An old wish of mine, I just shined it up some.
A6M3 (Navy Type 0 Carrier Fighter Model 22) "Hamp"Engine: x1 Nakajima Sakae 21 engine w/two-stage supercharger [1,130hp at take-off, 1,100hp at 9,350ft, 980hp at 19,685ft] w/ 3-bladed constant speed Sumitomo propeller
Speed: Altitude TAS Man. Press.
Ft. MPH " Hg. Blower
------------------------------------------------------------------------------------------
0 280 36.0 Low
5,000 296 36.0 Low
*9,300 310 36.0 Low
10,000 310 35.2 Low
15,000 304 29.3 Low
15,000 307 36.0 High
**15,300 308 36.0 High
20,000 305 31.0 High
25,000 300 25.6 High
30,000 294 20.3 High
* Low blower critical altitude for climb
** High blower critical altitude for climb
Climb Rate:Alt. Climb Rate Climb Time Blower Man. Press. TAS
Ft. Ft./min Min. " Hg. MPH
--------------------------------------------------------------------------------------------------
0 3,260 0 Low 36.0 140
5,000 3,060 1.58 Low 36.0 151
*7,000 2,980 2.24 Low 36.0 155
10,000 2,460 3.35 Low 32.8 159
10,000 2,340 3.35 High 36.0 159
**15,000 2,180 5.55 High 36.0 168
20,000 1,650 8.19 High 28.8 177
25,000 1,120 11.84 High 23.2 185
30,000 600 17.79 High 19.2 193
* Low blower critical altitude for climb
** High blower critical altitude for climb
Ceiling: 11,050 m
Fuel: 570 liters internal + 330 liters in a centerline drop tank
Range: 1,284 naut miles
Weight: 4,107lb empty, 5,835lb loaded
Dimensions:Span 36 ft. 2 1/4 in.
Length 29 ft. 9 in.
Height 9 ft. 2 in.
Wing area 232 sq. ft.
CG Approx. 31% MAC, 0.075 in. forward of main spar
Air foil (root) NACA 2315
Air foil (tip) NACA 3309
Max. chord thickness, center line 8 1/4 in.
Max. chord thickness, tip 4 1/8 in.
Chord, centerline 8 ft. 3 in.
Chord, fuselage side (20 in. from centerline) 8 ft. 1 in.
Chord, tip 4 ft. 1 1/4 in.
Mean chord 6 ft. 4.8 in.
Aspect ratio 5.5
Dihedral, on 30% chord 6.5 deg.
Taper ratio 44
Wing loading 21.3 lb/sq/ft
Power loading 5.42 lb/hp/sq/ft
Aileron area, total 20.2 sq. ft.
Aileron span, each 9 ft. 7 5/8 in.
Flap area, total 16.44 sq. ft.
Flap span, each 5 ft. 3 3/4 in.
Horizontal tail area, total 51.68 sq. ft.
Stabilizer area, total 40.84
Airfoil, root NACA-.0009-64 approx.
Airfoil, tip NACA-.0010
Span 15 ft. 5 in.
Mean chord 3 ft.
Aspect ratio 5.7
Taper ratio .439
Elevator area, total 10.85 sq. ft.
Percent balance 11.35
Trim tab area 1.19 sq. ft.
Fin area 7.92 sq. ft.
Rudder height 4 ft. 6 in.
Rudder area 7.7 sq. ft.
Rudder area forward hinge line 0.7 sq. ft.
Rudder trim tab area .065 sq. ft.
Percent balance 9.64
Armament: 2x 7.7mm Type 97 machine guns in upper cowl, 2x 20mm Type 99 Model 1 Mark 3 cannon w/100rpg in wings, 2x wing rack 132lb bombs
# Built: 560 Aircraft
Notes: Late production aircraft fitted with long barrel 20mm, Type 99 Model 2 Mark 3 cannon. (Perk Option?)
Sources:http://www.j-aircraft.com/research/zerofacts.htmhttp://www.wwiiaircraftperformance.org/japan/hamp-eb201.htmlhttp://rwebs.net/avhistory/history/Zeke32.htmWhy?Well, the two models of the zero we have already need a face-life eventually, and I'm sure with that being done this one could be modeled in as well. It would flesh out the IJNAF most used fighter plane of the war and help with expand the the Japanese plane-set during scenarios and in general.
(Sorry for the jammed together look of the speed and climb data, for some reason it doesn't want to put in my spaces... If anyone sees anything wrong with this info and/or would like to add anything, don't hesitate to say anything!)