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The Bagalini Bagaliante (a portmanteau of "Bagalini" and "Glider") is an Italian high-wing, strut-braced, single-seat, pusher configuration, conventional landing gear motor glider that was designed by Marino Bagalini and made available as plans for amateur construction.[1][2]

Bagaliante
Role Motor glider
National origin Italy
Designer Marino Bagalini

Design and development


The Bagaliante is constructed from wood and metal and is of pod-and-boom layout.[1]

The 12.2 m (40.0 ft) span wing employs a Göttingen 535 airfoil at the wing root, transitioning to an NACA 4412 section at the wingtip. The wing uses a semi-tapered planform, tapering outboard of the mid-span point. The specified engine is a 19 kW (25 hp) Rotax 277 two-stroke aircraft engine, mounted aft of the cockpit and driving a pusher propeller mounted above the tail boom. The fixed mainwheels are located beside the fuselage on small sponsons.[1][3]

Even with the small Rotax 277 fitted, the takeoff and landing distance is 46 m (150.9 ft)[1]

The estimated time to build the aircraft from the plans is 700 hours.[1]


Specifications (Bagaliante)


Data from Purdy[1]

General characteristics

Performance


See also



References


  1. Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, page 304. BAI Communications. ISBN 0-9636409-4-1
  2. Pilot Mix (n.d.). "Bagalini Bagaliante". Retrieved 8 September 2011.
  3. Lednicer, David (2010). "The Incomplete Guide to Airfoil Usage". Archived from the original on 19 July 2011. Retrieved 8 September 2011.





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