Dewoitine

Dewoitine D.371Camp

Antonov An-8 • Fighter

Dewoitine D.371
  • First flight1931
  • Introduction958
  • StatusRetired
  • Number built87

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
1
Length
7.44 m
Wingspan
11.79 m
Height
3.19 m
02

Performance

Maximum speed
400 km/h
Range
1,150 km
Service ceiling
36,100 ft
03

Powerplant

Powerplant
1 × Gnôme-Rhône 14Kds 14 cylinder two-row air-cooled radial piston engine (800 hp)
04

Armament

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