The MBB/Kawasaki BK 117 is a twin-engined light utility and transport helicopter developed jointly by Messerschmitt-Bölkow-Blohm of West Germany and Kawasaki of Japan under an agreement signed on 25 February 1977. MBB handled the rigid four-bladed rotor system, tail boom and controls, drawing on the earlier Bo 105, while Kawasaki took the airframe, landing gear and main transmission. The German prototype first flew on 13 June 1979 and the Japanese one on 10 August 1979; German certification came in December 1982 and US FAA certification in March 1983. Early aircraft used two Lycoming LTS101 turboshaft engines. The cabin seats up to ten and the type became widely used for air ambulance, rescue and police work. Each partner kept its own assembly line, and 443 were built before the BK 117 C-2 development, renamed EC145 and later H145, replaced it in production.
Facts
Engine Class Top Speed (km/h) Maximum Mass (kg) EnginePair of Lycoming LTS101 turboshaft engines 1 Connections
Exemplifies
Source MBB/Kawasaki BK 117 (Wikipedia)
Of Make
Source MBB/Kawasaki BK 117 (Wikipedia)
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Manufactured By
Also in Business Atlas: the manufacturer of this subject.
Source MBB/Kawasaki BK 117 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
jointly developed and manufactured by Messerschmitt-Bölkow-Blohm (MBB) of West Germany and Kawasaki of Japan
Originated In
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Source MBB/Kawasaki BK 117 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
jointly developed and manufactured by Messerschmitt-Bölkow-Blohm (MBB) of West Germany and Kawasaki of Japan
Also in Geography Atlas: where this subject originated.
Source MBB/Kawasaki BK 117 (Wikipedia)Lead, manufacturerQuote, Lead, manufacturer
jointly developed and manufactured by Messerschmitt-Bölkow-Blohm (MBB) of West Germany and Kawasaki of Japan
Sources
1. MBB/Kawasaki BK 117 (Wikipedia)
Further development
During 1983, the initial production version, designated as the BK 117A-1 was first delivered.
Lead
The MBB/Kawasaki BK 117 is a twin-engined light utility-transport helicopter
Design
Early versions of the BK 117 were powered by a pair of Lycoming LTS101 turboshaft engines
Further development, units built
In total, 443 BK 117s were manufactured by the two partners
Specifications (BK 117 B-2)
Empty weight: 1,727 kg (3,807 lb)
Specifications (BK 117 B-2), maximum mass
Max takeoff weight: 3,350 kg (7,385 lb)
Specifications (BK 117 B-2), top speed
Maximum speed: 250 km/h (160 mph, 130 kn) at sea level
Further development, status
this improved version of the rotorcraft has succeeded and eventually replaced the original BK 117 in production
Lead, manufacturer
jointly developed and manufactured by Messerschmitt-Bölkow-Blohm (MBB) of West Germany and Kawasaki of Japan
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