Time Machine Consultant : Maximizing the Bf-109 in January 1943

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Good call. I actually forgot all about that conversation. It just goes to prove the point how out of touch with reality that Goering (Or should we call him Herr Meier? ) and other High Command officials really were.

Either way good stuff everyone. This has finally turned into a good thread with good information. See how easy and better it is when people get rid of the chips on their shoulders...
 
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I have zero clue what German intel had on the RAF experiments with a Merlin Powered Mustang in 1942, nor do I know what they believed about the B-29 but if they knew about both and expected them in 1944 they really screwed up - which is hard to believe - regarding threat analysis and meeting them with priority developments.
 

This is not quite true - people tend to think of two-staged superchargers as some kind of magic wand, but in reality, the power outputs of the high altitude DB 605AS and D engines with the enlarged supercharger was identical to that of the two-staged Merlin 6x series and the licensed Packard 1650-3/7 that drove the Spitfire VIII/IX and the Mustang B/C/D. This is easily confirmable from an overlay of power curves for the respective engines.

Also the rated altitude of the earlier DB 605A and the BMW 801 were similiar, around 19 000 feet. The plus IMHO for the Bf 109 was that it was considerably lighter than the BMW 801 powered FW 190s, with the added advantage of a less draggy installation of an inline vs a radial and thus was effected much less by the gradual loss of power above the rated altitude. Similiarly, the gains from the adoption of the inline Jumo 213A for the FW 190D were related to the same factor of decreased drag - the Jumo powerplant neither offered more power or higher rated altitude compared to the radial BMW 801.

It also worth of noting that the later, two staged Merlin 66 / V1650-7 were geared for lower altitudes compared to the earlier ones, reflecting operational requirements, to around 16000 feet.
 
1. The flak 38 is not an aircraft gun. It is way to heavy and has a poor rate of fire. It's range and accuracy aren't needed in realistic scenarios. It is a very poor choice for a fighter armament.

2. The MK 108 barrel they chose was the longest they could without the risk of blowing up the gun. If you increase the barrel length the chamber pressure rises.

3. Yes the MK 108 is the holy cow.

4. Jumo 213 Jumo 222 were also in development. Of course the latter turned out to be a failure but I guess you with your infinite knowledge can predict that in 1937 eh?

"And DB 601/605 remained with same power from mid 1942 to mid 1944 (and still under the main rival, Merlin 60 series). I guess RLM failed to force DB to do that, don't you agree?" Wtf is this even supposed to mean. What do the development problems of the 601/605 have to do with anything I said?
 
Didn't wanted to bee to harsh, sorry

1.Since we're mounting it to aircraft, it becomes aircraft gun. For it's power (134g @ 900m/s) it's not over weighted, and it's surely lighter then MK 103. My guess is that higher accuracy power is always a good thing. Since we're about to upgrade (perhaps only up-neck) to 25mm (as I've said, 200-250g @ 700m/s) it would be a killer gun as a motor cannon, or two for FW-190 outer wing mounting.

2. Since MK 108 had about 1/3 of propellant of 103 had, my guess is that chamber pressure was pretty low. So they could mount a longer barrel if we took only pressures in account.

3. Again: nice.

4. DB-603 was reality in 1942. Jumo 213 was reality in 1944, with same power. What would you choose in 1942?

My tirade shows that RLM was not properly pushing DB to increase power of 601/603 line from 1942-44 as you stated: ...or you are wrong about that part in bold.
 

Again, "This is not quite true" The Allied liquied cooled engines,being smaller needed higher boost to develop comparable power. This ment that they needed higher pressure ratios from their superchargers to make rated power than the German engines but it does not mean that the Germans could use single stage superchargers at any hight they wished to. I know you didn't say they could but let us look at the examples you gave. For the DB 605AS to maintain 1.42 ata to 26,000ft it's supercharger needs just about a 4:1 pressure ratio which is actually quite good for a single stage supercharger. THe Merlin -3 engine because it is operating at 2.04 ata at military power (NOT WER) needs a supercharger than can supply a pressure ratio of 5.74:1 at about the same altitude.

Now to go any higher the Germans are either going to have to get more than 4:1 out of a single stage or add a second stage. Since a second stage doesn't add but mulitplies the British could have been using (in therory) a pair of 2.4:1 compressors. giving them a lot more potential for higher pressure ratios.
Practical factors that come into play are the higher the boost the hotter the air entering the engine and the more danger from detonation. However using two stages to get the same pressure ratio overall means less actual power used in the compressors and less actual heating of the air for the same pressure ratio. this is without using an inter/aftercooler. However it does help explain why inter/after coolers are almost manditory on two stage engines.

Pleae do not confuse the Military Power rating height for the WER height. THe former is limited more by the pressure ratio of the supercharger while the latter is limited by the volume flow of the supercharger.

 
It's still way too heavy and the ROF is very poor. Anything below 600 rpm you can pretty much forget about unless you pack a whole lot of them into your plane and the flak 38 only has 450 rpm. Heck you might as well take the MK 103 then (440 rpm), at least its more powerful.

2. Since MK 108 had about 1/3 of propellant of 103 had, my guess is that chamber pressure was pretty low. So they could mount a longer barrel if we took only pressures in account.
I'm pretty sure if they could they would've done so.

4. DB-603 was reality in 1942. Jumo 213 was reality in 1944, with same power. What would you choose in 1942?
Jumo 213 powered Fw 190s flew in 1942. The DB 603 still had serious teething problems even as late as late 1943. So it surely wasn't as perfected as you make it.

My tirade shows that RLM was not properly pushing DB to increase power of 601/603 line from 1942-44 as you stated
Sorry but I don't see the logic in that. As soon as someone puts you under pressure you magically solve all problems in no time? That doesn't make any sense. And I also said develop, which not only means increase in power. The most important thing at the time was manufacture though, which I clearly stated.
 
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Drog; I'm sure I wasn't clear on this: I meant to say that the requirement was to get to 40,000 ft RAPIDO ! The requirement was for a high altitude interceptor. The required performance - I don't know how many ft/min or how many min to 40,000 ft were stipulated - was high enough to believe that only a twin engined interceptor à la Lightning would have been able to do so. Of course several aircraft could reach 40,000 ft.

Qnd yeah, I'm also getting a bit confused as to what we're talking about. For some subject such as the Fw 187 we are talking about the late 30s, but for other subjects like a possible Bf 109 replacement we are in 1943. And early 1943 to be exact.
I agree that the Luftwaffe felt it was still on top of it by early 1943. This only changed dramatically after the Summer.


Kris
 

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It's rather interesting question.
The gun and especially its ammo was designed for destroying land target (armoured cars, tanks etc), it was rather lightweighted in comparison with Mk.101, its predessor.
As far as I know Germans tried to increase its rate of fire but failed.
And for such a little bird as Bf.109 it seems too bulky and I suppose reduced markably craft's flight characteristics.

But the interesting question - why Germans could't design anythig like that: Type 5 cannon - Wikipedia, the free encyclopedia
An introduction to collecting 30 mm cannon ammunition
According to 'Japanese Aircraft Equipment 1940-45 - Schiffer' its weight was 66 kg - less than half of the Mk.103 weight.
If Japanese managed...

Gun Type 5 on its characteristics seems about the ideal motor-cannon (against aircrafts) with its weight and power - initial velocity is close to the Mg.151/20.
And its ROF is 25% higher than of Mk.103. And it was easy to unificate production of ammo as cartridge for Type 5 looks like shortened cartridge for Mk.103. I know that there are some differences in dimensions, but rather small.
 
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just to add to the conversation : If you wanted to get to 40000ft fast why not develop a detachable take off rocket assisted launch ? That way you gain the altitude faster and use less fuel in the process .
 
Mauser MG 213 - Wikipedia, the free encyclopedia
They did. However the Mauser MG213 revolver cannon didn't make it into production before the war ended.

30-mm MK.213C is a low velocity gun exactly as Mk.108. it's not multiporpose moreover I suppose it was not efficient against fighters (especially in dogfighting) because of low velocity.
It's good just against heavy unmaneuverable bombers/
But if you have just the only one cannon - as Bf.109K has the only motor-cannon - usefulness a low-velocity 30-mm cannon became doubtful. Especially if you pay attention at quantity of ammo for such a cannon in the box on the board.

Besides - a cannon of ballistic similar or close to ballistic of rest of armamment (MG.131) is most desirable, dispersion of shots is no more than mediocre. in the case of combination a low velocity gun + medium velocity machinguns dispersion should be quite vast and combo fire is efficient only at short distance. It is a rule for WWII fighter pilots to fire from close distances if one desired to shoot opponent with guarantee, but situations could be different.
 
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MG213C has a mv of 1050 m/s though. Conversion was rather easy so you could use the one or the other based on what was necessary.
 
just to add to the conversation : If you wanted to get to 40000ft fast why not develop a detachable take off rocket assisted launch ? That way you gain the altitude faster and use less fuel in the process .

Germans, among others, were experiminting with rocket assited take-off in WW II.

It worked for take-off of heaviely loaded aircraft but might be less successful for climb performance. The solid fuel rockets didn't have much burn time and liquied fueled rockets start getting expensive to use as throw aways.
An how many hundred pounds of rocket fuel do you use to save how much gasoline?
 
Please note that it took the French about 6 years to get the the revolver cannon into production starting where the Germans left off. I don't believe the British were much quicker and according to some accounts the American version (M 39) did see combat in 1953.
I don't know if this is becasue of the Korean War slowing things down or if the Korean War actually might have moved up priority.
I am not sure I can believe that 'Not invented here' modifications would have slowed down production of a "ready to go" gun by 4-5 years assming all three countries waited until 1948 to actually do anything with the design.
 
The Germans had a rotary machinegun in WW1. If you go to the WW1 section, you can see a photo of it.
 

The T-160 was a modified M-39 and was used as past of Gunval program in Korea in 1953. IIRC the a/c were modified on a special contract with NAA and tested at Eglin when I was a kid there in 1952.

It was direct result of early returning F-86 fighter pilots complaining about high altitude deficiencies of 50 cal API hitting MiGs but not causing fires at 35K and above.
 
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MG213C has a mv of 1050 m/s though. Conversion was rather easy so you could use the one or the other based on what was necessary.
That's for the 2 cm version. The 3 cm version had half the muzzle velocity.

The Germans couldn't make the MG 213 to work despite working on it for years and throwing a lot of money/resources at it. It is still very unclear that they would have fixed the problems by 1946.
However, that it took the allies several years to come up with their version doesn't mean that much. That happened to a lot of German innovatations.


Kris
 

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