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As for moving up the P-82, I think that if they job was given to Fisher instead of that XP-75 monstrosity it could have been moved up. Basing it on the P-51D instead of the P-51H should have been entirely feasible.
. . . that XP-75 monstrosity . . .
Better install an ejection seat.I will say ten .50 cal machine guns as standard armament was an impressive number. Though I wonder what the actual firing rate would have been for the four nose-mounted guns which had to be synchronized to fire between two (counter-rotating) propellers.
Please note that the dish could and did turn 90 degrees from the fuselage axis and is nearly there in the photo.
The radar used on the F4U, F6F and P-38M used a 19in parabolic reflector.
That is, if you can lug it into the air. Was that "shape" in the P82 photograph actually crammed full of electronics, or partially a low drag fairing for the antenna? After reading Token's description of the 360° scanning antenna, I'm wondering if that "shape" isn't an attempt to get the antenna down and forward for a wider azimuth usable scan?But if you you want to get out and look around, see what you can find, do a nighttime fighter sweep, the SCR-720 was much better.
The P-82 was based on the XP-51F, which was a lightened version of the P-51 (and the basis of the P-51H).Basing it on the P-51D instead of the P-51H should have been entirely feasible.
That is, if you can lug it into the air. Was that "shape" in the P82 photograph actually crammed full of electronics, or partially a low drag fairing for the antenna? After reading Token's description of the 360° scanning antenna, I'm wondering if that "shape" isn't an attempt to get the antenna down and forward for a wider azimuth usable scan?
The earliest AN/APQ72s in the F4 were all tube, no solid state (I'm told) and many times the power and range of the SCR720, but they weren't THAT big.
The picture is in post #247 in this thread and is alleged to be an SCR720 installation. Just eyeballing the photos, it looks as if that 360° dish could get close to 270° unobstructed usable azimuth at zero elevation angle and below, and maybe 220 or so above that. That pod looks awfully big for an AI radar. It's hard to imagine that entire volume is filled with electronics.As for the F-82's, various models carried the SCR-720, the APS-4, and the APG-28. I have no idea what model is in the picture mentioned.
So if you integrated that into an enlarged P38 schnoz it might work after all, and perhaps counterbalance the aft RO position? It would be already out in front of the props.One reason the P-82 pod is so big is that tgey needed to get the radar out front so the props were not in the way. The APS-4 used on the P-82D used the same pod as the P-82C.
The antenna used what is called a helical scan or a unidirectional sector scan. It spun completely around 360 degrees, stepped up, spun 360 again, stepped up, etc. When it reached its upper scan limit it started back at the lowest currently set elevation. The radar only transmitted while the radar was pointed in the forward hemisphere, and was blanked when pointed aft. This made the mechanics of the radar more simple, and simple means light. Basically it consisted of an azimuth drive motor that spun the antenna around, the same direction all the time, and a more restricted elevation drive motor that controlled elevation. To construct an antenna, and more importantly drive system, that sweeps an antenna rapidly side to side is more complex. And for reference such a scan, back and forth in a sector, is called a bidirectional sector scan.
The additional weight of the radar pod created very few performance problems with the F-82F having a top speed of 460 mph. The G's SCR-720 radar weighed slightly less than the APG-28 and thus the aircraft's performance was slightly better.
The F, G, and H Twin Mustang was not a pilot's ideal night fighter due to the cockpit's limited field of view, and poor landing characteristics especially at night. Moreover, during nocturnal operations, the pilot and radar operator found it difficult to maintain night vision due to engine exhaust flame, instrument glare and the bright flashes from the aircraft's machine guns.
From an operational standpoint, some pilots felt a psychological discomfort of impending doom of a mid-air collision when they caught sight of the co-pilot/radar operator's fuselage out of the corner of their eyes. Another problem was with the J-8 Altitude Gyro used during instrument flying. Pilots either loved it or hated it because it read exactly opposite to the presentation of conventional gyroscopic instruments. When the miniature aircraft on the gyro appeared 'below' the reference line, instead of descending the F-82 was actually climbing and so, during an instrument landing approach, the pilot had to remain cognizant of what the aircraft was actually doing.