Douglas B-66 Destroyer

Airplanes

Length

22.86 m

Flat Wing Span

21.9456 m

Height

7.0104 m

Flat Wing Area

72.4644 m²

Cruise Speed

850.0673 km/h

Max Speed

1014.895 km/h

Max Ceiling

12009.12 m

Number of Engines

First Flight

1954-06-28

Entry Into service

1956-01-01

Number Built

294

Maximum Take-Off Weight

37.6482 t (paragliders: kg)

Pictures

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Aircraft	Maximum Take-Off Weight (t (paragliders: kg))
Douglas B-66 Destroyer	37.6482

Name	Aircraft Engine	Length (m)	Flat Wing Span (m)	Max Seating
Douglas A-3 Skywarrior		23.1648	21.9456		Compare
Mikoyan MiG 18-50	Lotarev D-36	24.9	23.3	18	Compare
Tupolev '73'		20.32	21.7		Compare
Saab 340 AEW&C	General Electric T700	20.57	21.44		Compare
Grumman Gulfstream II		24.0792	23.4696		Compare
OKB-1 140	Mikulin AM-TKRD-01	19.25	21.87		Compare

All data (24 fields)

Name: Douglas B-66 Destroyer
Manufacturer: Douglas Aircraft Corporation
Description: The Douglas B-66 Destroyer is a light bomber that was designed and produced by the American aviation manufacturer Douglas Aircraft Company.
First Flight: 1954-06-28
Entry Into service: 1956-01-01
Service End: 1975-01-01
Designer: Douglas Aircraft Corporation
Type: Light bomber
Length (m): 22.86
Height (m): 7.0104
Cockpit Crew: 3
Max Speed (km/h): 1014.895
Cruise Speed (km/h): 850.0673
Max Ceiling (m): 12009.12
Rate of Climb (m/s): 25.4
Armament: 2 × 20 mm M24 cannon in radar-controlled/remotely operated tail turret; 15,000 lb (6,800 kg)
National Origin: United States of America
Number Built: 294
Powerplant Description: 2 × Allison J71-A-11 (later Allison J71-A-13) turbojet engines
Primary Users: United States Air Force
Wikipedia Article (URL): en.wikipedia.org/wiki/Douglas_B-66_Destroyer
Flat Wing Span (m): 21.9456
Flat Wing Area (m²): 72.4644
Number of Engines: 2