Peculiarity of this new engine : 4-stroke, 4 cylinder horizontally opposed, spark ignition, air-cooled unit with reduction gera; power output greater than 60kW, weight less than 65 kg (ready to fly), high reliability and small overall dimension, due to reduction of components. Experimental tests demonstrate a remarkable weight to power ratio (1,02 kg/kW) comparable with the reference engine Rotax 912 UL-S (0,98 kg/kW).
A SI Engine for Ultra Light Aircraft Propulsion / Grassia, P.; Migliaccio, Mariano. - In: ATA. - ISSN 0001-2661. - STAMPA. - 57:11/12(2004), pp. 1-10.
A SI Engine for Ultra Light Aircraft Propulsion
MIGLIACCIO, MARIANO
2004
Abstract
Peculiarity of this new engine : 4-stroke, 4 cylinder horizontally opposed, spark ignition, air-cooled unit with reduction gera; power output greater than 60kW, weight less than 65 kg (ready to fly), high reliability and small overall dimension, due to reduction of components. Experimental tests demonstrate a remarkable weight to power ratio (1,02 kg/kW) comparable with the reference engine Rotax 912 UL-S (0,98 kg/kW).File in questo prodotto:
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