Does anyone have or know if the Navy provided a graph or numbers for the climb test?
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Interesting. I have seen three or four other comparisons saying the Vorsairs was superior to the P-51, but never this document.
Interesting that the Corsair is more maneuverable, but not surprising. One of the requirements for a Naval aircraft is good low-speed handling, which naturally translates into good maneuverability at medium speeds. The F4U seems to carry this into higher speeds.
I'm pretty sure an F6F will ALSO out-maneuver any P-51 since it has the most wing area of any single-seat WWII fighter, but it is also slower and likely has not as good roll performance.
The Super Hellcat turned into the Bearcat, but would likely have been a sure winner absent the F8F
The choice of the F4U over the P-51 / P-47 / F6f in Korea is starting to be more clear.
Note that F4U running very high MP compared fleet standard, and to P-51B 67", when 115/145 or 130/50 fuel was available to boost to 75". Note also that P-51B was carrying wing racks to slow it down about 12mph and reduce 500fpm in climb.Does anyone have or know if the Navy provided a graph or numbers for the climb test?
Thanks
Yes, thanks for your response. I've never put too much stock in this test since the Corsairs weren't standard production aircraft drag wise plus one ran at 65" instead of the normal 60" of boost. The Navy claimed that in the climb test "the F4U's are everywhere superior in climb, having an estimated margin of from 750 feet to 1,000 fpm at various altitude levels." In this first loadout, the P-51B weighed 9,423 lbs. and the F4U's weighed 12,162 lbs. (one ran at 65", the other at 60") In the second loadout, the P-51 weighed 9,100 lbs. the F4U's weighed the same 12,162 (same boost settings) with the Navy stating at this loadout "the F4U's are superior in climb to 20,000 feet and the P-51B superior above that altitude to ceiling." Neither of those Navy quotes make sense to me except the P-51B being superior above 20,000 feet. That's why I wondered if there's any data or chart to back up what the Navy said.Note that F4U running very high MP compared fleet standard, and to P-51B 67", when 115/145 or 130/50 fuel was available to boost to 75". Note also that P-51B was carrying wing racks to slow it down about 12mph and reduce 500fpm in climb.
Didn't look to the load outs to see if both were flown at full internal load - and as far as turn and roll performance, pilot skill matters.