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I have to wonder if the Japanese Military felt that the Zero needed to be replaced?
It seems a stretch to believe such a simplistic view of a reaction to the strategic situation Japan found itself in, but Mitsubishi's resources did focus on the J2M and improving the A6M, rather than concentrating on pushing the A7M toward service status. One author hints at the fact that Mitsubishi was overworked and under resourced but that doesn't explain the effort stream channeled toward improving the A6M instead of developing the A7M...
By 1944, the slow development of the A20 had given a reliable engine for the A7M2 but that was much too late.
There were probably vibration problems as I have read that rubber mounting buffers had to be installed in the Ki-83. Goodwin and Starkings "Japanese Aero-Engines" has "… and by late 1944 the few hand-built examples completed by then were running reliably and smoothly." on page 116.
Engine issues certainly sound like a logical reason behind delay in the project toward 1944/45, but again, why did Mitsubishi bring the project to a halt in 1940, then re-instate it in 1942? Did the government/military halt development? That seems the most logical reason, I'm sure Horikoshi and Co would have been following orders. Another example of the lack of strategic foresight the Japanese military regime displayed.
The J2M was an IJN aircraft, but was NOT a carrier aircraft. Not saying anything, just trying to be clear that the J2M was land-based.
Just an idea but the the Japanese engine development was a bit behind the times.
The aircraft development times were also behind the curve/s.
In 1939 (or earlier) to 1941/42 some other aircraft chose the route of small wing and high wind loading to get the max performance from smaller engines.
For the Japanese the "idea" of a interceptor may have also made sense because they had no (or little) radar coverage.
Once starting it on that path it is hard to stop.
That has always baffled me, why Mitsubishi chose a rival firm's engine instead of their own Kinsei. Perhaps the latter wasn't immediately available for use in the prototypes?an opportunity to choose a more powerful engine as a starting point, with Mitsubishi already having two of those in the pipeline at the time.
That has always baffled me, why Mitsubishi chose a rival firm's engine instead of their own Kinsei. Perhaps the latter wasn't immediately available for use in the prototypes?
Mea culpa. Cheers.
That has always baffled me, why Mitsubishi chose a rival firm's engine instead of their own Kinsei. Perhaps the latter wasn't immediately available for use in the prototypes?
We can note that Mitsubishi designed the Zero around the least powerful of their engines. I'll agree that Japanese engines were not the greatest in a time period we are taking a look, there was still an opportunity to choose a more powerful engine as a starting point, with Mitsubishi already having two of those in the pipeline at the time.
Read on down to item 4.B. RECOMMENDATIONS: "Suitable means of maintaining cockpit heat at altitude be installed. (Cockpit heater on P-39N is best seen to date)."The test in question was concluded on January 26, 1943. That's almost a year before the P-38 starting flying long range escort missions over Germany. In fact the tests were being conducted in the same time frame that the time the P-38 was entering combat in the Pacific and North Africa. Regardless of who decided not to improve the heating there was plenty of time to implement a fix before the P-38J began having issues over Germany.
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I would certainly agree that the P-38F was superior to its American contemporaries.
They always test the newer models against the P-39D-1 which is the heaviest and lowest powered model produced in 1942.