Antonov An-8

1955


TRANSPORT	Virtual Aircraft Museum / USSR / Russia / Antonov

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.

Specification

CREW	6
PASSENGERS	70
ENGINE	2 x turbo-prop AI-20D, 3810 kW
WEIGHTS
Take-off weight	43400 kg	95681 lb
Empty weight	24400 kg	53793 lb
DIMENSIONS
Wingspan	37.0 m	121 ft 5 in
Length	30.7 m	101 ft 9 in
Wing area	117.2 m²	1261.53 sq ft
PERFORMANCE
Max. speed	520 km/h	323 mph
Cruise speed	450 km/h	280 mph
Ceiling	9600 m	31500 ft
Range w/max.fuel	3900 km	2423 miles
Range w/max payload	1000 km	621 miles
ARMAMENT	2 x 23mm machine-guns

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