311  DAY  IN  THE  LIFE:  RISKY  AND  REWARDING  SPACEWALKS—SPACE  SHUTTLE  MISSION  STS-120/ISS-10A  CHAPTER  18  since  the  Columbia  accident  in  2003,  NASA  had  worked  hard  to  develop  a  method  to  repair  the  delicate  heat-  dissipating  tiles  that  protected  the  orbiter  during  reentry  into  the  Earth’s  atmosphere.  (This  was  in  addition  to  wing  leading  edge  repairs,  which  required  different  materials.)  The  tile  repair  material  was  a  consistency  somewhere  between  peanut  butter  and  toothpaste.  The  crew  would  apply  the  repair  material  to  damaged  tiles,  and  the  material  would  harden  to  the  firmness  of  a  pencil  eraser  and  insulate  (via  specifically  formulated  properties)  the  orbiter  during  its  super-heated  reentry.  This  material  was  squirted  out  of  a  container  called  the  Tile  Repair  Ablator  Dispenser  (T-RAD).  The  new  EVA  was  labeled  the  T-RAD  Detailed  Test  Objective.  Most  EVAs  are  planned,  preflight,  over  the  course  of  months  or  even  years  however,  the  operations  team  was  asked  to  quickly  finalize  a  tile  repair  test  procedure  because  of  the  criticality  of  the  test  and  the  familiarity  of  the  team  and  crew  with  the  tile  repair  testing.  A  debris  strike  had  damaged  a  tile  during  the  STS-118/ISS-13A.1  mission  that  flew  in  August  2007.  The  level  of  speculation  about  tile  repair  capability  prompted  Space  Shuttle  Program  management  to  conduct  an  official  test  as  soon  as  possible.  The  team  was  able  to  develop  this  EVA  within  a  few  short  weeks  using  some  already-developed  techniques  that  were  familiar  to  the  crew.  Parazynski  happened  to  be  on  the  EVA  Thermal  Protection  System  repair  collaborative  team,  as  was  the  STS-  120  lead  EVA  officer  Dina  Contella.  Putting  the  experiment  on  this  flight  with  quick  turnaround  was  acceptable  for  the  STS-120  operations  team  in  terms  of  the  limited  training  required.  In  fact,  it  seemed  serendipitous  that  the  team  that  worked  so  hard  on  creating  this  capability  would  get  to  execute  the  on-orbit  test.  The  team  agreed  to  insert  the  tile  repair  test  spacewalk  after  P6  installation  (EVA  3)  and  before  the  increment  crew  Node  2  EVA.  As  discussed  in  Chapter  4,  long  missions  with  a  number  of  spacewalks  can  be  very  tiring  to  the  crew.  This  Detailed  Test  Objective  EVA  would  be  shorter  than  usual  (4  hours)  to  better  allow  for  spacewalks  on  back-to-back  days  without  exhausting  the  crew.  When  Discovery  lifted  off  on  October  23,  2007,  the  spacewalks  had  evolved  from  the  original  three  planned  EVAs  to  five  EVAs.  It  was  to  be  the  first  ISS  docked  mission  with  five  planned  EVAs  and  the  first  mission  with  five  different  EVA  crew  members.  Flight  Days  1-3  (Tuesday,  October  23  through  Thursday,  October  25)  Outboard  (rotates)  S3  SARJ  (covered  in  MLI)  Inboard  Figure  5.  S3  SARJ  (circled)  rotates  the  outboard  segments  to  point  the  solar  arrays  at  the  sun.  The  EVA  crew  was  tasked  with  inspecting  this  SARJ  to  determine  the  source  of  increased  motor  current.  STS-120  launched  on  Tuesday,  October  23,  2007.  The  mission  proceeded  with  a  normal  early  mission  timeline,  including  checkout  of  the  spacesuits  on  October  24  (Flight  Day  2).  On  October  25,  the  day  the  shuttle  was  performing  a  rendezvous  with  the  ISS,  the  operations  team  was  approached  about  adding  a  new  EVA  task  to  the  mission  to  have  the  crew  look  at  the  starboard  Solar  Array  Rotary  Joint  (SARJ)  (Figure  5).  This  huge  round  gear  measures  4  m  (13  ft)  in  diameter  and  is  driven  by  a  motor  to  enable  the  solar  arrays  on  the  end  of  the  truss  to  track  the  sun  via  rotation  of  the  entire  end  of  the  truss.  The  engineering  community  had  seen  some  slightly  increased  currents  (~0.1  amp,  with  intermittent  changes  up  to  0.8  amp)  associated  with  the  motor.  Video  indicated  that  the  arrays  
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