general information

The mission profile, or life profile, is an important step to consider when using the reliability.space method.

For space applications, mission profiles are based on the same main phases. Furthermore, the stress applied on electronic equipment of satellites is mainly linked to the temperature, in addition to the electrical stresses dealt with directly at part level. From the regular mission profile definitions from FIDES, the other stresses such as vibrations, humidity and chemical pollution are considered, but they are mainly present only during the launch phase.

So, to define accurately the mission profile, it is necessary to know:
  • the type of mission of the satellite such as geostationary, Low Earth orbit, middle orbit, science satellite or other mission;
  • the different phases of use (on) and no use (off) of the equipment;
  • the location of the equipment on the platform or on the payload in order to estimate all the relevant stresses.
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time information

temperature information

mechanical information

chemical information

SUM UP
Phase Type Phase Name Unit Onboard Calendar Time
(h)
Ambient Temperature
(°)
ΔT
(°)
Cycle duration
(h)
Number of cycles Max Temperature
(°)
Humidity Rate
(%)
Random Vibrations
(Grms)
Saline Pollution Environment Pollution Application Pollution Protection Level