Ad: This forum contains affiliate links to products on Amazon and eBay. More information in Terms and rules
I'm a little disappointed that I seem to keep having to post the same stuff over and over.
Here are the (P-40 only) victory claim totals by Fighter Group:
33rd FG - 137 victories (active with P-40s Nov 42 - Feb 44)
57th FG - 144 victories (active with P-40s Aug 42 - Jan 44
325th FG - 133 victories (active with P-40s March 43 - Oct 43)
324th FG - 66 victories (active with P-40s March 43 - July 44)
79th FG - 118 victories (active with P-40s Dec 42 - March 44)
Well, most of the P-40 variants generally had a lower wing loading than most of the Yak variants. Big wing with a large wing area.
Aside from wing loading, power also makes a difference - the P-40M may have had a better (quicker by time) turning circle in their test because they flew it at a higher power setting.
Most of the M-105 powered Yaks (except the Yak 3 with a more souped up 105PF) seem to have similar power to mass ratios as P-40s, so long as the latter were flying at moderately high power settings, i.e. 57" Hg or 60" Hg etc. which they were capable of at all the altitudes combat normally took place on the Russian Front (up to about 10,000 ft). The VK-107 powered Yaks were considerably zippier of course.
Those are Claims not confirmed!
Who actually are shot down are in Luftwaffe records.
After a day of Combat you always know who did not return.
Those are Claims not confirmed!
Who actually are shot down are in Luftwaffe records.
After a day of Combat you always know who did not return.
What is missing from that data posted is the losses that occurred.
Hello Schweik,
If these tests really were flown at 1,000 feet as you commented earlier, then the P-40E/K would have the greater engine power available. It sounds like altitude was a bit higher where the P-40M had a slight advantage in power that was enough to offset its higher induced drag.
The only problem with this theory is that the P-40E/K were not capable of 57 or 60 inches Hg by 10,000 feet. In climbing flight (un-rammed) they were down to around 42 inches by 11,500 feet. I believe Shortround6 already commented on this
Here is another article about the P-40 in Soviet Service that has a lot more specifics.
It also paints a much less pretty picture of the Soviets' opinions of the P-40 series.
The P-40 in Soviet Aviation
- Ivan.
I have the rather uncomfortable feeling that we are kind of going in circles as several points raised on this page have already been dealt with I think two or three times. But I do have some of this data and I'll post it again for the benefit of those who missed it before. If you skipped it last time please read this.
.....
There are also some interesting comparisons by type:
Sortie to victory ratio for the P-40 was 30.2/1
Sortie to loss ratio for the P-40 was 93.3/1
Sortie to victory ratio for the P-47 was 26.47/1
Sortie to loss ratio for the P-47 was 98.1/1
Sortie to victory ratio for the P-51 was 40.4/1
Sortie to loss ratio for the P-51 was 107.2/1
It's worth noting here that while the P-51 has the best sortie to victory ratio, the P-40 has lowest loss rate of the three fighters they used. This proves nothing definitively but is common across nearly every Theater of operations where P-40s were active from Russia to the Solomons to Burma. It's also notable (though again proves nothing) that they had a better victory to sortie rate with the P-40 than the P-47.
There are some differences in USAAF losses depending on sources. The USAAF Statistical Digest gives for the period June, July and August 1943 391fighters lost on combat missions. MAW IV in the same period has about 260, including damaged aircraft that returned.
Hello Schweik,
Thanks for reposting. I had not seen this the first time but I also didn't read all 30-something pages of posts that were here before I joined in.
Are you sure you are interpreting the statistics correctly?
26 Sorties per Victory is better than 40 Sorties per Victory
and
93 Sorties per Loss is not as good as 107 Sorties per Loss.
I believe Shortround6 mentioned this before, but a lot of this might have to do with different mission profiles.
How long in duration is each sortie and what is the likelihood of running into aerial opposition?
- Ivan.
Well in the above posts the loss data is from the 325th squadron history, not MAW IV. The only losses I'm quoting from there are the Axis losses.
You also posted data ffrom MAW IV in the above posts and I am pointing out that another source has some 33% more USAAF fighter losses than MAW IV. Whether that has any bearing on the USAAF flown P-40's combat record I don't know; but it is curious that there is such a differnce in losses between the sources.
I have a hard time believing that brand new American crews in combat for the first time were somehow more effective with the same equipment than their DAF counterparts. Some of whom had been in combat almost continuously for 2 years at that pointPart of why the American units did better in terms of the ratio of victories vs losses though, is that they worked more as a team.
I have a hard time believing that brand new American crews in combat for the first time were somehow more effective with the same equipment than their DAF counterparts. Some of whom had been in combat almost continuously for 2 years at that point
Being able to withstand G loads was another of those rare skills (like marksmanship in general, or deflection shooting specifically, or a knack for riding a stall) that some pilots used to their advantage. Greg Boyington and the Australian Ace Nicky Barr both had developed personal techniques of 'bearing down' to withstand G load. Boyington was a wrestler and Barr was a rugby player, which apparently contributed to their having the right kind of (thick, muscular) necks for that business.
I think in later periods they started teaching this but I don't know when.
Some trivia.
Ivan Kozhedub was amateur weight lifter. At the age of 13 he could lift 2 poods (2x16.4kg) kettlebell with one hand. Later, as a flight cadet and a pilot he repeated this exercise many times - but keeping the kettlebell with his pinky.
Since just about every aircraft known to man gained weight somewhere along the design/development process the actual G loading went down. The Mustang was good for 8"G"s in service (12 Gs ultimate) at 8000lbs, since flying a Mustang at 8,000lbs meant you were seconds away from running out of fuel or oil you had to make allowances. 8 times 8,000 is 64,000. If the Mustang is grossing 9000lbs you divide 64,000 by 9,000 and get 7.111 There is actually a chart in the manual that explains this.
It's for all US warplanes, the Mustang just gained more weight than most, largely because it ended up carrying so much fuel.
Fully loaded with fuel Mustangs didn't fly that well either...