
(Duration of 2 days) LEOP consists of initial acquisition of the COMBINE spacecraft and initial check-out of the power and thermal system as well as some fundamental GNC functions including the momentum management function.
Success criteria for PRISMA LEOP:
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Ground has up to date orbit information, preferably from onboard GPS measurements, to predict passages of the spacecraft over Kiruna, and is able to establish two way communication on each pass.
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The spacecraft has deployed both its solar array panels and ground has verified this.
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The spacecraft has nominal power to all units that are at this stage activated.
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Thermally the spacecraft has stable temperatures that are within expected limits.
- The spacecraft is stably sun pointing with the –Y axis, and revolving at 1 revolution per hour and has removed the momentum induced by launch vehicle separation.
- The spacecraft is in its nominal branch configuration and is able to autonomously stay in that configuration and is not rebooting its core board.
- The spacecraft is using its resources within the expected limits.
Read reports here below