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

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Planetary Exploration Using Biomimetics An Entomopter for Flight on Mars Figure B-26: Flight Power vs. Velocity for a Wing Length of 0.7 m and Relative Lift Capacity of 0.5 kg ............................................................................................................... B-13 Figure B-27: Flight Power vs. Velocity for a Wing Length of 0.7 m and Relative Lift Capacity of 1.0 kg ............................................................................................................... B-14 Figure B-28: Flight Power vs. Velocity for a Wing Length of 0.7 m and Relative Lift Capacity of 1.5 kg ............................................................................................................... B-14 Figure B-29: Flight Power vs. Velocity for a Wing Length of 0.7 m and Relative Lift Capacity of 2.0 kg ............................................................................................................... B-15 Figure B-30: Flight Power vs. Velocity for a Wing Length of 0.8 m and Relative Lift Capacity of 0.5 kg ............................................................................................................... B-15 Figure B-31: Flight Power vs. Velocity for a Wing Length of 0.8 m and Relative Lift Capacity of 1.0 kg ............................................................................................................... B-16 Figure B-32: Flight Power vs. Velocity for a Wing Length of 0.8 m and Relative Lift Capacity of 1.5 kg ............................................................................................................... B-16 Figure B-33: Flight Power vs. Velocity for a Wing Length of 0.8 m and Relative Lift Capacity of 2.0 kg ............................................................................................................... B-17 Figure B-34: Flight Power vs. Velocity for a Wing Length of 0.9 m and Relative Lift Capacity of 0.5 kg ............................................................................................................... B-17 Figure B-35: Flight Power vs. Velocity for a Wing Length of 0.9 m and Relative Lift Capacity of 1.0 kg ............................................................................................................... B-18 Figure B-36: Flight Power vs. Velocity for a Wing Length of 0.9 m and Relative Lift Capacity of 1.5 kg ............................................................................................................... B-18 Figure B-37: Flight Power vs. Velocity for a Wing Length of 0.9 m and Relative Lift Capacity of 2.0 kg ............................................................................................................... B-19 Figure B-38: Flight Power vs. Velocity for a Wing Length of 1.0 m and Relative Lift Capacity of 0.5 kg ............................................................................................................... B-19 Figure B-39: Flight Power vs. Velocity for a Wing Length of 1.0 m and Relative Lift Capacity of 1.0 kg ............................................................................................................... B-20 Figure B-40: Flight Power vs. Velocity for a Wing Length of 1.0 m and Relative Lift Capacity of 1.5 kg ............................................................................................................... B-20 Figure B-41: Flight Power vs. Velocity for a Wing Length of 1.0 m and Relative Lift Capacity of 2.0 kg ............................................................................................................... B-21 xii Phase II Final Report
List of Contributors List of Contributors Georgia Tech Research Institute Mr. Robert J. Englar Prof. Robert C. Michelson Maj. Messam A. Naqvi Northland Scientific OAI Mr. Anthony Colozza (PI) Ms. Laurie Beringer Ms. Terri Deacey Mr. Franklin Porath Mr. Curtis Smith University of Missouri-Rolla Dr. Raja Banerjee Dr. Kakkattukuzhy Isaac Mr. Pavan Shivaram Independent Consultants Mr. Teryn DalBello Dr. Carol Kory Dr. Thomas Scott Acknowledgements We would like to thank Marc Seibert of NASA John H. Glenn Research Center (GRC) for his contributions to this project, and Rainee N. Simons of NASA GRC for his helpful discussions regarding the LTSA antenna. We would also like to acknowledge Daniel Maas of Maas Digital for his outstanding work on the video animation for this project. xiii
Page 1 and 2: Planetary Exploration Using Biomime
Page 3 and 4: Table of Contents Table of Contents
Page 5 and 6: List of Tables List of Tables Table
Page 7 and 8: List of Figures List of Figures Fig
Page 9 and 10: List of Figures Figure 3-54: Pressu
Page 11 and 12: List of Figures Figure 3-138: Stere
Page 13: List of Figures Figure 4-24: Averag
Page 17 and 18: Executive Summary Executive Summary
Page 19 and 20: Chapter 1.0 Introduction Chapter 1.
Page 21 and 22: Chapter 1.0 Introduction Figure 1-2
Page 23 and 24: Chapter 1.0 Introduction 1.1 Histor
Page 25 and 26: Chapter 1.0 Introduction 1.2 Origin
Page 31 and 32: Chapter 1.0 Introduction 1.3 Missio
Page 35 and 36: 1.3.3.1 Surface Imaging The Entomop
Page 43 and 44: Chapter 2.0 Entomopter Configuratio
Page 59 and 60: Chapter 3.0 Vehicle Design 3.1 Wing
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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 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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