USSR T-26/A-2

Tweet The T-26/A-2 based on the existing Light Tank and was in use from 1932. General Details Specifications Operational Date(s) 1932 Ordnance classification Quantity Produced 0 Weight unknown Crew 3 M.G's small 2 M.G's large(>10mm) n/a Length 4.85 mtr Width 2.42 mtr Height 2.08 mtr Engine Details/Performance Max Road Speed 22 mph Max Cross Country Speed 15 mph Range Road 87 miles Range Cross Country 60 miles Fuel Type Unknown Fuel Capacity 40 gal Horse Power 91 hp Power/Weight unknown General Information The T-26/A-2 based on the existing Light Tank and was in use from 1932. It was armed with 2 light machine guns. Armour Details Turret Front 15mm @ 30° (17mm) Side 10mm @ 30° (12mm) Rear 6mm @ 0° (6mm) Top 6mm @ 90° (6mm) Superstructure Front 15mm @ 45° (21mm) Side 15mm @ 30° (17mm) Rear 15mm @ 0° (15mm) Top 15mm @ 45° (21mm) Hull Front 15mm @ 30° (17mm) Side 15mm @ 30° (17mm) Rear 15mm @ 0° (15mm) Top 6mm @ 90° (6mm) Armour (x)mm @ (y)° (Effective mm @ 0°) Effective Armour - Maximum 21 mm - Minimum 6 mm

Hit probability is based on a static 2 x 2.4 metre panel at 0 degrees(vertical) at the range specified.

The data that has been used to create these records has come from Wikipedia, The Lone Sentry, The Bundes Archive and numerous books and websites that have provided the detailed information that has not been available anywhere else. The information we use to calculate the penetration tables, flight times and the hit probability comes from the Gun Calibre, the Shell Mass(Kg) and the muzzle velocity, plus range reductions to allow for gravity and wind resistance. This calculation originally came from a pre-war Krupp calculation which has been modified, and seems to fit the actual test results.

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