Moon & Mars Orbiting Spinning Tether Transport - Tethers Unlimited

More documents

Recommendations

Info

LEOGTO Boost Facility• TetherSim Numerical Simulation (10x real speed)– Tether Dynamics, Orbital MechanicsTUI/MMOSTT 12
LEOGTO Boost FacilitySystem Definition Task• TUI & Boeing have developed System RequirementsDocument for Tether Boost Facility• System Concept Definition– Identify key technologies– Mass and power budgets• Technology Readiness Level EvaluationTUI/MMOSTT 13
Page 2 and 3:
Tethers Unlimited, Inc.MMOSTT Final
Page 4 and 5:
Page 6 and 7:
Page 8 and 9:
Page 10 and 11:
Page 12 and 13:
Page 14 and 15:
Page 16 and 17:
Page 18 and 19:
Page 20 and 21:
Page 22 and 23:
Page 24 and 25:
NIAC Funded Tether Research• Moon
Page 26 and 27:
Electrodynamic Reboost• Power sup
Page 28 and 29:
Cislunar Tether Transport System•
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 64 and 65:
Page 66 and 67:
Page 68 and 69:
Page 70 and 71:
Tethers Unlimited, Inc.Cislunar Tet
Page 72 and 73:
Page 74 and 75:
Page 76 and 77:
Page 78 and 79:
Page 80 and 81:
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: Appendix L: Tether Boost Facility D
Page 194 and 195: Tethers Unlimited, Inc.Tether Rende
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 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 266 and 267:
Rapid Interplanetary Tether Transpo
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

You also want an ePaper? Increase the reach of your titles

Delete template?

Save as template?