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

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Planetary Exploration Using Biomimetics An Entomopter for Flight on Mars 100000 Length 0.3 m, RLC 1 kg 10000 Power (W) 1000 35° 45° 55° 65° 75° 85° 100 10 0 5 10 15 20 25 Velocity (m/s) Figure B-11: Flight Power vs. Velocity for a Wing Length of 0.3 m and Relative Lift Capacity of 1.0 kg Length 0.3 m, RLC 1.5 kg 100000 10000 Power (W) 1000 35° 45° 55° 65° 75° 85° 100 10 0 5 10 15 20 25 30 Velocity (m/s) Figure B-12: Flight Power vs. Velocity for a Wing Length of 0.3 m and Relative Lift Capacity of 1.5 kg B-6 Phase II Final Report
Appendix B: Sizing Results Length 0.3 m, RLC 2.0 kg 100000 10000 Power (W) 1000 35° 45° 55° 65° 75° 85° 100 10 0 5 10 15 20 25 30 35 Velocity (m/s) Figure B-13: Flight Power vs. Velocity for a Wing Length of 0.3 m and Relative Lift Capacity of 2.0 kg Length 0.4 m, RLC 0.5 kg 10000 Power (W) 1000 100 35° 45° 55° 65° 75° 85° 10 0 2 4 6 8 10 12 14 16 Velocity (m/s) Figure B-14: Flight Power vs. Velocity for a Wing Length of 0.4 m and Relative Lift Capacity of 0.5 kg B-7
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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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