Mission Description rev2

0285-EX-CN-2016 Text Documents

California Polytechnic State University

2017-11-29ELS_201753

LEO  Mission  Description         LEO  will  record  vibrational  and  thermal  measurements  with  two  accelerometers   and  a  thermocouple  and  also  record  vibrational  data  taken  by  a  second  CubeSat  that   will  be  transferred  through  WiFi  during  launch.     Upon  deployment  from  the  P-­‐‑POD,  LEO  will  turn  off  its  WiFi  module  and  take   pictures  of  the  StangSat  CubeSat  as  they  separate.  45  minutes  after  deployment  the   antenna  will  be  deployed  and  the  UHF  beacon  will  be  activated.  For  the  first  few   passes  the  ground  station  operators  will  attempt  communications  to  perform   checkouts  of  the  spacecraft.  Data  from  the  requested  EOIs  will  then  be  able  to  be   downlinked.     After  the  data  is  successfully  received  at  the  ground  station,  LEO  will  continue  to   operate  throughout  the  orbital  life  (approx  2.9  years)  as  a  digipeater  for  HAM   operators  who  will  have  access  to  telemetry  data  from  the  LEO  beacons.     The  CubeSat  structure  is  made  of  Aluminum  6061-­‐‑T6.  It  contains  all  standard   commercial  off  the  shelf  (COTS)  materials,  electrical  components,  PCBs  and  solar   cells.    

There  are  no  pressure  vessels,  hazardous  or  exotic  materials.     The  electrical  power  storage  system  consists  of  common  lithium-­‐‑ion  batteries  with   over-­‐‑charge/current  protection  circuitry.    


Document Created: 0270-04-11 00:00:00
Document Modified: 0270-04-11 00:00:00
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