen and him seemed to be having a competition with each other at times, trying to outdo each other to ever dizzying heights into the realms of the ridiculous.
I guess the bills still need to be paid after retirement…
You get the feeling Goldust and Byoin are familiar with each other….
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Thanks for that. I had been looking for this for a while, and had also wondered about the statement about the canard being able to be moved in flight.
What does that tell us about the original engine fitted to the Mirage?
It tells us various things actually, mostly that customers wanted options, a lot of it for political or industrial reasons.
The Avon powered Mirage was looked at by Australia, as they had used an earlier version of that engine to e=re-engine their licence built CAC Sabres, and there was some political influence apparently to get a British component on board. Remember this was really the first time Australia had moved away from a British fighter (apart from perhaps WW2 and all the expediency that entailed) and was incidentally the first fighter used, and licence built in Australia that had been designed in the metric system.
The Australians were interested in the more powerful ATAR 09K, but by the time a decision needed to be made, it hadn’t yet been fitted to a Mirage III airframe, and thus the lower risk and lower powered 09C was selected.
” Thus by early May it was apparent that the expected advantages in takeoff performance, rate of climb, and range for the Mirage III with the Avon Mk67 were not a significant improvement over the Mirage IIIE, whereas overall performance above 40 000ft was somewhat inferior, although the Avon version was able to achieve higher speeds without afterburner at altitudes below 45 000ft. On the other hand, the development potential of the Avon Mk67 engine was limited to the fitment of a larger tailpipe (36″ diameter as opposed to 28.8″ in the standard engine) and the expected benefits to thrust and fuel consumption were not comparable with those available from the ATAR 9K.
The ATAR engine offered important additional benefits, being lighter and cheaper than the Avon and was perceived to have benefits due to ease of manufacturing and servicing together with simplicity of operation…”
Incidentally, 160 ATAR 09C’s were licence produced in Australia in the end, with a final local content of 85%.
Here is an excellent reference book, detailing much of the above, of the Mirage story in Australia:
http://www.radschool.org.au/Books/the_raaf_mirage_story_opt.pdf
The primary driver for the selection of the J-79 in Israel was military credits/aid from the US, as well as the existing use of that engine by the hundreds in Israeli service, and has been discussed above.
By the time South Africa was re-engining the Cheetah (and Mirage F-1), the Mirage III had been in service around the globe for about 30 years.
In the meantime, the rise of the turbofan had occured, with no new fighter designs then being looked at featuring turbojets.
It is also worthwhile recalling that South Africa was casting an eye around for a modern turbofan to power the Carver, and the re-engining of the Cheetah and Mirage F-1 must be looked at in that light.
It is also worthwhile remembering that whilst looking around and fitting a turbofan to the Cheetah, Mirage F-1, and considering it for the Carver, the ATAR Plus programme was on the go, where certain elements of the ATAR 09K50 were being redesigned (with new compressor, new turbine, and new electronics) to achieve a thrust increase of 10% plus.
The M4k had a very high thrust available, as the Typhoon or Rafale have today (actually, they are a league above, but it is normal as they are another generation)
I’m not so sure of this last part.
What was the rationale behind the Chiliean Mirage 5 EV basically being a front fuselage hybrid with the Mirage F1?
Was the intention simply better avionics, or was the intention to arm it with a better beyond visual range AAM?
I’ve always found it to be a very interesting model. With its air-to-air refuelling probe, more modern avionics, and more powerful ATAR 09K50, it was the most capable Mirage III/5 model out there until the advent of the Cheetah C.
Merci Guillaume, Please please, give us a hint of what was there 🙂 extra fuel … ?
It is a hybrid, partly a Kfir airframe design, with the fuselage starting to widen at that junction that was built to house the J-79.
All the original SAAF Mirage airframes were utilised to build the original Cheetah E, R reconnaissance models, and D two seaters.
There weren’t enough left over for the Cheetah C programme.
The Cheetah C utilises portions of the Kfir airframe, but in a slender new build rear fuselage that doesn’t need to somehow accomodate the bulkier, heavier J-79 and its associated cooling requirements.
The front fuselage portions are also new. It’s a very interesting hybrid. The differences between the air-to-air refuelling probes and their position also show there are differences beneath the skin of the Cheetah C and Kfir C10, apart from the obvious differences in the front fuselage/nose, and rear fuselage.
Hence my inference to the “big cats”. I was referring to the Pantera which was equipped with the ATAR 09K50 too. The rear fuselages of the Cheetah C and Pantera are different even with the same engine, which are different yet again from the Kfir. The Cheetah C fuselage in the cockpit area is also deeper than the Pantera.
The J-79 installation was an Israeli expedient, based primarily on supply, military credits, and existing maintenance facilities and supply lines due to them already using hundreds of airframes with the J-79. The Israelis never used the most powerful of the ATAR’s, the 09K50, so I suppose that made sense to them.
I’ll reiterate the point that due to the engine and its associated structural/cooling requirements, the Kfir must weigh more than any ATAR powered model, even the heavier, more powerful ATAR 09K50 editions.
The entire Mirage III development family is very interesting, with airframes turning out quite different as they developed. Even the wing planform changed, and it would have been even more had one of the Advanced Combat Wing designs (there were I think 3 different versions) on the Cheetah been fitted to service aircraft instead of only test aircraft. Again, that was a budget/Cold War ending issue that stopped that.
It is testimony to the wonderful adaptive original design by Dassault. As can be seen, the end of the line of the Mirage III family are very different beasts to the original. Dassault got the basics very right.
Sorry, Do you mean that small bump visible on the fuselage spine profile ?
Other MirageIII/5 variants used the Atar 9K50, Like the Venezuelan Mirage 50EV, or the M 50FC/CH that became the Panthera.
I do mean that bump, Serge, and as you’ve correctly inferred, the other Mirage III airframe fitted with the ATAR 09K50 doesn’t have that same feature…
hello mein kaiser,
could you tell me more about the cheetah vs kfir’s difference in terms of structure?
it seems that you are implying that the cheetah airframe is better suited for all the modern upgrades (canards, radar, etc)
Hello, my sizzling delicious friend.
I’m not saying that at all.
Lion cubs and cheetahs aren’t the only big cats…you get others, such as a panther for example. All cats, yet all different…;)
For example, have a look at my picture on the last page of the Cheetah C, the one taken from the three-quarter view.
Look at the midway point of the dorsal fuselage, near the low profile airscoops.
You will see something interesting regarding the fuselage structure that hints at something.;)
I’m saying that the slightly more powerful J-79 as fitted to the Kfir was not a better aerodynamic match compared to the ATAR 09K50 in the airframe we are discussing…
You’re right, we can’t assume anything about either aircraft. I only came rushing to the Kfir’s defence when a poster above described it as a ‘POS’ aircraft – I’m almost pretty sure it isn’t (and very few combat aircraft can ever be described as such?)
I don’t think it is either.
I’m just going from what has been told to me….that the J-79 wasn’t the perfect match, and that the relatively marginal extra thrust (over the 9K50, not the original 09C admittedly) was eaten up by the heavier weight of the engine, and extensive modifications (wider intakes, cooling, shielding, wider rear fuselage etc) needed to install the engine.
It made perfect sense from an Israeli POV, as I’ve mentioned, due to the credits available from the US, and the fact that the Israeli airforce used the J-79 by the hundred.
But I wouldn’t assume it lead to a better performance per se, taking all things into consideration.
EDIT: My main, admittedly convoluted point about the Cheetah C vs Mirage III empty weight applies to the vanilla Kfir C2 and C7.
Official weight of the Mirage 5 is 7150kg.
The Kfir C7 is given as 7280kg.
Yet even a cursory examination will reveal the J-79 is 300kg heavier than the Mirage 5 ATAR 09C. And we haven’t even started to address the Kfir’s obviously different, beefed-up stronger undercarriage, additional heat shield requirements, cooling requirements, and additional structures such as canards and wing dog-tooth extensions.
Either way, the last/latest of the Mirage III design line were bigger, heavier, far more capable aircraft than the originals were….but that is to be expected with the march of time. 30 years down the line, give or take, a development thereof was a multirole fighter, capable of strike missions with PGM’s, and capable of using BVRAAM’s out to about 60km, and yet also having helmet guided short range AAMs for the merge. That capability was not to be sneezed at 20 years ago by anyone, and shows what can be squeezed or wrung out of a design.
On the subject of weight:
It is interesting to view the cockpit position of the Mirage III and developments through time.
The original Mirage IIIC fighter had the rear of the cockpit that started slightly behind the air intakes.
As is well known, the multirole Mirage IIIE had a fuselage extension (about 300mm), bringing the rear of the cockpit in line with the air intakes.
The Cheetah C has a further fuselage extension, with the rear of the cockpit now well forward of the air intakes.
The Mirage IIICZ has an official empty weight of around 6400kg.
The Mirage IIIE had an official empty weight of 7050kg.
The Cheetah C is largely redesigned, with a maximum takeoff weight a full 3 tons heavier than the Mirage IIIE.
It has slightly a slightly enlarged wing area courtesy of the dogtooth extensions instead of the traditional slot.
It has a different, beefed up undercarriage.
It has canards.
It is longer, and has an air-to-air refuelling probe.
It has a heavier, more powerful engine.
It has an internal jamming suite, multimode radar and electronics.
Different control motors for its flight system.
Cockpit canopy…
The list goes on….
Take a look at the pics of the two aircraft below: A Mirage IIICZ and a Cheetah C. They’re almost two different aircraft, sharing the same layout.
The 6600kg empty weight given on wiki for the Cheetah C is fiction, as is the original Kfir empty weight (canards, heavier engine, cooling/heat shield requirements etc) when compared to the Mirage 5 it is based on…
And the developed multirole Kfir C10 will be that much heavier yet again.
Ultimately, if the Kfir has a greater payload and range, it can be excused for having a greater empty weight, surely?
Why do you assume that?