You signed in with another tab or window. Reload to refresh your session.You signed out in another tab or window. Reload to refresh your session.You switched accounts on another tab or window. Reload to refresh your session.Dismiss alert
Temperature management of the cubesat airframe and avionics implies a requirement to have an ability to monitor temperature during development, testing and possibly flight.
The system controller board appears the likely candidate to add a temperature measurement IC which could monitor RTDs or Theromocouples (Type K or Type E (vacuum)? TBD).
The system controller board has the capacity to react to temperature events.
There is an open SPI connection on the ATMEGA128L on the current design.
kwilsonpdx
changed the title
Add RTD/thermocouple - digitial temperature measurement capability to system controller
Add RTD/thermocouple - digital temperature measurement capability to system controller
Oct 22, 2016
Temperature management of the cubesat airframe and avionics implies a requirement to have an ability to monitor temperature during development, testing and possibly flight.
The system controller board appears the likely candidate to add a temperature measurement IC which could monitor RTDs or Theromocouples (Type K or Type E (vacuum)? TBD).
Here is an example IC for reference:
https://cds.linear.com/docs/en/datasheet/2984fb.pdf
The text was updated successfully, but these errors were encountered: