France Renault FT Kegresse-Hinstin M24/25 Ordnance classification - Light Tank

Tweet The Renault FT Kegresse-Hinstin M24/25 was designed in 1924, manufactured by Renault based on the existing fully tracked Light Tank and was in use from 1925 to 1930. General Details Specifications Operational Date(s) 1925 - 1930 Ordnance classification Light Tank Quantity Produced 10 Weight 6.5 tonne Crew 2 M.G's small 1 M.G's large(>10mm) n/a Length 4.08 mtr Width 1.74 mtr Height 2.15 mtr Engine Details/Performance Max Road Speed 8 mph Max Cross Country Speed 4 mph Range Road 35 miles Range Cross Country 14 miles Fuel Type Petrol Fuel Capacity unknown Horse Power 35 hp Power/Weight 5 hp/tonne General Information The Renault FT Kegresse-Hinstin M24/25 was designed in 1924, manufactured by Renault based on the existing fully tracked Light Tank and was in use from 1925 to 1930. The vehicle was powered by Renault '4 Cylinder 35hp' petrol powerplant producing 35 HP which could drive the vehicle on roads at up to 8 mph with a range of about 35 miles before refuelling. Its cross country performance was poor providing a max speed of about 4 mph and a range of about 14 miles. It was armed with 1 light machine gun. This was a development version of the FT17 with Kegresse-Hinstin suspension and rubber tracks. Armour Details Turret Front 16mm @ 13° (16mm) Side 16mm @ 15° (17mm) Rear 16mm @ 15° (17mm) Top 8mm @ 65° (9mm) Superstructure Front 16mm @ 70° (47mm) Side 16mm @ 0° (16mm) Rear 16mm @ 0° (16mm) Top 6mm @ 67° (7mm) Hull Front 16mm @ 29° (18mm) Side 16mm @ 0° (16mm) Rear 16mm @ 0° (16mm) Top 6mm @ 67° (7mm) Armour (x)mm @ (y)° (Effective mm @ 0°) Effective Armour - Maximum 47 mm - Minimum 7 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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