Cruise Speed
333.1342 km/h
Entry Into service
1947-03-01
Maximum Take-Off Weight
36.2398 t (paragliders: kg)
Maximum Range
3471.355 km
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Lockheed P-2 Neptune |
36.2398 |
3471.355 |
Similar airplanes
All data (26 fields)
- Name
- Lockheed P-2 Neptune
- Manufacturer
- Lockheed Corporation
- Description
- 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
- P2
- First Flight
- 1945-05-17
- Entry Into service
- 1947-03-01
- Service End
- 1984-01-01
- Designer
- Lockheed Corporation
- Type
- Maritime patrol and anti-submarine warfare aircraft
- Length (m)
- 27.7368
- Height (m)
- 8.8392
- Cockpit Crew
- 7
- Max Speed (km/h)
- 584.1919
- Cruise Speed (km/h)
- 333.1342
- Max Ceiling (m)
- 6827.52
- Armament
- 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
- National Origin
- United States of America
- Number Built
- 1177
- Powerplant Description
- 2 × Wright R-3350-32W Duplex-Cyclone 18-cylinder air-cooled radial piston engine, 2759 kW (3700 hp) each
- Primary Users
- United States Navy, Japan Maritime Self-Defense Force , Royal Australian Air Force , Royal Canadian Air Force
- Status
- Retired
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_P-2_Neptune
- Flat Wing Span (m)
- 31.3944
- Flat Wing Area (m²)
- 92.903
- Wake Category
- M
- Number of Engines
- 2