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The $10–12 million jet would be the longest-range single-pilot business aircraft, it would keep the HondaJet configuration, stretched from 42.6 to 57.8 ft (13.0 to 17.6 m), and has a 56.7 ft (17.3 m) wingspan, 16 ft (4.9 m) larger, for a maximum takeoff weight of 17,500 lb (7,900 kg) and a 3,300 ft (1,000 m) takeoff distance, while its ...
Honda Aircraft Company is an aircraft manufacturer headquartered in Greensboro, North Carolina, responsible for the production of the HondaJet family of aircraft. Originally a secret research project within Honda R&D, Honda Aircraft Company was formed as a wholly owned subsidiary of Honda Motor Company in August 2006 under the leadership of HondaJet designer Michimasa Fujino. [2]
The Honda MH02 was an experimental business jet built by Honda, in cooperation with Mississippi State University, to research engine placement and composite construction. The prototype was completed in 1992, making its first flight on 5 March 1993.
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Takeoff safety speed. The speed at which the aircraft may safely climb with one engine inoperative. [7] [8] [9] V 2 min: Minimum takeoff safety speed. [7] [8] [9] V 3: Flap retraction speed. [8] [9] V 4: Steady initial climb speed. The all engines operating take-off climb speed used to the point where acceleration to flap retraction speed is ...
The takeoff decision speed V 1 is the fastest speed at which the pilot must take the first actions to reject the takeoff (e.g. reduce thrust, apply brakes, deploy speed brakes). At speeds below V 1 the aircraft can be brought to a halt before the end of the runway. At V 1 and above, the pilot should continue the takeoff even if an emergency is ...
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For his work at Honda Aircraft, Fujino has received the American Institute of Aeronautics and Astronautics (AIAA) Aircraft Design Award (2012), the SAE International Award, the Clarence L. Kelly Johnson Aerospace and Vehicle Design Award (2014), and the International Council of the Aeronautical Sciences Award for Innovation in Aeronautics.