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CougsInSpace / CougSat1-Hardware

All hardware comprising CougSat-1 exists here
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ENVIRONMENTAL CONTROL- Establish Component Failure Temperatures #428

Open mvguerrero opened 5 years ago

mvguerrero commented 5 years ago

In order to determine any trouble our current design might run in to in the space environment, we should first know which components are most susceptible to heating and cooling.

mvguerrero commented 5 years ago

A good place to start is this out-gassing document, which provides a list of materials that the satellite may have. https://docs.google.com/spreadsheets/d/1Ffi6Van7d6UFOOZWv35CHvjAYAZviSq5Q2YHk5JZeZU/edit#gid=0

mvguerrero commented 5 years ago

https://docs.google.com/spreadsheets/d/1-Y5DcxFlxzLKLqIWymtka-N0zlOLK5Fd1R_8o3NRlR0/edit?usp=drivesdk

This is the link to the actual spreadsheet! Originally it was done by manufacturer, but the resources page may have changed from then to now. https://github.com/CougsInSpace/Resources/tree/master/SupplierDocuments

mvguerrero commented 5 years ago

Looking through the list of capacitors, they are very similar in component failure temps. The most strict range I found so far was -15 to 80. I am going to move on from those