Boeing B-52 Stratofortress

Length
48.5 m
Flat Wing Span
56.4 m
Height
12.4 m
Flat Wing Area
370 m²
Cruise Speed
818.5833 km/h
Max Speed
1046.074 km/h
Max Ceiling
15240 m
Number of Engines
8
Aircraft Engine
First Flight
1952-04-15
Entry Into service
1955-02-01
Number Built
744
Maximum Take-Off Weight
221.323 t (paragliders: kg)

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Aircraft Weight Variants

Aircraft Maximum Take-Off Weight (t (paragliders: kg))
Boeing B-52 Stratofortress 221.323

Similar airplanes

Name Length (m) Flat Wing Span (m) Max Seating
Dornier Do 214 51.6 60 40 Compare
Convair YB-60 52.1208 62.7888 Compare
All data (26 fields)
Name
Boeing B-52 Stratofortress
Manufacturer
Boeing
Description
The Boeing B-52 Stratofortress is an American nuclear-capable subsonic jet-powered strategic bomber.
ICAO Code
B52
First Flight
1952-04-15
Entry Into service
1955-02-01
Designer
Boeing
Length (m)
48.5
Height (m)
12.4
Cockpit Crew
5
Max Speed (km/h)
1046.074
Cruise Speed (km/h)
818.5833
Max Ceiling (m)
15240
Rate of Climb (m/s)
31.85
Armament
1 × 20 mm (0.787 in) M61 Vulcan cannon originally mounted in a remote-controlled tail turret on the H-model, removed in 1991 from all operational aircraft.; Approximately 70000 lb mixed ordnance; bombs, mines, missiles, in various configurations.
National Origin
United States of America
Number Built
744
Powerplant Description
8 × Pratt & Whitney TF33-P-3/103 turbofans, 76 kN thrust each
Primary Users
United States Air Force, NASA (historical)
Status
In service
Wikipedia Article (URL)
en.wikipedia.org/wiki/Boeing_B-52_Stratofortress
Flat Wing Span (m)
56.4
Flat Wing Area (m²)
370
Wake Category
H
Aircraft Engine
Pratt & Whitney JT3D
Number of Engines
8