Phase II Final Report - NASA's Institute for Advanced Concepts

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Planetary Exploration Using Biomimetics An Entomopter for Flight on Mars 25 Wing Length 0.8 m Flapping Frequency (Hz) 20 15 10 35° 45° 55° 65° 75° 85° 5 0 100 1000 10000 100000 Power Consumption (W) Figure B-7: Flapping Frequency vs. Power Consumption (Watts) for a Wing Length of 0.8 m 20 18 Wing Length 0.9 m Flapping Frequency (Hz) 16 14 12 10 8 6 35° 45° 55° 65° 75° 85° 4 2 0 100 1000 10000 100000 Power Consumption (W) Figure B-8: Flapping Frequency vs. Power Consumption (Watts) for a Wing Length of 0.9 m B-4 Phase II Final Report
Appendix B: Sizing Results 16 Wing Length 1.0 m 14 Flapping Frequency (Hz) 12 10 8 6 4 35° 45° 55° 65° 75° 85° 2 0 100 1000 10000 100000 Power Consumption (W) Figure B-9: Flapping Frequency vs. Power Consumption (Watts) for a Wing Length of 1.0 m 100000 Length 0.3 m, RLC 0.5 kg 10000 Power (W) 1000 35° 45° 55° 65° 75° 85° 100 10 0 2 4 6 8 10 12 14 16 18 Velocity (m/s) Figure B-10: Flight Power vs. Velocity for a Wing Length of 0.3 m and Relative Lift Capacity of 0.5 kg B-5
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Planetary Exploration Using Biomime
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Table of Contents Table of Contents
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List of Tables List of Tables Table
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List of Figures List of Figures Fig
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List of Figures Figure 3-54: Pressu
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List of Figures Figure 3-138: Stere
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List of Figures Figure 4-24: Averag
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List of Contributors List of Contri
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Executive Summary Executive Summary
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Chapter 1.0 Introduction Chapter 1.
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Chapter 1.0 Introduction Figure 1-2
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Chapter 1.0 Introduction 1.1 Histor
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Chapter 1.0 Introduction 1.2 Origin
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Chapter 1.0 Introduction 1.3 Missio
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1.3.3.1 Surface Imaging The Entomop
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Chapter 2.0 Entomopter Configuratio
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Chapter 3.0 Vehicle Design 3.1 Wing
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3. Density: 1.40E-2 kg/m 3 4. Press
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Chapter 3.0 Vehicle Design 3.4 Reci
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Chapter 3.0 Vehicle Design 3.5 Fuel
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Chapter 4.0 Entomopter Flight Opera
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Phase II Final Report - NASA's Institute for Advanced Concepts

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