|
Engine Name |
Horse power |
Cylinder Displacement (per Cylinder) |
Compression Ratio |
Number of Cylinders |
Max RPM |
Engine Type |
Prop Reduction |
|
|---|---|---|---|---|---|---|---|---|
|
|
2200 |
|
|
|
3700 |
|
|
|
|
Span |
Length |
Height |
Wing Area |
mtow |
Max HP |
Vmax MPH |
Remarks |
Airfoil Section ROOT / TIP |
Wing Loading |
Power Loading |
Eff.K |
|
41.53 |
31.91 |
15.25 |
279 |
11066 |
2180 |
422 |
|
NACA 2219 NACA 2213
|
39.66 |
5.08 |
0.7886 |
Mean roll rates were calculated by averaging rolls at 250, 300 & 400 mph at5,000, 10,000 and 18,000 ft and corrected to an average stick force of 50
lbs:
Typhoon IB.....54 degrees/sec
(Roll rate of Spit IX with a stick force of 40 lbs is 66 degrees/sec at 300mph at 15,000 ft.)
|
Speed |
Wing Data |
Tanks |
Engine |
|---|---|---|---|
|
422 mph at 18000ft time to 15000ft , 6.2mins ceiling 34000ft 405 mph at 12500 ft time to 12500 3.2 minutes |
Wing incidence 0 degrees Tailplane incidence -0.5 degrees 80 degree flap throw rudder 27 degree throw aileron throw up 18 degrees down 18 degress 30 minutes elevator throw up 24 degress down 24 degress 30 minutes prop diameter 14ft |
Inner Leading Edge - 35 Imp Gal Self Sealing each wing Starboard & Port Main Fuel Tanks - 40 Imp gal each wing Drop tanks 90 Imp gal each Coolant tank behind spinner 7.25 Imp gal Oil tank, aft of firewall - 18 Imp gal |
Prop Anti clockwise from pilot's view.
engine net dry weight 2470 lbs overall len 6'10.5" overall height 3'10" overall width 3'4"
|
