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Again, thank you for a thoughtful comment. But you are reading things that I didn't want to write, perhaps because of my unclear writing and bad grammar.And regardless - this would not have been a game changer. There were plenty of other alloys that were used successfully in aircraft that dominated the Zero so it goes back to the fact that the Zero, although a great performer at the start of the Pacific War was not some leading edge design. It was quickly surpassed in performance and became quickly obsolete.
Errr, no, not even from a flimsy gun. 7075 offered advantages but wasn't the only reason why "most Japanese aircraft had better power to weight ratios than their contemporaries." The design of structure and weight saving design methods (stamped parts, milling some structural components, lightening holes in structure, minimal structural members to achieve maximum G loading, etc.) were part of the equation that helped achieve light weight but effected strength and durability. I can tell you at the end of the day 7075 was not much lighter than 6061 and depending on the application, 6061 was the better material. Bottom line you weren't saving that much weight by using 7075!
So your comment "the Allies didn't have the alloys or construction techniques necessary to build ultra light aircraft" is simply not true. The fact that 7075 was not available to the allies is irrelevant. There were plenty of allied designers who "could have" easily gone into a lightweight design concept but were not directed that way due to the mandate from their customers.
Lastly, the Zero, like many other Japanese combat aircraft of the period had terrible interchangeability characteristics. I think this included the Tojo and Jack.
Here a comparison of 7075 to 6061 that goes into laymen's explanations
6061 Aluminum vs. 7075 Aluminum – Differences in Properties, Strength and Uses
This article presents a brief comparison of the properties, strength, and applications between 6061 and 7075 aluminum.www.thomasnet.com
Ah, thank you for the link that was amazing.We can compare the Spitfire I with A6M2. Fully loaded, the former weighted 300 kg more, a good deal of it being that Merlin III was heavier than the Sakae 12 by 110-120 kg, and because of the presence of the liquid cooling system (another 150-200 kg?). Stick the Sakae on the Spitfire I istead of the Merlin it's ancilliaries and now it weights ~2350 kg instead of 2640 kg (5820 lbs) - between the A6M2a (2338 kg) and A6M2b (2421 kg).
(figures for the Zeros are without the drop tank, source is the Shinpachi's translation)
SAI 403 was good for 575 km/h - see here.
And yet, the Pacific Ocean Area is where the Hellcat gained the majority of it's kills. After the Guadalcanal campaign wrapped up, there was not a lot of carrier action intil the arrival of Essex. After a few minor raids, they went out and smothered Wake Island. The Japanese put up 22 fighters to oppose three carrier air groups. I call that overwhelming superiority.
Again, what are they??? (outside the 7075 discussion) If you look at the bigger picture, they really didn't, they just did some things a little differently to achieve their mission goals.Again, thank you for a thoughtful comment. But you are reading things that I didn't want to write, perhaps because of my unclear writing and bad grammar.
Here's my point: The Zero had advanced technologies in it that the Allies didn't have.
Again there's nothing specific there. Yes, the discovery and use of 7075 was an achievement but at the end of the day it really wasn't that great of an advancementI mentioned 7075 because it was just one example of an advanced technology. I didn't mention magnesium because it was a much poorer airframe option compared to aluminum. And IIRC it required using arc welding to build into airframes and it was more expensive. I'm not sure why you bring it up as it was never adapted to mass manufacturing AFAIK for WW2 aviation... and I can only think of one prototype that used it. But I do see your point that there were other lightweight materials that the Allies could have used in a prototype. My point, though, was that their aviation industry was not suited to build ultralight fighters. Althoughtomo pauk did pretty much cripple my argument by mentioning the Spitfire MK I which was only slightly heavier, had more horsepower, etc... although it was at the expensive of firepower, range, etc..
OK And my point about interchangeability involved finished component parts - a very basic part of aircraft manufacturing that the Japanese seemed not to get right.I did not mean to imply anything about component interchangeability, about 7075 being universally better than other aluminum alloys, or magnesium being a substitute for 7075 and I apologize for having made so many distracting side comments.
And that's the real point - the Allies more than had the means and capability of doing so, the doctrine of aircraft design directed by those at places like Wright Patterson said otherwiseTo recap, as with all mass produced components that go into an aircraft, 7075 was (just as you say) one of many techniques that the Japanese used to make their aircraft lighter. As I mentioned earlier, the Allies couldn't have built a lighter aircraft because they did not invest resources in it the way the Japanese did. I'm sure if the US wanted to, it could have built anything it wanted to.
And even that statement is a stretch. 7075 is not great to machine so you would have to look at two similar components that can both be machined the same way. Because of stiffness/brittleness of 7075, certain components wouldn't be able to be manufactured in certain applicationsRegarding 7075, according to Horikoshi, IIRC, it was primarily used in wing spars because of its tensile strength and light weight. So it wasn't used in the parts of the aircraft that needed ductility. But it was one of many reasons why Japanese aircraft weighed a lot less than Allied ones. (I was under the mistaken impression that wing spars need quite a bit of ductility in order to avoid breaking off and just going off my basic understanding of flight engineering, am not sure why 7075 received so much credit for being "30% lighter than alternatives" now that I think about it.
Many Thanks!Anyway, one last thing: i just want you to know that I respect your expertise and writing skill on this forum and my comment comes from a place of respect and admiration. Please don't take offense at anything that I've written as that is not my intent.
And again, many thanks!!!Ah, thank you for the link that was amazing.
Agree!Regarding comparisons in weight, I don't think fully loaded is the best comparison as the A6M2 carried large amounts of fuel, whereas the Spitfire carried very little even compared to some of its European theater opponents. But even so, it's pretty obvious that the Spitfire was a very lightweight aircraft, as was the BF-109E. So clearly the Japanese construction technology used to achieve light weight wasn't a magic bullet. It just led to slightly lighter power loadings.
(One of those comments was meant for Tomo btw, sorry for the confusion)Again, what are they??? (outside the 7075 discussion) If you look at the bigger picture, they really didn't, they just did some things a little differently to achieve their mission goals.
Again there's nothing specific there. Yes, the discovery and use of 7075 was an achievement but at the end of the day it really wasn't that great of an advancement
OK And my point about interchangeability involved finished component parts - a very basic part of aircraft manufacturing that the Japanese seemed not to get right.
And that's the real point - the Allies more than had the means and capability of doing so, the doctrine of aircraft design directed by those at places like Wright Patterson said otherwise
And even that statement is a stretch. 7075 is not great to machine so you would have to look at two similar components that can both be machined the same way. Because of stiffness/brittleness of 7075, certain components wouldn't be able to be manufactured in certain applications
Many Thanks!
And again, many thanks!!!
Agree!
Again, a great development but not earth shattering.(One of those comments was meant for Tomo btw, sorry for the confusion)
We might have to agree to disagree about the significance of 7075 but a hint as to its significance is that it took the US four years to adapt it to production and that they chose to invest four years of effort in adapting it for mass production.
I'm well aware of 7075 being used today. I have fabricated parts from it, driven rivets into it, and inspected hundreds of machined parts made from it, it's only one component in the bigger piece of the pie. 7075 was an advancement but I can tell from experience there's nothing magical about it, then or now.7075 is still used today, just as you might expect for any advancement in metallurgy. So, to recap, I don't mean "ancient aliens" or something when I say "advanced technology", we're talking about breakthroughs. And while you might trivialize 7075, I prefer to give credit where credit is due.
The same methods were being used in the United States and Europe during the same time period, the article doesn't mention that. Drillmatic and automatic riveting machines were being designed and introduced in the US during the late 1930 and into the 1940s (I believe the same in the UK and Canada). What was grossly being dismissed was the Japanese ability to manufacture aircraft almost in the same capacity as western manufactures, that was a surprise to some who were very closed minded about Japanese ability during period.My understanding (from reading Horikoshi and Sumitomo's report as well as other post-war analyses) is that a combination of labor-intensive construction methods, such as building the wing "integral" with the fuselage, bracket placement, "drilling" out holes (which later Allied aircraft used extensively), early use of flush riveting, and other techniques (see the article for details) led to the Zero being ahead of its time in its deployment of new weight-saving technologies.
Not really. Read my previous post. What he accomplished was good, very good, but it wasn't earth shattering. There were many manufactures that were on par and even ahead of his design team and manufacturing methods. If the methodologies were so great, production should have been on par or exceeding what allied factories were putting out, and I'm talking early in the war.That didn't mean the Allies never developed them. It just meant that Horikoshi's team were among the first to adopt them.
They probably were.Getting back to the original discussion, the Tojo vs. Jack, I wish we knew more about whether the technologies used in the Zero were used in the Tojo or Jack. Because Horikoshi was somewhat involved with the Jack, it may be why it used so many "cutting" edge weight saving technologies and why the Tojo was a more conventional aircraft.
They do, lol! But look into how the zero was constructed and compare it to its contemporaries. There's no raving advancements there, just a good formula that gave the Japanese a few years of aerial supremacy.EDIT: You dropped in the same link that I linked to in my comment, while i was responding. Great minds think alike?
You raise a good point, the A6M was designed for the low power of the available engines, that caused the design to have limited growth, it was also designed for outstanding agility, trouble is that agility came at a cost of high speed maneuverability, every flight report you read about the A6M will quote exceptional low speed turn performance but heavy controls at 250mph and solid over 300, the opposite to western aircraft.Let's not forget that the "lightness" of early Japanese aircraft was something of a necessity given the relative low horsepower engines available to them at the time. The original version (A6M1) had a 780 hp engine. Even the A6M2 with the Sakae still had a sub 1000 hp engine. The original specs stated that manuverability will equal the A5M and to achieve that with the engine used the aircraft had to be made as light as possible.
Armor protection, SS tanks, navigation/communication equipment, bigger guns, more guns, more ammunition even the life raft added weight, Japanese fighters had better power to weight but it had nothing to do with the alloy they were made from.My understanding is that 7075 was mass manufactured in such quantities that it was in all Japanese aircraft, which would explain why most Japanese aircraft had better power to weight ratios than their contemporaries.
lightening holes in structure,
ExactlyView attachment 691182
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There's no better example of the different philosophy's between the Western and Japanese forces. How many of you would pick the Zero seat when .30 .50BMG 20mm SAPI rounds start coming through the rear fuselage?.
The British don't get the credit they should, their torpedoes worked, both airborne and submarine. (problem with magnetic exploders) and the British figured out how to drop them in shallow water about 13 months before Pearl Harbor.One place the Japanese had a lead was aerial torpedoes. Of course, almost the entire world had better torpedoes than we did when WWII started.
The Japanese were able to design an aerial unit that could be dropped into Pearl Harbor without hitting the bottom of the harbor. At the time, U.S. torpedoes were not very good and were never able to be dropped in quite as shallow water.
Didn't the Japanese study the Taranto raid as proof of concept before deciding the Pearl Harbor attack was feasible?.The British don't get the credit they should, their torpedoes worked, both airborne and submarine. (problem with magnetic exploders) and the British figured out how to drop them in shallow water about 13 months before Pearl Harbor.
The British don't get the credit they should, their torpedoes worked, both airborne and submarine. (problem with magnetic exploders) and the British figured out how to drop them in shallow water about 13 months before Pearl Harbor.
In this case 3 out of 3 IIRC, at least one of them was still around in April 1943 and participated I-GO operation against Guadalcanal.3 pilots rescued out of how many?, have you looked into what happened to the survivors of the Kutai Butai after they returned to Japan?.
I agree that pilots are hard to replace, and that the Japanese lost a lot of aircrew in 1942. That being said it wasn't the Zero pilots taking the heavy losses, it was the bomber crews. I would agree that the bombers should have been better protected as they had to absorb punishment in order to successfully complete their missions. As I have pointed out in past posts the USN claims for Zeros shot down was greatly exaggerated. The losses suffered were not so significant that a decent training program couldn't have made up the losses, which was the real issue. USN aircrew losses in 1942 were very high as well. The life expectancy of a torpedo bomber crew was basically 1 mission. The difference was that the Americans were training their replacements. The other advantage the American had was their emphasis on air sea rescue. A Japanese pilot who was lost on a strike mission was lost forever, whereas the USN tried to rescue as many as possible. As an example, at Midway, of the 10 pilots from VF-8 that had to ditch 7 were rescued and lived to fight another day.
According to Lundstrom the Japanese lost 3 AM97 and 13 Zero pilots in air-to-air combat with F4F in 1942 up to and including Miday. The USN lost 7 F4F pilots to Zeros. Some of those Zero pilots could have been rescued. How many of those pilots would have been saved by self-sealing tanks or armor? Plenty of pilots on both sides died after ditching or bailing out. Regardless, the 9 extra dead pilots that may or may not have been saved by better protection is irrelevant in the overall scheme of things. I don't have the numbers, but I would wager the Japanese lost more Zero pilots when their ships were bombed than in the air-to-air combat. I would also wager that they lost more Zero pilots in training.
In any event the real problem wasn't its performance advantage over the F4F, it was the need to climb fast enough to intercept bombers. USN action reports are chock full of complaints about the F4Fs being unable to climb fast enough to intercept before the bombers attacked. Naval fighters had two main roles in 1942 (fighter bombers weren't a thing at that time in naval warfare,) destroying enemy bombers before they could hit your ships and protecting your bombers from being destroyed so that they could sink the enemy. Fighters playing knights of the air jousting with one another was very romantic, but it isn't the real business of war. Fighters existed because bombers existed.
The Japanese were limited in aircraft design due to their lack of powerful engines. They had to make compromises in design and the case can be made that they made the right choices for the Zero. In addition to their fast rate of climb which would have been tremendous advantage in defense if they were properly directed, their long range and great endurance was a big advantage in strike missions.