Development of the Microlift Glider

Authors

  • Piero Morelli OSTIV Sailplane Development Panel

Keywords:

Meteorology, Aerodynamics, Design

Abstract

According to the FAI Sporting Code, a microlift glider has a maximum takeoff mass not exceeding 220 kg and a maximum wing loading not exceeding 18 kg/m2.  These gliders are intended for utilizing weak atmospheric lift conditions, hardly usable for conventional sailplanes.  This paper presents the development, use and future of these aricraft.

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Issue

Vol. 30 No. 1-2 (2006)

Section

Articles

License

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This paper is UNCLASSIFIED (for public reasons) and has been cleared by the appropriate agencies, company and government. This paper represents original work by the author(s). No portion of the material is covered by a prior copyright; or for any portion copyrighted, the author has obtained permission for its use.
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