Would the STM32L073RZ be suitable for low earth orbit operational environment
Hi all,
I am considering the STM32L073RZ for a low earth orbit application. Would this MCU be suitable for the following operational environment?
Altitudes of 590 – 630 km.
Temperature environment range is -40°C to +70°C.
Total Ionizing Dose (TID) exposure to 12 krad(Si).
Would this device be susceptible to outgassing in a vacuum environment?
If not suitable then are any alternatives available from ST? I have a strong preference for the ST development environment.
Regards
