Soviet aircraft the west coulda/shoulda used?

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Hello

A Mikulin 35A, are you shure?

But it was so big and heavy: weight 830 kg, instead of about 600 for the Klimov, the Merlin and DB-601 Engines…for 2840 inch²!!!

Mikulin AM-35 - Wikipedia, the free encyclopedia


Its specific power is 25.8 (29 for take off.) hp/ lit and power to weight ratio 1.445 (1.62 hp/kg)

For the Klimov 105PA those indicators are 31.5 hp/l and 1.8 (1.9) hp/kg

About 42.5 and 1.95 for the V-1710F-20R Allison.

Personally, I would rather follow TsAGI devices

Ôîðóì ñàéòà www.airforce.ru: Ñòàòüÿ



« В марте 1944 г. в ОКБ-155 был проработан вариант истребителя МиГ-3 с мотором Пратт-Уитни R-2800-63 и турбокомпрессором Дженерал Электрик С-23, которые устанавливались на американском истребителе Рипаблик Р-47D-10RE "Тандерболт". За основу проекта был принят истребитель МиГ-9Е (И-211). При расчетной мощности 2250 л.с. (с учетом скоростного наддува) самолет должен был иметь максимальную скорость 740 км/ч на высоте 10000 м и практический потолок 14500 м. Полетная масса должна была составить 3800 кг. 8 апреля 1944 г. материалы были представлены на рассмотрение в НКАП, однако дальше теоретических разработок "дело не пошло »


With google translator it's making something like this : "The design bureau 155 made (designed) a MiG-3 version with a PW R-2800-63 engine with supercharger GE C-23 that were taken from a Republic P-47 D-10 RE « Thunderbolt ».
The basic airframe was from the MiG-9 E (I-211) experimental fighter. At calculated power of 2250 hp (with dynamic blow) the plane should fly at 740 km/h at 10000m with a service ceiling of 14500m.
The TO weight should be 3800 kg. In april 1944 all documents were send to NKAP to validate the project, but this affair wait no further than theoretical studies".

From the La-5FN datasheet, I extrapolated (roughly) MiG-9E performance:

Мотор М-82ФН Райт Пратт-Уитни
R-2600 2800
Вес сухого мотора 850 900 1030
Мидель мотора 1,25 1,50 1,40
Мощность на 2-й
границе высотности 1450 1450 1500
Расчетная высота
(с учетом скорост.
наддува) 6100 4800 7800
..........................................

Мощность у земли
Макс. Скорость
на расч. Высоте 650 620 685

670 km/ at 6100m and 1450 hp with an M-82FN should give 640 km/ at 4800m (1450hp at rated altitude) with a Wright R-2600 and 705km/h at 7800 with a PW R-2800 (1500 at RA) engines.

Not so bad.

Altea
Well, I guess you could re-engine to the Wright R-2600.
 
I agree with you regarding sim data versus real data, MM

It's two different worlds that need to remain seperate!

I know that arguing the poor performance of a flight model requires involvement of actual data, but it doesn't work in the other direction. I know alot of younger folks tend to use sim performance in debates over actual machines events, perhaps because they haven't applied themselves to actual reference material (that does require reading, something that seems to be rare these days).

When I offer data and/or statistics in a debate, I go for actual legitimate reference sources and once in a while, I even learn something...I think we all do at one point or another. That's the beauty of a great forum like this, where everyone can bring the best of the best to the table. :thumbleft:

As far as working in the woods goes, that was many moons ago...I'm older now, and don't heal near as quick as I used to...you couldn't pay me enough money to "get up top" these days! :lol:
 
According to hartmann, he always went for the oil cooler. The Il-2 did fly rather straight as it wasn't very agile. Even more so, its best defense would be to fly in formation.

One really has to understand just how well these attack aircraft could defend themselves when flying in close formation. They were never the sitting ducks they are often thought to be. Rudel's memoirs are quite illustrative: he flew his Ju 87 until the last days of the war, and kept on instructing his squadron that if they stayed in close formation they were going to be allright. Looking at the loss figures for Ju 87, Hs 129 and Il-2 it becomes obvious that they had little to fear from interceptors. However ... that was on the Eastern front: Ju 87s suffered horrible losses over Italy. But then again, so did the Fw 190F.

I also have to respectfully disagree about the MK 108 being more of a grenade launcher with the shells lobbing towards the target. yes, its MV was lower than that of the MG 151 but it was comparable to the older MG FF which was used by the Fw 190A until late 1943 and beyond. We have to keep certain things in perspective: a gun fires rather straight at least for the first second. In case of the MK 108 that means a range of 500 m. At longer range it was definitely not accurate enough. But which fool fires at a target half a mile away?

Kris
 
I never really understood why the Mikulin engine of the MiG-3 was only good at higher altitude. I mean, I can understand the need for a high altitude interceptor but why couldn't the engine have been retuned for lower altitude again?


Kris
 
I never really understood why the Mikulin engine of the MiG-3 was only good at higher altitude. I mean, I can understand the need for a high altitude interceptor but why couldn't the engine have been retuned for lower altitude again?
I think the problems were more airframe than powerplant
The MiG-1 was a pig for spinning in, whilst the MiG-3 attempted to address the inherent limitations of the airframe, they were never fully worked out. At the low- and medium-altitude combats that characterised the Eastern Front, the MiG-3 lacked manoeuvrability and of course an engine being tasked at the wrong altitude.

So handling and manoeuvrability; the engine of course, didn't help.

It was fitted with a Shvetsov ASh-82 radial and was proposed for production as the MiG-9 (not to be confused with the jet MiG-9) but the Soviets weren't interested in disrupting manufacture of the La-5 for an aircraft that didn't offer any advantages over it.
 
If I may I would like to answer both of your last posts.

ALL shells are subject to gravity which means that they ALL fall about 16ft in the first second of flight. They all fall about another 48ft in the second second of flight. the question is how far have they flown in that 1 second (or 2 seconds). Shells forward velocity will fall off slower at higher altitude. Thinner air means less drag. Low velocity guns are harder to use for defection shooteing. Not only is the shell dropping but you have to lead the target aircraft more. A plane that is going 500kph is actually traveling at 138meters a second. While the firing planes speed is added to the muzzle velocity of the fired shell you can start to see some of the aiming problems. like were is the target plane actually going to be in 1 second:)

As far as the AM 35 was concerened. It was "retuned" for lower altitude. it was called an AM 38.

To change from a high altitude engine to a low altitude engine is more than changing timing or carburator jets. the gear ratio in the supercharger drive has to be changed.
 
I never really understood why the Mikulin engine of the MiG-3 was only good at higher altitude. I mean, I can understand the need for a high altitude interceptor but why couldn't the engine have been retuned for lower altitude again?




1) The MiG fighter was never designed as a high altitude fighter, but as a general air superiority fighter.
2) It was never intended to use a M-35A, but a 1400hp Mikuline 37 (basically an AM-35 with an intercooler).

Because the M 37 was unavailable, the Mikuline AM 35A engine was used, giving only 1120 hp (1350 for TO) at SL and 1200 at 6 km.

The low altitude version was called the Mikulin 38. Basically the same engine that a M 35, but with a much smaller supercharger. It was giving 1600 hp at 1000-1500m. Too low for a fighter.

Some MiG-3 airframes were fitted with AM-38 for experimental purposes.

http://www.airpages.ru/eng/ru/mig3_2.shtml

VG
 
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Robert S Johnson may disagree with you on that point

It's not about armour at least, not to the exclusion of all else. Turning an aircraft into a barge full of pig iron does not make it more survivable. How do you armour control surfaces and tail units? Rear gunners were horribly exposed. The oil cooler wasn't protected. All you do is slow the aircraft down and make life easier for a cannon-armed Luftwaffe bird and the Wehrmacht flak emplacements once they were over the target. The Il-2's real ace card was numbers.

Without a general balance between

survivability
hitting power
manoeuvrability
speed
ceiling
range

for single-engined combat aircraft they're either going to fail, or require air superiority in which to operate. The other aircraft of WWII that famously sacrificed all else for one attribute (in this case, manoeuvrability) was the A6M-series aircraft and once the Allies worked out its ace card it became easy prey for the late-war USN/USMC fighters.

Let's look at the P-47 wrt that list

survivability - yep, pretty sure I've got Robert S Johnson on board with that one
hitting power - well, it couldn't crack a tank open but 8 x .50s and underslung ordnance still made it a battlefield menace you couldn't ignore
manoeuvrability - once the payload is delivered, the P-47 is back in the fighter role, he's got a good chance of leaving the scene of the crime before the Luftwaffe show up but if they do, they've still got to contend with a very capable fighter, not a scrap dealer wallowing around like a sinking barge.
speed - covered that
ceiling - not that important for ground attack but the P-47 wasn't shy in the high-altitude performance stakes
range - about 920Kms for the P-47 vs 600Kms for the Il-2 on internal fuel

Now take me through the list with the Il-2



Robert S Johnson may disagree with you on that point

I don't know if S Johnson will disagree or not. But he certainly never flew assault missions with an Il-2 and probably never saw on what they are look like. And what if his point of view (with some limited interest) is contradicted by thousands af stormovik pilots and their fighter pilots guardians. I said what if, but actually it is already maid;

:: Àðòåì Äðàáêèí :: ß äðàëñÿ íà Èë-2 :: ñêà÷àòü êíèãó â rtf, fb2, iSilo, Rocket eBook :: Áèáëèîòåêà OCR Àëüäåáàðàí

Unfortunately it's not soon translated in English. "Only vet's interviews: I fought on a Il-2" With no political -background.


- Turning an aircraft into a barge full of pig iron does not make it more survivable.
A barge? If there was a barge in the story it's not probably the one you're thinking about. Have you got some valuable numbers to support that was the P-47 a more nimble plane or a better turner?

A 1941 year Stormovik had a wing loading of only 138,5 kg/m² (122 clean condition), and a specific power of 3.17 kg/hp. 159 and 3.5 in 1944, 284 and 3.13 for the P-47D respectively.
So wich one is the barge, and why?



-The oil cooler wasn't protected
Where have you taken that from?

-All you do is slow the aircraft down and make life easier for a cannon-armed Luftwaffe bird and the Wehrmacht flak emplacements once they were over the target.

Do you know how many armour-percing bullet proportion there were in flak ammnution stocks? In a Luftwaffe fighter?

Now take me through the list with the Il-2

survivability - yep, pretty sure I've got Robert S Johnson on board with that one
J've got my mother in law on Il-2 side. And so what? There is a lot of aeras where the P-47D is able to be definitly lost by a single but happy mauser rifle shot from a german infanteryman. Not a single place like that on the Il-2, except maybe for the oil radiator exhaust slot; but it's less than 3-4 inch, at rear 10° max trajectory angle. No one chance on 10 million to hit it from the groud.

hitting power - well, it couldn't crack a tank open but 8 x .50s and underslung ordnance still made it a battlefield menace you couldn't ignore
0.5 caliber is much to big for the infantery and soft-skins, to light for armored cars. Better than nothing, but unadapted for ground support mission.


manoeuvrability - once the payload is delivered, the P-47 is back in the fighter role, he's got a good chance of leaving the scene of the crime before the Luftwaffe show up but if they do, they've still got to contend with a very capable fighter, not a scrap dealer wallowing around like a sinking barge.
A very capable figher? Maybe at height and only in boom zoon tactics. A low height the P-47 TOT is worse than the stormovik one.

speed - covered that
100 ok! But 190F-8 was much faster at SL. And anyway, it was making attacks only at 400 km/h to provide some accuracy.

ceiling -
I don't give a damn for what we need.

range - about 920Kms for the P-47 vs 600Kms for the Il-2 on internal fuel
About 95% of VVS stormovik missions were made at the front line or at best 15-25 km iside german lines. And from 30-50 km distant airfieds.
In the navy it was different, stormoviks suffered because of their short range. But thy was never designed for maritime purpose


VG
 
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0.5 caliber is much to big for the infantery and soft-skins, to light for armored cars. Better than nothing, but unadapted for ground support mission.

This comment kinda jumped out. If a .50 cal is much too big for this (which honestly I do not understand as the objective is to kill they enemy), then would not the 20mm from the Il-2 also be way too big??

If a P-47 can shoot holes through a boiler of a locamotive which is at least half an inch thick, why do you feel it would be ineffective against amoured cars?
 
I think everyone posting on this site, VG33, understands that the IL-2 is a hero of the Great Patriot War. We know more were built (by a very slim margin) than other types. That said, it still remains true that the IL-2 was appropriate for the EASTERN FRONT - unique to the conditions and the Soviet doctrine. I am happy that your Mother in Law agrees with you, :) VG, but unless she was a combat pilot, I think the comment is a wee bit over the top. As is "Not a single place like that on the Il-2, except maybe for the oil radiator exhaust slot; but it's less than 3-4 inch, at rear 10° max trajectory angle. No one chance on 10 million to hit it from the groud...".

I understand that that once perfected, the Il-2 had a great pilot survivability rate - well - so did the P-47 :) Johnson is certainly living proof of that.

To me VG - the key distinction between the two was that the P-47 was air conditioned and the Il-2 wasn't. :) :)

Think about it.

MM
 
In any case, VG, the glorious legacy continues.
 

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Have you got some valuable numbers to support that was the P-47 a more nimble plane or a better turner?

The P-47 had a higher wing loading and slightly higher power mass. On paper the the IL-2 would have a better sustained turn rate, however the P-47 had a better roll rate which enabled it to enter into and out of a turn quicker.

Not a single place like that on the Il-2, except maybe for the oil radiator exhaust slot; but it's less than 3-4 inch, at rear 10° max trajectory angle. No one chance on 10 million to hit it from the groud.
Every aircraft has a vulnerable spot and although the IL-2 was probably the most heavily armored aircraft of WW2 many were brought down by fighters and flak by a round or shrapnel making its way to an oil cooler or radiator line.
 
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This comment kinda jumped out. If a .50 cal is much too big for this (which honestly I do not understand as the objective is to kill they enemy), then would not the 20mm from the Il-2 also be way too big??
They would. It' better to use Il-2 ShKAS 0.3 cal for this purpose. And 23 or 37mm guns for tanks.



If a P-47 can shoot holes through a boiler of a locamotive which is at least half an inch thick, why do you feel it would be ineffective against amoured cars?
A locamotive is made of common steel, a Panzer from armour. To make a hole in the armour you need at least an anti armor bullet.

What is the Brinell or Rockwell hardiness value od your thug steel, the 0.5 bullet stell, the panzer armor?

Regards

VG
 
What is the Brinell or Rockwell hardiness value od your thug steel, the 0.5 bullet stell, the panzer armor?

Rockwell or Brinell testing has no bearing in this situation because there is an element of force, density and trajectory. You factor in the weight of the round and the muzzle velocity plus the harness value of the round. Hardness testers are static and designed to take a surface hardness in a non-dynamic environment.
 
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I just read an AP round that was used in WW2 could go through 22.2mm of face hardened steel @ 91m, and 19mm @ 500m.


I'm still somewhat confused as to how 2 x 7.62mm are better anti personnel/lite vehicle then 8 x .50's.

From D-Day to VE Day, they destroyed something like 86,000 railway cars, 9,000 locomotives, 6,000 AFV, and 68,000 trucks. Apparently the combination was a good one.
 
I just read an AP round that was used in WW2 could go through 22.2mm of face hardened steel @ 91m, and 19mm @ 500m.


I'm still somewhat confused as to how 2 x 7.62mm are better anti personnel/lite vehicle then 8 x .50's.

From D-Day to VE Day, they destroyed something like 86,000 railway cars, 9,000 locomotives, 6,000 AFV, and 68,000 trucks. Apparently the combination was a good one.
Not to mention over 4,000 aerial victories in the ETO between 1943 and 1945 (including a V-1 buzzbomb).
 
The P-47 had a higher wing loading and slightly higher power mass. On paper the the IL-2 would have a better sustained turn rate, however the P-47 had a better roll rate which enabled it to enter into and out of a turn quicker.
I agree for the turn rate, but have no data for the roll rate, and roll acceleration. Roll rate/acceleration depends a lot of inertia moments, that means distance x weight influence. So if the Il-2 wing is lighter, despite of its biger size, the plane could have a better roll too, despite some prejudices.


many were brought down by fighters and flak by a round or shrapnel making its way to an oil cooler or radiator line.
Not by a 7.92 cartridge. In the P-47 you can hit the pilot, the oil circuitry, the fuel circuitry, or the ignition circuitry leading to the complete plane loss, by a simple Mauser rifle.

Regards
 
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Not by a 7.92 cartridge. In the P-47 you can hit the pilot, the oil circuitry, the fuel circuitry, or the ignition circuitry leading to the complete plane loss, by a simple Mauser rifle.

Regards
Ok, so...cannon rounds taking out half the engine, flak tearing wingtips off, 30mm cannon takes off rear elevator, 7.92 rounds shatter instruments, 20mm holes to wings, fuselage, canopy and stabilizer just to name a very few instances of severe damage where they flew back across the channel and you're saying that a single rifle shot can do what all the above mentioned couldn't?

Seriously...
 

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