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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:
Once all categories are filled, you can validate the phase click the button. You can edit a phase by double-clicking it from the sum-up table below. Paste saved answers to load them |
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time information |
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temperature information |
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mechanical information |
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chemical information |
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| 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 | |