  Throughout a typical Earth orbit a satellite is constantly bombarded by
radiation with trapped and solar protons being of particular concern as they
gradually damage the focal plane devices throughout the mission and degrade
their performance. To understand the impact the damage has on CCDs and how it
varies with their thermal history a proton radiation campaign has been carried
out using a CCD280. The CCD is irradiated at 153 K and gradually warmed to 188
K in 5 K increments with Fe55 X-ray, dark current and trap pumping images taken
at 153 K after each anneal step.
  The results show that despite the trap landscape changing throughout the
anneal it has little impact on parallel charge transfer inefficiency. This is
thought to be because most traps are unaffected and a lot of those that do
anneal only move from the continuum between distinct trap species and into a
nearby divacancy trap 'peak' whose emission time constant is similar enough to
still impact the CTI.
  In terms of using a CCD280 or similar devices in a mission the CTI being
unaffected by thermal annealing up to 188 K means that any CTI correction
needed as the radiation damage builds up does not have to take into account the
thermal history of the focal plane. However, it is possible that a significant
amount of annealing will occur at temperatures greater than 188 K and care
should be taken when a mission is operating in this range to gather accurate
pre-flight data.
