Flat Wing Aspect Ratio
7.5
Cruise Speed
607.4555 km/h
Entry Into service
1962-08-01
Maximum Take-Off Weight
61.235 t (paragliders: kg)
Total Fuel Capacity
34825.79
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Total Fuel Capacity |
|
Lockheed P-3 Orion |
61.235 |
34825.79 |
Similar airplanes
All data (29 fields)
- Name
- Lockheed P-3 Orion
- Manufacturer
- Lockheed Corporation
- Description
- The Lockheed P-3 Orion is a four-engined, turboprop anti-submarine and maritime surveillance aircraft developed for the United States Navy and introduced in the 1960s.
- ICAO Code
- P3
- First Flight
- 1959-11-01
- Entry Into service
- 1962-08-01
- Production End
- 1990-01-01
- Designer
- Lockheed Corporation
- Length (m)
- 35.3568
- Height (m)
- 10.0584
- Cockpit Crew
- 11
- Max Speed (km/h)
- 761.1713
- Cruise Speed (km/h)
- 607.4555
- Min Speed (km/h)
- 246.3158
- Max Ceiling (m)
- 8625.84
- Rate of Climb (m/s)
- 9.906
- Armament
- 10 wing stations in total (3x on each wing and 2x on each wing root) and eight internal bomb bay stations
- Endurance (h)
- 17
- National Origin
- United States of America
- Number Built
- 650
- Powerplant Description
- 4 × Allison T56-A-14 turboprop engines, 3661 kW (4910 hp) each
- Primary Users
- United States Navy, Republic of China Navy , Japan Maritime Self-Defense Force , Republic of Korea Navy
- Status
- Active
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_P-3_Orion
- Flat Wing Span (m)
- 30.1752
- Flat Wing Area (m²)
- 120.77
- Flat Wing Aspect Ratio
- 7.5
- Wake Category
- M
- Number of Engines
- 4