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Antonov An-8 ✕ Lockheed P-2 Neptune ✕
Manufacturer Antonov Lockheed Corporation
Description The Antonov An-8 (NATO reporting name: Camp) is a Soviet-designed twin-turboprop, high-wing light military transport aircraft. The Lockheed P-2 Neptune (designated P2V by the United States Navy (USN) prior to September 1962) was a maritime patrol and antisubmarine warfare (ASW) aircraft.
ICAO Code AN8 P2
First Flight 1956-02-11 1945-05-17
Entry Into service 1958-01-01 1947-03-01
Production End 1961-01-01
Service End 1984-01-01
Designer Antonov Lockheed Corporation
Type Military transport aircraft Maritime patrol and anti-submarine warfare aircraft
Length (m) 26 27.7368
Height (m) 9.7 8.8392
Cockpit Crew 6 7
Max Seating 48
Max Speed (km/h) 610 584.1919
Cruise Speed (km/h) 480 333.1342
Max Ceiling (m) 9600 6827.52
Rate of Climb (m/s) 7.12
Armament One 23 mm cannon in the tail turret. 8,000 lb (3,629 kg) including free-fall bombs, depth charges, and torpedoes; 2.75 in (70 mm) FFAR in removable wing-mounted pods
Capacity Description 48 persons / 11000 kg max payload
National Origin United States of America
Number Built 151 1177
Powerplant Description 2 × Ivchenko AI-20D turboprop engines, 3863 kW (5180 hp) each 2 × Wright R-3350-32W Duplex-Cyclone 18-cylinder air-cooled radial piston engine, 2759 kW (3700 hp) each
Primary Users Soviet Air Force, Aeroflot United States Navy, Japan Maritime Self-Defense Force , Royal Australian Air Force , Royal Canadian Air Force
Status One in service with Uhuru Airlines Retired
Wikipedia Article (URL) en.wikipedia.org/wiki/Antonov_An-8 en.wikipedia.org/wiki/Lockheed_P-2_Neptune
Flat Wing Span (m) 30 31.3944
Flat Wing Area (m²) 117.2 92.903
Flat Wing Aspect Ratio 11.7
Wake Category M M
Number of Engines 2 2