A technical summary and compilation of characteristics and specifications on steep-gradient aircraft
Power is provided by one 825 shaft horsepower Lycoming YT- 53-L-l shaft turbine engine mounted in the fuselage. ... The Aerocycle is powered by a 40 hp Kiekhaefer Mercury Mark 55 two-stroke outboard motor which drives the rotors by anbsp;...
| Title | : | A technical summary and compilation of characteristics and specifications on steep-gradient aircraft |
| Author | : | United States. Federal Aviation Agency |
| Publisher | : | - 1961 |
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