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Subject: Question regarding Mirage III
Aussiegunneragain    6/20/2009 12:14:30 AM
I was wondering whether anybody could clear something up that has been bothering me for a while. There are various sites on the internet that states that the Mirage III had an initial rate of climb of about 16000 feet per second. Considering that types with similar TWR's, speed etc like the Mig 21 and F-104 had initial ROC's of between 30,000 and 50,000 feet per second this seems very low, especially given the Mirage's big wing and consequent low wing loading. Can anybody confirm for me whether the internet sites are correct and if so, explain how the Mirage had such a poor climbing performance?
 
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DropBear       10/12/2009 1:03:47 PM
Mirage1110 standard climb speed of 400knots (with afterburner deselected) gave an initial rate of climb of 25,000 feet per minute.
 
Max rate of climb (afterburner engaged) at 450knots ( 0.95Mach) gave a rate of climb of 50,000 feet per minute.
 
Sourced: page121, The RAAF Mirage Story. 1989. Susans, M.(WingCmdr).
 
 
 
 
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Aussiegunneragain       10/16/2009 7:51:50 PM

Mirage1110 standard climb speed of 400knots (with afterburner deselected) gave an initial rate of climb of 25,000 feet per minute.

 Max rate of climb (afterburner engaged) at 450knots ( 0.95Mach) gave a rate of climb of 50,000 feet per minute.

 Sourced: page121, The RAAF Mirage Story. 1989. Susans, M.(WingCmdr). 



Thanks Drop, I thought 16,000 FPM was way to low. I must admit being a bit suprised that it could do 50,000 FPM with afterburner engaged though, plausible but I didn't think that it was up near Lightning territory.
 
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DropBear       10/16/2009 10:41:44 PM
...especially given the Mirage's big wing and consequent low wing loading.
 
I missed this first pass.
 
When discussing manoeuvering, the book commentary states that as the Miracle was a poor platform where agility was concerned, the aircraft would suffer from the elevon and pitch damper control surfaces would "dump lift" to achieve adequate nose-up authority. This in turn, reduced the wing area and consequently lead to an increase in wing loading.
 
Another interesting tidbit was that all Miracles accepted by RAAF were flight tested at no less than 50,000 feet and that the first two examples (home-built) were taken to 70,000 with the aid of partial-pressure flight suits.
 
Source: Same chapter, same book.
 
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Aussiegunneragain       10/16/2009 11:26:11 PM

...especially given the Mirage's big wing and consequent low wing loading.
 
I missed this first pass.
 
When discussing manoeuvering, the book commentary states that as the Miracle was a poor platform where agility was concerned, the aircraft would suffer from the elevon and pitch damper control surfaces would "dump lift" to achieve adequate nose-up authority. This in turn, reduced the wing area and consequently lead to an increase in wing loading.

Another interesting tidbit was that all Miracles accepted by RAAF were flight tested at no less than 50,000 feet and that the first two examples (home-built) were taken to 70,000 with the aid of partial-pressure flight suits.

Source: Same chapter, same book.

Yes, that is generally what you will get with tailless deltas because they use one control surface to do two jobs, which inevitably means that neither is done as well as would have been the case with a conventional design. The other disadvantage is the rapid loss of speed associated with that type of wing when the aircraft is turning. This is probably why the Israelis tended to use the Mirage in the vertical. However, in my question I was specifically referring to the impact that the large wing area should have and apparently did have on rate of climb.
 
On the manouverability of the type I would also note that everything is reletive to the overall performance of it's contemporaries. The Mirage's strengths were that it was reasonably easy to fly and that in the E model  had good range, so could make good use of its afterburners. The Mig-21 was manouverable at high altitude but lost manouverability at low altitude, had a lousy view out of the cockpit and a terribly short range so was vulnerable to being run out of fuel, and had to be very careful with useing its afterburners. The F-104 wasn't manouverable in any flight regime, had a mediocre range and was too easy to crash during hard manouvers. The Lightning was manouverable and kicked arse in terms of acceleration and rate of climb, but suffered the Mig-21's disadvantage with range. The F-4 was pretty good at everything except for its lack of a gun until the E model, but it cost twice as much as a Mirage. The F-8 was probably the best all round dogfighter of the time but not so good an interceptor because of its poor range and rate of climb. 
 
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sentinel28a       10/18/2009 5:08:39 AM
Chuck Horner said in his book that if you got jumped by a Lightning (he was flying F-100s at the time), your best bet was to just try to outlast him, because you damn sure weren't going to take him in the vertical (which you could with a Hunter) or by outmanuevering him (which was the case with the Javelin).  The Lightning really was an underrated fighter.
 
But since we're talking about the Mirage III--I was reading that the Swiss mounted Falcons on theirs.  Why? Didn't the Swiss have Magics?
 
And where's our French posters?  For once we have a thread on a French fighter that really was a world-beater for awhile.
 
 
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Privateer       10/18/2009 8:41:10 AM
The Swiss never used the Magic on their Mirage IIIS interceptor variant (they never bought the Magic at all), only the Sidewinders and Falcons (esp. the AIM-26B variant with a semi-active radar seeker). Two of these missiles could be carried on two additional pylons under the rear fuselage.
 
The Swiss selected a different radar system for their Mirage IIIS, the Hughes TARAN-18, and compatible Falcon missiles instead of the usual Thomson-CSF Cyrano IIbis radar and Matra R.530 missile offered with the Mirage IIIE. The different radar was also compatible with the FLORIDA air defense system, which was also developed by Hughes under a separate contract for the Swiss air force.
 
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DropBear       10/18/2009 8:56:06 AM
For once we have a thread on a French fighter that really was a world-beater for awhile.
 
And an absolute piece of $h1t at the same time! 
 
 
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sentinel28a       10/18/2009 8:24:23 PM
I dunno, DB...the Israelis kicked major ass with their Mirages.  I suppose you could make the argument that it was in spite of the Mirage's shortcomings, but I think it was a sound design that continues to do well.
 
 
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Aussiegunneragain       10/19/2009 3:30:35 AM

I dunno, DB...the Israelis kicked major ass with their Mirages.  I suppose you could make the argument that it was in spite of the Mirage's shortcomings, but I think it was a sound design that continues to do well.

 


Senty, DB has a raging anti-fetish with the Mirage 111 which is entirely based on the fact that it had a high peacetime crash rate due to engine failure in Australian service and because its radar wasn't that flash. The bit he always "forgets" is that most of the early supersonic fighters had distinctly average safety records and avionics. In fact two of his favourites, the F-100 and F-104, had lousy safety records. What's more neither the F-100 nor the early F-104's had a radar at all. I prefer to balance peacetime operability and paper stats against the wartime record of a type and on the later count the Mirage 111 was one of the best. It wasn't just the Israelis that did well with it, in 71' the Pakistani Mirage 111's wiped the floor with the Indian Mig-21's which in turn wiped the floor with the Pakistani F-104A's. IMHO its a nice demonstration of pecking order amongst those three fighters.
 
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usajoe1       10/19/2009 4:16:30 AM
 It wasn't just the Israelis that did well with it, in 71' the Pakistani Mirage 111's wiped the floor with the Indian Mig-21's which in turn wiped the floor with the Pakistani F-104A's. IMHO its a nice demonstration of pecking order amongst those three fighters.
 
I think the Mig 21 was the second best fighter of the 60's, after the F-4. The reason it's record in A2A combat is so poor is because almost every time it went to war its pilots were of much lower quality. The few times they had competent pilots they did very well.
 
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