Antonov An-8

· Antonov

Airplanes

Length

26 m

Flat Wing Span

30 m

Height

9.7 m

Flat Wing Area

117.2 m²

Flat Wing Aspect Ratio

11.7

Max Seating

Cruise Speed

480 km/h

Max Speed

610 km/h

Max Ceiling

9600 m

Number of Engines

First Flight

1956-02-11

Entry Into service

1958-01-01

Number Built

151

Maximum Take-Off Weight

40 t (paragliders: kg)

Maximum Range

2780 km

Pictures

No pictures yet for this family.

Aircraft	Maximum Take-Off Weight (t (paragliders: kg))	Maximum Range (km)
Antonov An-8	40	2780

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Bartini Beriev VVA-14		25.97	30		Compare
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Gulfstream V	Rolls-Royce BR700	29.3827	28.4836		Compare
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All data (29 fields)

Name: Antonov An-8
Manufacturer: Antonov
Description: The Antonov An-8 (NATO reporting name: Camp) is a Soviet-designed twin-turboprop, high-wing light military transport aircraft.
ICAO Code: AN8
First Flight: 1956-02-11
Entry Into service: 1958-01-01
Production End: 1961-01-01
Designer: Antonov
Type: Military transport aircraft
Length (m): 26
Height (m): 9.7
Cockpit Crew: 6
Max Seating: 48
Max Speed (km/h): 610
Cruise Speed (km/h): 480
Max Ceiling (m): 9600
Rate of Climb (m/s): 7.12
Armament: One 23 mm cannon in the tail turret.
Capacity Description: 48 persons / 11000 kg max payload
Number Built: 151
Powerplant Description: 2 × Ivchenko AI-20D turboprop engines, 3863 kW (5180 hp) each
Primary Users: Soviet Air Force, Aeroflot
Status: One in service with Uhuru Airlines
Wikipedia Article (URL): en.wikipedia.org/wiki/Antonov_An-8
Flat Wing Span (m): 30
Flat Wing Area (m²): 117.2
Flat Wing Aspect Ratio: 11.7
Wake Category: M
Number of Engines: 2