Figure 10.4.1 Erection of the First 5m Segment......................................................................... 357 Figure 10.4.2 First 5 Segments from the Shuttle Cargo Bay...................................................... 357 Figure 10.4.3 The Dual-keel Space Station.................................................................................359 Figure 10.4.4 Erection of the Mars Mission Vehicle Assembly Bay......................................... 359 Figure 10.4.5 Outline of Launch and Assembly Sequence......................................................... 360 Figure 10.4.6 Angular Convention............................................................................................. 361 Figure 10.4.7 Sun Power Vs. Angular Position.......................................................................... 362 Figure 10.4.8 Drag Compensation Velocity Increment Requirements....................................... 365 Figure 10.4.9 Basic Orbit Transfer Options................................................................................ 367 Figure 10.4.10 Hybrid Orbit Transfer......................................................................................... 368 Figure 10.4.11 1 MW Planar Array Demonstrator.......................................................................373 Figure 10.4.12 1 MW Pre-commercial Demonstrator................................................................ 375 Figure 10.4.13 Large Planar Array............................................................................................. 377 Figure 10.4.14 1 MW Prototype Task Schedule......................................................................... 378 Figure 10.4.15 1 MW Prototype Timeline.................................................................................. 378 Figure 10.4.16 Phase C/D Task Schedule...................................................................................379 Figure 10.4.17 Phase C/D Timeline............................................................................................ 379 Figure 11.1 Sensitivity Analysis Curve of Spacecraft, Transportation and Ground Segments.. 392 Figure 11.2 Conversion and Power Transmission Systems Costs in Spacecraft Segment........ 394 Figure 11.3 Sensitivity Analysis of HLLV Costs in Transportation Segment............................395 Figure 11.4 Rectenna Structure and Power Collection on Ground Receiving Station Segment. 396 Figure 11.5 Staged Plan for ISPO Financing.............................................................................. 405 Figure 11.6 Viability of Space to Earth Solar Power Satellite Operation....................................412 Figure 11.7 Revenues and Costs for 120 5GW SPS Operation................................................. 413 Figure 11.8 Revenues and Costs, including 3% Capital Cost, for 120 5 GW SPS Operation.... 414
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