APPENDIX 400 robotic arm maneuvers, 239–240 software upgrade, 111 visiting vehicle missions, 239 single-loop configuration, ITCS, 206–207 Single MT or Single LT mode for pumps, 178 Skylab, xiii, 135 sleep time for crew, 24 Smith, Brian T., 243 Smith, Steve, 298 smoke detectors, 345–346 “Snoopy” cap, EMU, 288 software state of charge (SOC) calculations, 162 updates to, 110–116 User Application Software, 105–106 Solar Alpha Rotary Joints (SARJs) Electrical Power System function, 160, 163, 168–169 issue with during STS-120/ISS-10A, 311–312, 313–314 and software upgrades, 111 structure of, 311, 312 vs. Thermal Radiator Rotary Joint (TRRJ), 204 in truss structure, 42 solar array blankets, 163, 164, 316 solar array masts, 163, 164, 170 solar arrays, See also P6 solar arrays P6 4B solar array repair Solar Alpha Rotary Joints (SARJs) in assembly of ISS, xix, xxi, 157, 164–165 battery charging/discharging, 157, 165 deployment of, 164 as electrical power sources, 156–157 location and size, 308 longeron shadowing, 170–171 motion control considerations, 124, 125 parking to accommodate visiting vehicles, 111, 170 power output, 161 power planning for, 162 in primary power system, 159–160, 163–165 retraction problems, 164–165 Sequential Shunt Unit (SSU) operation, 165 and software upgrades, 111 structure of, 164, 315–316 surface-on image of all, 156 thruster impact on, 131–132 and torque compensation, 132 Solar Array Wing (SAW), 163, 164, 169, 315 solar inertial attitude, 192–193 solar radiation pressure impacting motion control, 129 Solid Oxygen Generator “candles,” 335 Solid State Mass Memory Units (SSMMUs), 99 Soviet Union, xiv Soyuz crew vehicle as crew transport, xix, 20–21 docked at ISS, xvi, 235 docking system, 31, 46, 235 as emergency escape vehicle, 348, 349, 350 landing of, 31 Soyuz U and FG rockets, investigating fault with, 210 space-based optical surveillance, debris tracking, 144 Spacecraft Communicator Position (CAPCOM), xxv Space Integrated GPS/Inertial Navigation System (SIGI) receivers, 121, 126 space junk. See orbital debris Space Operations Support Center (SOSC), xxviii Space Shuttle Program. See also making of a mission entries beginning with STS and C&C MDM triple failure, 273 crew contribution to ISS assembly, 309 debris tracking and evaluation, 146 docking system, 39, 41, 46, 235 EMU design vs. ISS, 283, 285 EVA training vs. ISS, 294, 295 flight control vs. ISS, xxvii planned EVA to test repair of orbiter tiles, 310–311 program defined, xiv role in ISS development, xiii–xiv, xv spacewalk role in ISS assembly, 281–282 transport role for ISS, xviii Space Shuttle Program Office, xv Space Station Freedom, xiii, xiv, 43, 44–45, 170–171, 225 Space Station Integration and Promotion Center (SSIPC) (Tsukuba, Japan), xxviii Space Station Remote Manipulator System (SSRMS) (“big arm”), 251–255 in capturing visiting vehicles, 239, 254 challenges of bringing into operational status, 262–264 controlling from Cupola Workstation, 242 Control Moment Gyroscopes (CMGs) in, 120, 132 vs. EVA in planning ISS assembly tasks, 290, 291 grapple fixtures, SSRMS, 254–255, 256, 257 handling of OBSS during solar array repair, 317 ISS assembly role, 68, 252 joints and rotations, 252, 253, 254 location and appearance, 37, 252 in operation, 257 summary of properties, 251 vehicle berthing role, 239–240 working with during EVA, 250, 301–302 Space Surveillance Network (SSN), 143, 145 Space-to-Ground Antenna, 226 Space-to-Ground Subsystem. See Ku-band communication system Space-to-Ground (S/G) voice loops, xxvii, 178, 224 Space Transportation System (STS) designations, xiv, xix. See also entries beginning with STS Space Vision System (SVS), 44 spacewalk in detail (STS-120/ISS-10A), 306–331 flight days 1–3 (launch, rendezvous, motor check of SARJ), 311–312 flight days 4–5 (EVA 1: payload, Node 2), 312–313 flight days 6–7 (small scale distractions and SARJ inspection), 313–314 flight days 8–12 (P6 solar array repair), 314–330 last-minute added spacewalks, 310–311 lessons learned, 330–331 original mission, 307–308 planning, 309–310 Wheelock’s personal perspective, 322–323 Spacewalks Position (EVA), xxvi SpaceX Control Center (MCC-X), xxviii, 246. See also Dragon (SpaceX) cargo vehicle Special Purpose Dexterous Manipulator (SPDM), 43, 255–256 Standard MDMs, 98 Standard mode, ISS, 106 Standby state, MDM, 100 Starboard Thermal Control Radiator, 202, 203 Starboard Thermal Radiator Rotary Joint (TRRJ), 356, 357, 358 Starliner crew vehicle, 246 star mappers on Service Module, 128 state of charge (SOC) software calculations, 162 state vector in orbit determination, 125 Station Power, Articulation, Thermal, and Analysis (SPARTAN), 161, 162, 171, 356, 358 Station Support Computer (SSC), 93 Stover, Scott, 36, 215, 329 Stowage Officers (ISOs), 4 stowage space, managing with racks, 54 Stowage Tracking Position (CIO), xxv Structural Dynamics Measurement System, 42 structures and mechanisms, ISS, 36–59 primary structure, 36–46, 205 secondary structure, 46–59, 141–143, 349 Structures and Mechanisms Position (OSO), xxv STS-2, 251 STS-92/ISS-3A, 39, 135 STS-97/ISS-4A, 198, 252 STS-98/ISS-5A, 40, 45, 54, 107, 135, 198, 252 STS-100/ISS-6A, 47, 252, 259, 262, 271, 273 STS-102/ISS-5A.1, 271 STS-104/ISS-7A, 262, 272 STS-110/ISS-8A, 135, 264, 292, 298 STS-111/ISS-UF-2, 256, 263–264 STS-113/ISS-11A, 228 STS-114/ISS-LF-1, 78, 135, 274 STS-115/ISS-12A, 203 STS-118/ISS-13A.1, 120, 286, 311 STS-119/ISS-15A, 156 STS-120/ISS-10A, 164, 271, 301. See also spacewalk in detail STS-121/ISS-ULF1.1, 320–321 STS-122/ISS-1E, 58, 330