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  -Four deployable, non-articulating solar array wings  
  -15 Ahr Battery, 11 CPVs, tenperature & pressure telemmetry  
  -16 Selectable V/T charge control with default setting  
  -Battery sizing based on assumptions of loading and battery efficiency  
  -DOD will not exceed 35% during norminal operations  
  -Power balance calculations use CB + implementation margin estimates  



link to Solar Arrays 


link to Battery 


link to Harness Routing