A Weight Prediction Model for Electric Propulsion System applied on Light Helicopters (CS.27)

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dc.contributor.authorMauri, F.L.C.
dc.contributor.authorMerlo, F.
dc.contributor.authorTramontana, G.
dc.date.accessioned2026-08-11T11:54:37Z
dc.date.issued2023
dc.description.abstractAim of this work is to present a possible high-level conceptual method of weight prediction to manage config-urations where an electric propulsion system is able to support the thermal engine failure to guarantee a com-plete safe landing and not only an emergency one like autorotation. Boundary conditions for this analysis are a starting failure event at an altitude of 6000ft associate with a descending/landing time of 6’ ca.
dc.identifier.urihttps://hdl.handle.net/20.500.11881/4513
dc.language.isoen
dc.subject.otherAircraft Design
dc.titleA Weight Prediction Model for Electric Propulsion System applied on Light Helicopters (CS.27)

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