Antonov An-8
1955
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  TRANSPORTVirtual Aircraft Museum / USSR / Russia / Antonov  

Antonov An-8

Military and civil transport aircraft of similar type designed for the Soviet Air Force and Aeroflot respectively. Both aircraft carried the NATO reporting name Camp. The prototype of the former was exhibited at Tushino in 1956, powered by two 3,800kW Kuznetsov turboprop engines and with a cannon in a tail turret.

Antonov An-8


Specification 
 CREW6
 PASSENGERS70
 ENGINE2 x turbo-prop AI-20D, 3810 kW
 WEIGHTS
    Take-off weight43400 kg95681 lb
    Empty weight24400 kg53793 lb
 DIMENSIONS
    Wingspan37.0 m121 ft 5 in
    Length30.7 m101 ft 9 in
    Wing area117.2 m21261.53 sq ft
 PERFORMANCE
    Max. speed520 km/h323 mph
    Cruise speed450 km/h280 mph
    Ceiling9600 m31500 ft
    Range w/max.fuel3900 km2423 miles
    Range w/max.payload1000 km621 miles
 ARMAMENT2 x 23mm machine-guns

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