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Intended as fastest autogyro of day, two-seat wingless machine using A-12 and A-14 technology and with usual welded KhMA structure. Scheibe fins on braced tailplane with elevators and direct-control rotor. Main gears with vertical shock struts carried on triangulared outriggers each side of fuselage. Pilot with synchronized ShKAS and observer with twin ShKAS and AFA-13 reconnaissance camera. Chief designer M.L.Mil, construction manager A.A.Kuznetsov. Completed April 1937 and taxi tests began by Chyernavskii and Ivanov, but A-12 crash caused further work to be halted. No reason to doubt airworthiness of A-15 but effectively terminated Soviet autogyro development. Autogyros picked up again at Kharkov, Kuibyshev and Riga 30 years later. Bill Gunston "The Osprey's Encyclopedia of Russian Aircraft", 2000
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Technical data for A-15
Engine: 1 x M-25V,
rotor diameter: 18.0m,
length: 8.6m,
height: 4.1m,
weight empty: 1695kg,
fuel+oil: 385+40kg,
weight loaded: 2560kg,
est. max speed: 260km/h,
min speed: 50km/h,
ceiling: 6400m,
take-off run: 35-60m,
landing run: 0m
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