The B6N was a significant death trap, something that has to be considered when calculating the worth of any aircraft (otherwise the F-104 was the best fighter of the 1960s and early 70s). A strong wind would kill the B6N, unlike the Avenger, a plane that, like all Grumman designs of the era, was almost insanely robust.
Regarding the C6N: If adding a torpedo to an aircraft that was never meant to carry anything more than a two man crew, one 7.7mm mg, and a camera didn't have a massive impact on its performance it would be a miracle (as an example the TBD, which was built from the first drawing as a bomber, was almost 50 MPH faster without a torpedo than with it).
The same sorts of issues existed with pretty much every Japanese design, they were either fragile, unreliable, or both. The range figures for most IJN aircraft are also, unlike at least some U.S. designs, wildly optimistic for any sort of real world use, relying on "clean" aircraft being flown at the leanest possible engine settings and ignoring "form-up" and other issues like idle time on deck (Interestingly, the U.S. went the other way when considering range. As an example the P-38, when pilots were trained to play the same sort of range tricks employed by IJN flyers had close to 40% more endurance. The P-80 has an often repeated range of 1,200 miles (although some source will show as low as 750 miles), yet a clean model managed an unrefueled LA-NYC flight of 2,500 miles at an average speed of 548 MPH.)
The same hold true for speed figures, although in this American designers tended to be as... hopeful as their Japanese counterparts. The most common max speeds quoted for the F6F is 380 MPH, with the F4U at 417 mph, while the N1K1-J is generally quoted at 363 MPH and the A7M at ~390 MPH. It is worth noting the the top speeds for both of these aircraft (as well as most other Japanese and Luftwaffe designs) were achieved during testing by U.S. engineers post war, with the aircraft having the advantage of higher octane fuel than was ever available to the Axis, something that was worth 10-20 MPH and comparable improvements in climb. Again, both aircraft are very good designs, illustrating that Japanese designers took a back seat to no one in WW II, but they were made in scant numbers and had such long gestation periods as to be little more than footnotes.
Can you quote a source for your comments on the B6N. I am curious because I haven't heard this kind of structural weakness mentioned before.
Regarding C6N, Perhaps a couple 550 pound bombs (or perhaps a single 500 kg bomb) would not impact performance as much. This plane at just a bit below 400 mph had the surplus performance to waste this way.
Regarding range estimates, the Japanese were the early long range experts. Flying missions against the Philippines from Taiwan isn't trivial. FWIW, the USN completely discounted the range information that they received from Grumman for the Hellcat because they were unable to come anywhere near reproducing it in practice. In practice, US planes flew on either Auto-Rich or Auto-Lean without a pilot tweaking the mixtures.
I will hold comments regarding the jets because as you pointed out earlier, they are irrelevant to discussions on wartime aircraft.
There are LOTS of misconceptions regarding the performance of Japanese WW2 aircraft. I know I am not the authority on this subject, but here goes anyway:
First of all, increasing octane isn't going to do anything for an engine that isn't tuned for it. Remember this wasn't the era of computer controlled ignition that automatica retards when it detects knocking. Also 10-20 mph needs a LOT of extra power. Consider that the speed increase is the cube root of the power increase assuming nothing else (altitude especially) has changed. Japanese fuel was typically 91-92 octane which is a little lower than US fuel, but German C3 fuel at 96 / 100 octane nominal was MUCH better quality than US fuel as stated in the tests of the FW 190 that now sits at Udvar Hazy. The question is how the octane number is calculated. Is it Research, Motor or (R+M)/2 and is it under rich or lean conditions. Don't group all the Axis together in this regard.
Japanese tended to document "maximum speed" as that achieved with "Military" power and not War Emergency Power. Consider that the official maximum speed in the manual for the A6M2 was only 316 mph and the USN test of Koga's Zero achieved 332 mph in a plane that wasn't in perfect shape. Saburo Sakai believed it was 345 mph with "overboost" which would have been the equivalent of our WEP which is how US aircraft are tested.
Typical sources list the maximum speed of the J2M3 Raiden 21 as 371 mph. The US tests of a J2M2 Raiden 11 achieved 407 mph and the J2M3 Raiden 21 achieved 417 mph. If you look at photographs of the J2M3 (Tail Code S12), you will note that it did NOT have the "High Activity" version of the propeller that can be seen on a photo of a Yokosuka plane that has its tail propped up.
One of the factors that I hinted at earlier is the rather poor performance of the Nakajima Ha-45 Homare engine. This little tiny (1940 Cubic Inch) engine could in theory put out 1990 hp at take-off. It probably actually did this if built and maintained correctly, but under field conditions, 1300 hp was more typical if it ran reliably at all. Consider that the Japanese even worked on replacing the "1990 hp" Homare with a 1500 hp Ha-112 on the Ki-84 Hayate. Sounds like a silly idea if you didn't know about the problems operational aircraft were having. The famous 427 mph Hayate probably was able to perform that well because it had some pretty good mechanics and good spare parts in the post-war USA to keep the Ha-45 up to its design performance.
One other surprising thing I found is that many if not most of the late war Japanese designs had laminar flow airfoils which may account for some performance gains. What is interesting is plotting engine power graphs against maximum speed. If you do this, you find that either the planes built by the Japanese were incredibly draggy or something else is going on to account for the lack of claimed speed.
Regarding Fragility, the Ki-43 Hayabusa had that issue. The A6M Reisen had it also to some extent, but in general, later planes did not. Fragility in structural strength and load bearing really isn't the same thing as proper armour. On the other hand, the F8F Bearcat WAS fragile. Its wing tips were designed to break off at 6G or so.
- Ivan.