Originally posted by Soda
Was there any significant structural difference between the two that would account for this?
The biggest difference was in wingspan (over 3 ft), however the profile remained the same.
A6M2 Model 21:Wingspan, 39 ft. 4 7/16 in.;
length, 29 ft. 8 11/16 in.;
height, 10 ft. 1/16 in.;
wing area, 241.541 sq. ft.;
empty weight, 3,704 lb.;
loaded weight, 5,313 lb.;
maximum weight, 6,164 lb.;
wing loading, 22 lb./sq.ft.;
power loading, 5.5lb./hp;
maximum speed, 331 mph at 14,950 ft.;
cruising speed, 207 mph;
climb to 19,685 ft., 7 min. 27 sec.;
service ceiling, 32,810 ft.;
normal range, 1,160 st. miles;
maximum range, 1,930 st. miles.
A6M5 Model 52: - same airframe as A6M5 model 52 b
Wingspan, 36 ft. 1 1/16 in.;
length, 29 ft. 11 7/32 in.;
height, 11 ft. 6 5/32 in.;
wing area, 229.27 sq. ft.;
empty weight, 4,136 lb.; ***
loaded weight, 6,025 lb.;***
wing loading, 26.3 lb./sq. ft.;
power loading, 5.3 lb./hp;
maximum speed, 351 mph at 19,685 ft.;
cruising speed, 230 mph.;
climb to 19,685 ft., 7 min. 1 sec.;
service ceiling, 38,520 ft.;
maximum range, 1,194 st. miles.
*** (A6M5b was slightly heavier, due to added armor protection and different armament - 125 rounds instead of 100 per cannon, one 7.7mm type 2 MG replaced with 13.2mm type 3 MG, armored windshield, etc)