Bagalini Bagaliante

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Bagaliante
Role Motor glider
National origin Italy
Designer Marino Bagalini

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]

Contents

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

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References

  1. 1 2 3 4 5 6 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.