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

More documents

Recommendations

Info

Planetary Exploration Using Biomimetics An Entomopter for Flight on Mars used to power the electronics and other systems, the type and capabilities of the communications system, the type and approach of the navigation and control system, the construction materials used in the vehicle, and the landing and sampling approach. Figure 2-7: Orbital Image of Surface Features on Mars Figure 2-8: Image of Mars Surface from Pathfinder Lander As a basis for the Entomopter design and analysis, a concise summary of the Mars environmental conditions was assembled. Some of the more recent Mars science missions (particularly the Pathfinder mission) have provided detailed information on various aspects of the Mars environment. However, many aspects of that environment are still not well understood, so the information provided in the following tables and figures represents the present state of knowledge. This 32 Phase II Final Report
Chapter 2.0 Entomopter Configuration and Operation 2.4 Environmental Conditions for Flight on Mars information and the influence it has on the Entomopter design may be subject to change as our understanding of the Mars environment increases. 2.4.1 Physical Properties Table 2-1: Physical Properties of Mars Inclination of Equator to Orbit Day Period Solar Radiation Intensity 25.2 o 24 hours, 39 minutes Mean: 590 W/m 2 Parihelion: 718 W/m 2 Apehelion: 493 W/m 2 Gravitational Constant 3.73 m/s 2 Sidereal Year Surface Temperature Extremes 687 days (Mars) 130 o K to 300 o K 2.4.2 Atmospheric Conditions Table 2-2: Mars Atmospheric Composition [243] Gas Percent Volume Carbon Dioxide (CO 2 ) 95.32 Nitrogen (N 2 ) 2.7 Argon (Ar) 1.6 Oxygen (O 2 ) 0.13 Carbon Monoxide (CO) 0.07 Water Vapor (H 2 O) 0.03 Neon (Ne) Krypton (Kr) Xenon (Xe) 2.5 ppm 0.3 ppm 0.08 ppm Mars atmospheric profiles are listed in Appendix A. This appendix consists of four atmospheric profiles generated by different sources and for different locations on Mars. The data available with each profile is not necessarily the same. The first profile is a reference atmosphere supplied by JPL. This data was generated for a latitude of -20°. It provides data on temperature, pressure, viscosity, and density from just above the surface to nearly 10 km [142]. 33
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 and 14: List of Figures Figure 4-24: Averag
Page 15 and 16: List of Contributors List of Contri
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 49: Chapter 2.0 Entomopter Configuratio
Page 59 and 60: Chapter 3.0 Vehicle Design 3.1 Wing
Page 101 and 102:
Chapter 3.0 Vehicle Design 3.3 Wing
Page 103 and 104:
Page 105 and 106:
Page 107 and 108:
Page 109 and 110:
Page 111 and 112:
Page 113 and 114:
Page 115 and 116:
Page 117 and 118:
3. Density: 1.40E-2 kg/m 3 4. Press
Page 119 and 120:
Page 121 and 122:
Page 123 and 124:
Page 125 and 126:
Page 127 and 128:
Page 129 and 130:
Page 131 and 132:
Page 133 and 134:
Page 135 and 136:
Page 137 and 138:
Page 139 and 140:
Page 141 and 142:
Page 143 and 144:
Page 145 and 146:
Page 147 and 148:
Page 149 and 150:
Page 151 and 152:
Page 153 and 154:
Page 155 and 156:
Page 157 and 158:
Page 159 and 160:
Page 161 and 162:
Page 163 and 164:
Page 165 and 166:
Page 167 and 168:
Page 169 and 170:
Page 171 and 172:
Page 173 and 174:
Chapter 3.0 Vehicle Design 3.4 Reci
Page 175 and 176:
Page 177 and 178:
Page 179 and 180:
Page 181 and 182:
Page 183 and 184:
Page 185 and 186:
Page 187 and 188:
Chapter 3.0 Vehicle Design 3.5 Fuel
Page 189 and 190:
Page 191 and 192:
Page 193 and 194:
Page 195 and 196:
Page 197 and 198:
Page 199 and 200:
Page 201 and 202:
Page 203 and 204:
Page 205 and 206:
Page 207 and 208:
Page 209 and 210:
Page 211 and 212:
Page 213 and 214:
Page 215 and 216:
Page 217 and 218:
Page 219 and 220:
Page 221 and 222:
Page 223 and 224:
Page 225 and 226:
Chapter 3.0 Vehicle Design 3.6 Powe
Page 227 and 228:
Page 229 and 230:
Page 231 and 232:
Page 233 and 234:
Page 235 and 236:
Page 237 and 238:
Page 239 and 240:
Page 241 and 242:
Page 243 and 244:
Chapter 4.0 Entomopter Flight Opera
Page 245 and 246:
Page 247 and 248:
Page 249 and 250:
Page 251 and 252:
Page 253 and 254:
Page 255 and 256:
Page 257 and 258:
Page 259 and 260:
Page 261 and 262:
Page 263 and 264:
Page 265 and 266:
Page 267 and 268:
Page 269 and 270:
Page 271 and 272:
Page 273 and 274:
Page 275 and 276:
Page 277 and 278:
Chapter 5.0 Potential Payload Funct
Page 279 and 280:
Page 281 and 282:
Page 283 and 284:
Page 285 and 286:
Chapter 6.0 Media Exposure 6.1 Intr
Page 287 and 288:
Chapter 6.0 Media Exposure 6.3 Onli
Page 289 and 290:
Chapter 6.0 Media Exposure 6.6 Spec
Page 291 and 292:
Chapter 7.0 Conclusion Chapter 7.0
Page 293 and 294:
Appendix A: Mars Atmosphere Data JP
Page 295 and 296:
Appendix A: Mars Atmosphere Data Ge
Page 297 and 298:
Appendix A: Mars Atmosphere Data Ge
Page 299 and 300:
Appendix A: Mars Atmosphere Data Ma
Page 301 and 302:
Page 303 and 304:
Page 305 and 306:
Page 307 and 308:
Appendix B: Sizing Results Appendix
Page 309 and 310:
Appendix B: Sizing Results 30 Wing
Page 311 and 312:
Appendix B: Sizing Results 16 Wing
Page 313 and 314:
Appendix B: Sizing Results Length 0
Page 315 and 316:
Page 317 and 318:
Page 319 and 320:
Appendix B: Sizing Results Lenght 0
Page 321 and 322:
Page 323 and 324:
Page 325 and 326:
Page 327 and 328:
Page 329 and 330:
Appendix C: List of References Appe
Page 331 and 332:
Appendix C: List of References 41.
Page 333 and 334:
Page 335 and 336:
Page 337 and 338:
Page 339 and 340:
Page 341 and 342:
Page 343 and 344:
show all

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

Create successful ePaper yourself

Delete template?

Save as template?