• Source: Paxton man-powered aircraft
  • The Paxton man-powered aircraft was the project of architect Tony Paxton, to create a compact human-powered aircraft, suitable for sports flying.
    It was a low-wing monoplane, but mounted on top of a tall undercarriage 6 ft (1.8 m) off the ground. The airframe was constructed of metal tubing, with extensive use of styrofoam in order to create the wing ribs and fuselage formers. The wings were of constant chord and made use of the thick-sectioned high-lift GU25-5(11)8 aerofoil. The wings were also wire braced, and fitted with tip plates at each wingtip. Control was very similar to that of the Weybridge Dumbo machine; the cruciform tail featured movable control surfaces on both fins and the tailplanes, with lateral control being achieved by rotating each wing, in its entirety, around the spar.
    The pilot sat in the open air, in a reclined position, and powered a 2-bladed pusher propeller via a bevel-geared drive system.
    Initial tests with the aircraft resulted in a failure of the drive system. A later attempt to tow the aircraft aloft ended when the craft tipped over forwards. According to the author Keith Sherwin, subsequent developments to the aircraft proved to be successful, implying that it had flown.


    Specifications


    Data from Man-Powered FlightGeneral characteristics
    Crew: 1
    Wingspan: 51 ft (16 m)
    Wing area: 153 sq ft (14.2 m2)
    Airfoil: GU25-5(11)8
    Empty weight: 85 lb (39 kg)
    Gross weight: 220 lb (100 kg)
    Propellers: 2-bladed
    Performance


    See also



    Aircraft of comparable role, configuration, and era

    HMPAC Puffin
    Malliga 1
    MacCready Gossamer Albatross
    MacCready Gossamer Condor
    Goodhart Newbury Manflier
    Southend MPG Mayfly
    Weybridge Dumbo

    Related lists

    List of Human-powered aircraft


    References

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