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

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Planetary Exploration Using Biomimetics An Entomopter for Flight on Mars 60 Wing Length 0.4 m 50 Flapping Frequency (Hz) 40 30 20 35° 45° 55° 65° 75° 85° 10 0 100 1000 10000 100000 Power Consumption (W) Figure B-3: Flapping Frequency vs. Power Consumption (Watts) for a Wing Length of 0.4 m 40 35 Wing Length 0.5 m 30 Flapping Frequency (Hz) 25 20 15 10 35° 45° 55° 65° 75° 85° 5 0 100 1000 10000 100000 Power Consumption (W) Figure B-4: Flapping Frequency vs. Power Consumption (Watts) for a Wing Length of 0.5 m B-2 Phase II Final Report
Appendix B: Sizing Results 30 Wing Length 0.6 m 25 Flapping Frequency (Hz) 20 15 10 35° 45° 55° 65° 75° 85° 5 0 100 1000 10000 100000 Power Consumption (W) Figure B-5: Flapping Frequency vs. Power Consumption (Watts) for a Wing Length of 0.6 m 25 20 35° 45° 55° 65° 75° 85° Wing Length 0.7 m Flapping Frequency (Hz) 15 10 5 0 100 1000 10000 100000 Power Consumption (W) Figure B-6: Flapping Frequency vs. Power Consumption (Watts) for a Wing Length of 0.7 m B-3
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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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