CHAPTER  3  SYSTEMS:  STRUCTURE  AND  MECHANISMS—THE  INTERNATIONAL  SPACE  STATION’S  SKELETON  52  and  some  electrically  controlled—  serve  to  reduce  the  exposure  of  the  outer  window  pane  to  contamination  from  jet  firings  or  material  off-  gassing,  provide  debris  shielding  for  that  outer  pane,  and  block  sunlight  from  entering  the  ISS  cabin.  How  big  are  the  windows?  Size  (diameter)  of  common  ISS  windows:  n  US  hatch:  20.3  cm  (8  in.)  n  US  Laboratory:  51  cm  (20  in.)  n  JEM  (two):  51  cm  (20  in.)  n  Cupola  center:  70.6  cm  (27.8  in.)  n  Cupola  trapezoidal  (six):  0.22  m  area  (322  in2)  n  Service  Module  Window  #9:  48.3  cm  (19  in.)  None  of  the  windows  on  the  ISS  are  composed  of  a  single  pane  of  glass,  nor  is  each  pane  as  thin  as  one  found  in  a  home  window.  Rather,  two  panes  of  relatively  thick  glass  maintain  the  pressure  integrity  of  the  module  and,  typically,  there  are  additional  thinner  protective  panes  on  the  inside  and  outside  of  the  window.  That  makes  for  a  total  of  four  panes.  The  inner  protective  pane  (called  the  “scratch  pane,”  as  it  is  intended  to  prevent  the  crews  from  inadvertently  scratching  the  glass  pressure  pane)  can  be  removed  if  necessary.  A  vacuum  is  drawn  on  the  inter-pane  space  to  prevent  condensation  from  forming  between  the  two  panes  of  window  glass.  That  is  the  purpose  of  the  flex  hose  that  Mike  Foale  is  inspecting  in  Figure  19.  That  flex  hose  also  proved  to  be  an  inviting  hand  hold  for  early  ISS  crew  members  over  time,  this  resulted  in  the  development  of  a  small  leak  in  that  hose.  A  protective  box  has  now  been  installed  over  these  flex  hoses  to  ensure  they  do  not  get  bumped  and  start  leaking,  as  shown  in  Figure  20.  Figure  19.  Expedition  8  Commander  Mike  Foale  using  the  Ultrasonic  Leak  Detector  in  2004  to  pinpoint  a  small  leak  that  had  developed  in  one  of  the  seals  of  the  hose  used  to  maintain  a  vacuum  between  the  panes  of  glass  within  the  large  window  of  the  US  Laboratory.  Once  the  leak  point  was  identified,  the  hose  was  disconnected  (which  stopped  the  leak  to  space)  until  a  replacement  hose  could  be  flown  to  the  space  station.  Figure  20.  The  US  Laboratory  window  with  its  shutter  closed  (noted  by  white  cover  visible  through  the  window)  and  protective  box  covering  its  vacuum  flex  hose.  Clockwise  from  the  box  is  the  handwheel  crews  use  to  open  and  close  the  shutter.  
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