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ⓘ Aeroalcool Quasar




Aeroalcool Quasar
                                     

ⓘ Aeroalcool Quasar

The aircraft was designed by American Frank Porter with assistance from James Waterhouse of the Federal University of São Carlos in Brazil, to comply with the US light-sport aircraft rules. It features a cantilever low-wing, a two seats in side-by-side configuration enclosed cockpit under a forward hinged canopy, tricycle landing gear and a single engine in tractor configuration.

The plane is made of aluminum sheet and has a 9.25 30.3 m wingspan ft. The initial motor used was a Japanese 60 HP 45 kW with a HKS 700E four-stroke power unit, which gives it a cruising speed of 210 km / h 130 km / h while burning only 9 gallons IMP Gal 2.0, 2.4 gallon US per hour of auto fuel.