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With the objective to assess potentially performant hybrid electric architectures, this paper presents an aircraft performance level evaluation, in terms of range and payload, of the synergies between a hybrid electric energy system configuration and a cryogenic fuel system. The selected platform is a Liquid Natural Gas (LNG) Unmanned Aerial Vehicle (UAV) that shows up to 46% range increase and up to 7% gain on payload with a reference hybrid electric aircraft that uses conventional drop-in JP-8 fuel.
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This page is a summary of: Synergistic hybrid-electric liquid natural gas drone: S.H.I.E.L.D, Aircraft Engineering and Aerospace Technology, February 2020, Emerald,
DOI: 10.1108/aeat-10-2019-0211.
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