Flat Wing Area
153.6616 m²
Flat Wing Aspect Ratio
9.17
Cruise Speed
547.177 km/h
Entry Into service
1943-01-01
Maximum Take-Off Weight
62.369 t (paragliders: kg)
Maximum Range
8690.458 km
Pictures
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Aircraft Weight Variants
| Aircraft |
Maximum Take-Off Weight (t (paragliders: kg)) |
Maximum Range (km) |
|
Lockheed Constellation |
62.369 |
8690.458 |
Similar airplanes
All data (30 fields)
- Name
- Lockheed Constellation
- Manufacturer
- Lockheed Corporation
- Description
- The Lockheed Constellation ("Connie") is a propeller-driven, four-engined airliner built by Lockheed Corporation starting in 1943.
- ICAO Code
- CONI
- First Flight
- 1943-01-09
- Entry Into service
- 1943-01-01
- Production End
- 1958-01-01
- Service End
- 1978-01-01
- Designer
- Lockheed Corporation
- Type
- Airliner and transport
- Length (m)
- 35.3568
- Height (m)
- 7.3152
- Cockpit Crew
- 5
- Max Seating
- 95
- Max Speed (km/h)
- 606.7227
- Cruise Speed (km/h)
- 547.177
- Min Speed (km/h)
- 160.9344
- Max Ceiling (m)
- 7315.2
- Rate of Climb (m/s)
- 8.2296
- Capacity Description
- typically 62–95 passengers (109 in high-density configuration) / 18300 lb payload
- Number Built
- 856
- Powerplant Description
- 4 × Wright R-3350-DA3 Duplex-Cyclone 18 cylinder air-cooled turbocharged radial piston engines, 2424 kW (3250 hp) each
- Primary Users
- Trans World Airlines
- Status
- In very limited service
- Wikipedia Article (URL)
- en.wikipedia.org/wiki/Lockheed_Constellation
- Flat Wing Span (m)
- 38.4048
- Flat Wing Area (m²)
- 153.6616
- Flat Wing Aspect Ratio
- 9.17
- Wake Category
- M
- Number of Engines
- 4