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Promising Electric Aircraft Drive Systems - page 13 / 23

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Comparing Electric Aircraft Power-systems

  • Power-systems are normalized by maximum power and total available energy

  • System weight is used as a figure of merit

  • Two reference mission used as a basis for comparison

    • Light Utility General Aviation (GA)

      • >

        3525 lb GTOW

      • >

        170 Knts

      • >

        300 HP

      • >

        4.75 hr endurance

    • Light Primary Trainer

      • >

        1100 lb GTOW

      • >

        85 Knts

      • >

        67 HP

      • >

        1.5 hr endurance

  • Electric aircraft synergistic advantages not considered EAA Electric Aircraft World Symposium 2010: Michael Dudley

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