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And the last time he flew one?Easily, when the only person in the world who owns four Zeros says so.
And kudos to him, but at the same time I see no substancial evidence supporting his claim about the Camarillo ZeroGranted, there may be some pro-Japanese bias on the part of the source, but I know how hard Mr. Harada fought for years to get an original Sakae for his airworthy example. It sat, otherwise completely restored, with no engine for close to half a decade.
In your experience have you ever flown any of these aircraft (or similar)?There may likewise be some pro-American bias in this as well on the part of some pilots. I don't know. I just thought I'd help answer the questions posed in this thread with my experience.
Ok, I'll but that, but according to thouse who fly the Camarillo Zero, the fact that an 1830 is on the front end of the aircraft means little under 200 knots.The Sakae series of radials were amazing pieces of technology in terms of their weight in relation to their power output. It, and the similarly designed Mitsubishi powerplant that lost out to it in competition in 1939, were in large part responsible for the ultimate success of the Zero - so said Jiro Horikoshi. Since no other nation took the 'light fighter' concept to fruition as did the Japanese - nobody mass-produced comparable engines to the Sakae. Thus . . . today it's essentially irreplaceable and the performance of Zeros equipped with lesser (heavier) powerplants see their performance suffer. Now, it may be that the "suffered dramatically" opinion that originated with Nobuo Harada took into consideration fuel consumption - something that obviously would not play any role in an air show hop.
We would if this was a boaring political forum.But, Jeez! Now I know why I avoid posting in forums. Put this effort into debating heath care or something.
Ron Cole
I am not judging it based on ground observations. I am basing it on conversations with people who actually FLY the aircraft that exist and fly today.That's kind of a bizarre statement. In the first place none of these aircraft are pushed to their limits during airshow displays - especially the Chino Zero which is the only originally-powered Zero in the world and is flown very cautiously, as it should be. Secondly, how can anyone judge and compare performances of aircraft from the vantage point of the ground???
I have heard that argument before and from what I have read and seen, it had basis from other engines.And, indeed, the myth that the Nakajima Sakae was a copy of any other engine originated in the bigoted environment of wartime when whites couldn't conceive that the Japanese were capable of independent ingenuity.
I didn't post my information to start an argument. Just thought I'd share what I know, since the question was posed. My friend Naburo Harada, who owns several restored Zeros in Japan and oversees the Harada Collection (The Harada Collection), knows more than anyone on earth about this engine, the power to weight issue, and the consequences of not using the original Sakae.
Ron Cole
View: https://www.youtube.com/watch?v=UmUseKNrh6Q
I think Eric, knows this guy. Says nothing about this aircraft's "airshow" performance being affected by the instllation of the 1830.
This discussion seems lively, doesn't it? The propeller on our Zero is Japanese and is interchangeable with a Hamilton Stanard since it was made under license in Japan to H-S drawings.
The Sakae 21 engine is Japanese and is NOT interchangeable with a Gnome-Rhone 14 or any other Gnome -Rhone. The Japanese made improvements and built their own design ... and it is reliable and well made. If you own the 1944 Fighter Conference proceedings, you will see that the Zero is the ONLY fighter in the group that didn't experience a mechanical failure in the flight tests. Surely that says SOMETHING about the Japanese Sakae 21 engine, huh? Ours still runs great every time we crank it up, and it's 70 years later. It is the ONLY example flying and it is DEAD reliable so, unlike the American or British or Russian radials, we have a population of ONE and it runs great all the time.
MTBF? ..... LONG .... in our experience ...
I'm impressed with it, even if it IS a lower-power engine.
Of course, I also think the Zero is the prettiest radial-powered fighter ever made ... and that may be personality fault that is not correctable ...
Maybe this one?
Ron, understand that on this site, there is a great wealth of information gathered, exchanged and debated and yes sometimes it turns into an argument. Like you many of us have spent many years around aircraft (I've been in the aviation business going on 34 years, have an A&P/IA, CFII and I have also worked on and flown several different war birds and jet aircraft), so when a "broad brush" comment is made, those of us who have worked on these war birds tend to question their validity and if there is something to be learned based on documented fact or direct information from a pilot of maintainer, even the better. I never thought you were condescending so please don't think any of our comments were, it's a matter of extracting and validating accurate information so we can all learn by each other's experience.I shared my information, which was my intent. I'm an aviation artist. That's my living and my business. I don't have time to argue for the sake of arguing. To each his own, but that's not my idea of a wise expenditure of effort. I apologize if that sounds condescending.
I have an old copy of Flight Journal, where Corky Meyer writes about testing, I believe it was the Aleutian Zero, and he mentions that the engine in the plane was a copy, or license built copy of a American engine. I'll have to pull the magazine for the accurate info, it's part of my bathroom library. But IIRC, he states the engine was a copy even down to the American company's logo (cannot remember which American company he is referring to), which had I believe the middle of the logo had been altered with a Japanese stamp or design in the middle of the logo? Anyone have any info on this? I have had this question on my mind for quite some time, and this seemed like a opportune time to ask. Is Corky Meyer incorrect? Anyone have any info? I'll pull the magazine and re-read the article to get the exact details as they were written. It may not have been Corky, but that is the name that is sticking in my mind.
Thanks in advance. Great thread by the way, and thanks to all who have contributed.
In regards to the engines, I have heard the Gnome Rhone 14k variant, and have also heard that it was "derived" from the P&W Twin Wasp.
Ron Cole,
Our J2M Raiden has some serious intergrannular corrosion issues, but is a beautiful aircraft. When we finish the Bell YP-59A, I'd love to take a crack at the Raiden! It would require a new wing spar and spar caps, not to mention many other items including longeron, but could be done. The only question is whether or not the Planes of Fame staff wants the Raiden to be restored or prefers it as-is.
As for the Zero engine:
The Nakajim Sakae 21 is a Japanese design, not P&W and not Gnome-Rhone. They used design features taken fromm other radials, but ALL radials do that ... or else they're completely different engines.
There are other two-row, 14-cylinder radials out there, but the Sakae 21 is not a copy of any of them as far as I know.
I don't know about the Zero needing a Sakae to fly like a Zero ... it would seem the powerplant would be unimportant as long as the weight and power are close and the RPM range is similar. However, I don't really KNOW, so I can't argue the point at all. I'll ask about the weight, power, and RPM and see what comes up. We can find the weight, power, and RPM on the internet, but I prefer to verify with actual pilots and mechanics on an original A6M5 Zero to trusting Wikipedia ... which is wrong almost as often as Obama.
My understanding is that all other Sakae-like replacement engines are moderately larger than the Sakae and usually require new-build cowlings to accommodate them - at least that being the case with the A6M2 - and thus resulting in a host of modifications that go beyond just an engine swap, not to mention what that does to the center of gravity. Such issues resurrect the original problem with the Zero in terms of its relative inability to be modified in wartime to accommodate heavier equipment. It was the first aircraft in the world, it is believed, to have incorporated its duraluminum skin as a structural member. Before that, aircraft were structurally designed on paper to withstand certain forces, then covered to be aerodynamic - but that's how far the designers went to keep the Zero light. It doesn't suffer added weight well, in any form.
From what I understand the Camarillo Zero's cowl is actually the same size as the original Zero cowl however there were internal components altered to accommodate the slightly larger P&W engine and again from what I understand the size difference is nominal. Eric might be able to get info on that as he's a regular around that aircraft but from what I read about the two engines the difference in diameter is about 3 inches. C/G issues in minor structural mods are usually non events and many times are easily remedied by using ballast in the nose or tail, if even necessary. As a matter of fact sometimes ballast is necessary to compensate for obsolete wartime equipment (mainly radios) removed during the restoration.
I don't believe the Zero was first aircraft to incorporate aluminum (or duralumin) skin as a structural member. I can recall portions of the DC-3 that had skin carrying a structural load and were repair sensitive if damage was over a certain size.
Ron, understand that on this site, there is a great wealth of information gathered, exchanged and debated and yes sometimes it turns into an argument. Like you many of us have spent many years around aircraft (I've been in the aviation business going on 34 years, have an A&P/IA, CFII and I have also worked on and flown several different war birds and jet aircraft), so when a "broad brush" comment is made, those of us who have worked on these war birds tend to question their validity and if there is something to be learned based on documented fact or direct information from a pilot of maintainer, even the better. I never thought you were condescending so please don't think any of our comments were, it's a matter of extracting and validating accurate information so we can all learn by each other's experience.
An old saying - validated performance numbers don't lie, oppinions can be debated!