|Width (with rotors)||?|
|Rotor (disk) load||25.7|
|Power load (kg/hp)||3.5|
Instead of tube frame supporting the engine-rotor blocks, a straight wing was installed. In flight it provided 25% of a lift force, unloading main rotors.
Helicopter was flown, but tests were not completed. The reason was that there were no serious plans to use experimental aircraft (as helicopters were at the time) for passenger traffic.
|Modified March 28, 1997||Back to|