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

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Planetary Exploration Using Biomimetics An Entomopter for Flight on Mars Coefficient of Lift (CL) 4 3 2 1 0 0 20 40 60 80 100 120 -1 -2 -3 -4 Time Fraction (t) Figure 3-125: Coefficient of Lift Baseline Case1 Case2 Case3 Case4 Case5 Case6 Case7 Case8 Case9 Case10 Case11 Case12 Case13 Case14 Case15 Case16 Case17 Case18 Case19 Case20 Case21 Case22 Case23 Case24 Case25 Case26 Case27 Case28 Coefficient of Moment (Cm) 1.2 1 0.8 0.6 0.4 0.2 0 0 20 40 60 80 100 120 -0.2 -0.4 -0.6 -0.8 -1 Time Fraction (t) Figure 3-126: Coefficient of Moment Baseline Case1 Case2 Case3 Case4 Case5 Case6 Case7 Case8 Case9 Case10 Case11 Case12 Case13 Case14 Case15 Case16 Case17 Case18 Case19 Case20 Case21 Case22 Case23 Case24 Case25 Case26 Case27 Case28 144 Phase II Final Report
Chapter 3.0 Vehicle Design 3.3 Wing Aerodynamics Coefficient of Power(Cp) 6 4 2 0 0 20 40 60 80 100 120 -2 -4 -6 Tiem Fraction(t) Figure 3-127: Coefficient of Power Baseline Case1 Case2 Case3 Case4 Case5 Case6 Case7 Case8 Case9 Case10 Case11 Case12 Case13 Case14 Case15 Case16 Case17 Case18 Case19 Case20 Case21 Case22 Case23 Case24 Case25 Case26 Case27 Case28 Now the results produced above can be used to determine the variability of each response with each variable. Some of the relations determined for C L with variables are as follows: a. Keeping everything the same, and just changing the span of Entomopter, Case 19 and Case 20 of the design-of-experiments array depicts the change shown in Figure 3-128 below: 145
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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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Page 117 and 118: 3. Density: 1.40E-2 kg/m 3 4. Press
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Chapter 3.0 Vehicle Design 3.5 Fuel
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Chapter 3.0 Vehicle Design 3.6 Powe
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Chapter 4.0 Entomopter Flight Opera
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Chapter 5.0 Potential Payload Funct
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Chapter 6.0 Media Exposure 6.1 Intr
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Chapter 6.0 Media Exposure 6.3 Onli
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Chapter 6.0 Media Exposure 6.6 Spec
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Chapter 7.0 Conclusion Chapter 7.0
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Appendix A: Mars Atmosphere Data JP
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Appendix A: Mars Atmosphere Data Ge
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Appendix A: Mars Atmosphere Data Ge
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Appendix A: Mars Atmosphere Data Ma
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Appendix B: Sizing Results Appendix
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Appendix B: Sizing Results 30 Wing
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Appendix B: Sizing Results 16 Wing
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Appendix B: Sizing Results Length 0
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Appendix B: Sizing Results Lenght 0
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Appendix C: List of References Appe
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Appendix C: List of References 41.
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Phase II Final Report - NASA's Institute for Advanced Concepts

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