Question: 1: Basic Sizing (Reference Aircraft & Final Aircraft Design) Determine design take-off weight and basic weight breakdown (empty, fuel, payload). Construct basic payload-range analysis. Determine

1: Basic Sizing (Reference Aircraft & Final Aircraft Design) Determine design take-off weight and basic weight breakdown (empty, fuel, payload). Construct basic payload-range

1: Basic Sizing (Reference Aircraft & Final Aircraft Design) Determine design take-off weight and basic weight breakdown (empty, fuel, payload). Construct basic payload-range analysis. Determine Thrust to Weight ratio and Wing Loading from a constraints analysis. Determine wing area and select engine power requirements. C AR e CDO TODA LDA CLTO CLL alcr MCR TSFCCR Pyldmax PaxTyp RangeTyp 10.2 0.825 0.017 2100m 1500m 1.8 2.1 0.26 0.84 0.515/hr 35,000kg 200 4500nm 1: Basic Sizing (Reference Aircraft & Final Aircraft Design) Determine design take-off weight and basic weight breakdown (empty, fuel, payload). Construct basic payload-range analysis. Determine Thrust to Weight ratio and Wing Loading from a constraints analysis. Determine wing area and select engine power requirements. C AR e CDO TODA LDA CLTO CLL alcr MCR TSFCCR Pyldmax PaxTyp RangeTyp 10.2 0.825 0.017 2100m 1500m 1.8 2.1 0.26 0.84 0.515/hr 35,000kg 200 4500nm

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