Antonov

Antonov An-8 Camp

Antonov An-8 • Transport

  • First flight11 February 1956
  • Introduction958
  • StatusOperational
  • Number built15

History

The Antonov An-8 (NATO reporting name: Camp) is a Soviet-designed twin-turboprop, high-wing light military transport aircraft.

Development

In December 1951, OKB-153 initiated the design of a twin-engined assault transport aircraft, designated DT-5/8 (Desahntno-Trahnsportnyy [samolyot] – assault transport aircraft), to be powered by two Kuznetsov TV-2 turboprop engines, and fitted with a large rear cargo door to allow vehicles to be driven straight into the hold.[2] On 11 December 1953, the Soviet Council of Ministers issued directive No.2922-1251 to the Antonov OKB, requiring them to build a twin-turboprop transport aircraft derived from the DT-5/8. Bearing the in-house designation Izdeliye P the resulting aircraft had a high wing carrying two turboprop engines, atop a rectangular-section fuselage which could carry 60 troops or 40 passengers. Alternatively. the aircraft could carry a range of vehicles (including ASU-57 assault guns, BTR-40 or BTR-152 armoured personnel carriers) or artillery pieces. The aircraft was fitted with a tricycle undercarriage with main gear units housed in pods on either side of the fuselage, and an upswept rear fuselage providing clearance of the tail unit for loading and unloading.[

Technical data

Specifications

01

Crew & dimensions

Crew
6 (pilot, copilot, navigator, flight engineer, tail gunner, wireless operator)
Length
26 m (85 ft 4 in)
Wingspan
30 m (98 ft 5 in)
Height
9.7 m (31 ft 10 in
02

Performance

Maximum speed
610 km/h (380 mph, 330 kn)
Range
2,780 km (1,730 mi, 1,500 nmi)
Service ceiling
9,600 m (31,500 ft) [1
03

Powerplant

Powerplant
2 × Ivchenko AI-20D turboprop engines (5,180 shp)
04

Armament

Armament
Guns: One 23 mm cannon in the tail turret.