Moon & Mars Orbiting Spinning Tether Transport - Tethers Unlimited

More documents

Recommendations

Info

Cislunar Tether Transport System• Developed Orbital Architecture for Round Trip LEO⇔LunarSurface Transport• Whole System Launch Mass = 30x Payload Mass– LEO Tether Boost Facility Mass = 13x Payload Mass, Lunar Tether Facility = 17x Payload• 13 Payloads/Year• Incremental Commercial Development PathTUI/MMOSTT 6
Rapid Earth-Mars Transport• Reusable Architecture for Round Trip Earth to Mars Transport• Rapid Transfer Times (90-130 days)INTERPLANETARY TRANSPORT USINGROTATING TETHERSEarth’s gravitationalsphere of influencePayload pick-upTapered tetherLoaded TetherCenter of massorbitPatch pointSolPatch pointMars’ gravitationalsphere of influenceLoaded TetherCenter of massorbitPayload releaseOriginEscapetrajectoryInterplanetarytrajectoryPayload releaseDestinationInboundtrajectoryTapered tetherPayload captureTUI/MMOSTT 7
Page 2 and 3: Tethers Unlimited, Inc.MMOSTT Final
Page 24 and 25: NIAC Funded Tether Research• Moon
Page 26 and 27: Electrodynamic Reboost• Power sup
Page 30 and 31: MXER Tethers Included in NASA’sII
Page 32 and 33: 5mt Payload Tether Boost Facilityfo
Page 34 and 35: LEOGTO Boost Facility• Initial Fa
Page 36 and 37: Tether Boost FacilityControl Statio
Page 38 and 39: LEOGTO Boost Facility• TetherSim
Page 40 and 41: Rendezvous• Rapid AR&C Capability
Page 42 and 43: Proposed RETRIEVE TetherExperiment
Page 44 and 45: µTORQUE on Delta IV• Delta-IV Se
Page 46 and 47: Opportunities for NASATechnology De
Page 48 and 49: AIAA 2000-3842COMMERCIAL DEVELOPMEN
Page 50 and 51: --Commercial Tether Transport AIAA
Page 52 and 53: -Commercial Tether Transport AIAA 2
Page 54 and 55: Commercial Tether Transport AIAA 20
Page 56 and 57: Commercial Tether Transport AIAA 20
Page 58 and 59: Momentum Exchange/Electrodynamic Re
Page 60 and 61: DESIGN AND SIMULATION OF A TETHER B
Page 62 and 63: Tether Boost Facility Design AIAA 2
Page 70 and 71: Tethers Unlimited, Inc.Cislunar Tet
Page 78 and 79:
Tethers Unlimited, Inc.Cislunar Tet
Page 80 and 81:
Tethers Unlimited, Inc.Cislunar Tet
Page 82 and 83:
Interim Report Outline- Configurati
Page 84 and 85:
Mission Definition¥ Payload Capaci
Page 86 and 87:
Baseline Control Station DetailsTET
Page 88 and 89:
Baseline Grapple AssemblyCAPTURES A
Page 90 and 91:
LEO Facility System ArchitectureGRA
Page 92 and 93:
Payload Adapter Assembly Subsystems
Page 94 and 95:
Potential Reeling FunctionsReeling
Page 96 and 97:
LEO Control Station Weights16
Page 98 and 99:
Payload Adapter Assembly Weights18
Page 100 and 101:
Tether Boost FacilityRequired Power
Page 102 and 103:
Electrical Propulsion Voltage´ Spe
Page 104 and 105:
Potential Reeling FunctionsReeling
Page 106 and 107:
Preliminary Reeling AnalysisθθAss
Page 108 and 109:
Tether Boost FacilitySystem Require
Page 110 and 111:
Table of Contents1 Scope ..........
Page 112 and 113:
2 ReferencesThis section lists docu
Page 114 and 115:
The system shall measure and contro
Page 116 and 117:
4 Ground Rules & AssumptionsThis se
Page 118 and 119:
Appendix F: Tether Boost Facility D
Page 120 and 121:
Appendix F Tether Boost Facility De
Page 122 and 123:
Appendix F Tether Boost Facility De
Page 124 and 125:
Page 126 and 127:
Page 128 and 129:
Page 130 and 131:
Page 132 and 133:
Page 134 and 135:
Page 136 and 137:
Page 138 and 139:
Page 140 and 141:
Page 142 and 143:
Appendix L: Tether Boost Facility D
Page 144 and 145:
Page 146 and 147:
Page 148 and 149:
Page 150 and 151:
Page 152 and 153:
Page 154 and 155:
Page 156 and 157:
Page 158 and 159:
Page 160 and 161:
Page 162 and 163:
Page 164 and 165:
Page 166 and 167:
Page 168 and 169:
Page 170 and 171:
Page 172 and 173:
Page 174 and 175:
Page 176 and 177:
Page 178 and 179:
Page 180 and 181:
Page 182 and 183:
Page 184 and 185:
Page 186 and 187:
Page 188 and 189:
Page 190 and 191:
Page 192 and 193:
Page 194 and 195:
Tethers Unlimited, Inc.Tether Rende
Page 196 and 197:
Page 198 and 199:
Page 200 and 201:
Page 202 and 203:
Page 204 and 205:
Page 206 and 207:
Ongoing Tether Work Under NIAC Fund
Page 208 and 209:
Cislunar Tether Transport System•
Page 210 and 211:
Rapid Earth-Mars Transport• Reusa
Page 212 and 213:
EarthMars Launch Windows• MMOSTT
Page 214 and 215:
Incremental Development Path1. TORQ
Page 216 and 217:
LEOGTO Boost Facility• TetherSim
Page 218 and 219:
Tether Boost FacilityControl Statio
Page 220 and 221:
Modular Design• Design Components
Page 222 and 223:
Payload Accommodation AssemblyConfi
Page 224 and 225:
Electrodynamic Thrusting• Drive c
Page 226 and 227:
Tether Facility Reboost• Use Elec
Page 228 and 229:
Rendezvous• Rapid Automated Rende
Page 230 and 231:
Rendezvous Method: Preparation• P
Page 232 and 233:
Development Issues• Automated Ren
Page 234 and 235:
Potential Flight Experiments• Hig
Page 236 and 237:
Opportunities for NASATechnology De
Page 238 and 239:
Acknowledgements• Boeing/RSS - Jo
Page 240 and 241:
IAF-99-A.5.10RAPID INTERPLANETARY T
Page 242 and 243:
Rapid Interplanetary Tether Transpo
Page 244 and 245:
Page 246 and 247:
Page 248 and 249:
Page 250 and 251:
Page 252 and 253:
Page 254 and 255:
Page 256 and 257:
Page 258 and 259:
Page 260 and 261:
Page 262 and 263:
Page 264 and 265:
Page 266 and 267:
Page 268 and 269:
Page 270 and 271:
Page 272 and 273:
IAF-00-S.6.04TETHER SYSTEMS FOR SAT
Page 274 and 275:
IAF-00-S.6.04controlled very precis
Page 276 and 277:
IAF-00-S.6.04Perigee Altitude (km)3
Page 278 and 279:
IAF-00-S.6.04The LEO⇒GTO Tether B
Page 280 and 281:
IAF-00-S.6.04AcknowledgmentsThis re
Page 282 and 283:
Tethers Unlimited, Inc.Appendix K:
Page 284 and 285:
Page 286 and 287:
Tethers Unlimited, Inc.at a rate of
Page 288 and 289:
Page 290 and 291:
Tethers Unlimited, Inc.Appendix L -
Page 292 and 293:
Page 294 and 295:
Page 296 and 297:
Tethers Unlimited, Inc.Appendixm M:
Page 298 and 299:
Page 300 and 301:
Page 302 and 303:
Appendix N. MXER Tether for Deployi
Page 304 and 305:
Page 306 and 307:
Page 308 and 309:
Electrodynamic Thrustingto Reboost
Page 310 and 311:
100000 95000 90000 85000 80000 7500
Page 312 and 313:
Momentum Exchange/Electrodynamic Re
Page 314 and 315:
NOMENCLATURESymbol MeaningA payload
Page 316 and 317:
DepartureangleA = 1.5π - (ω + u
Page 318 and 319:
Tether material has a "characterist
Page 320 and 321:
Rendezvous of Grapple with PayloadT
Page 322 and 323:
adius vector to the new center of m
Page 324 and 325:
days from payload pickup at one pla
Page 326 and 327:
"JupiterandBeyond"Tether cut CUT:<
Page 328 and 329:
Tethers Unlimited, Inc.Appendix Q:
Page 330 and 331:
Tethers Unlimited, Inc.Appendix R:
Page 332 and 333:
Page 334 and 335:
Page 336:
show all

Moon & Mars Orbiting Spinning Tether Transport - Tethers Unlimited

Create successful ePaper yourself

Delete template?

Save as template?