“…Reliability models (Electromigration [5,7], Ohmic contact degradation [25,26], Coffin-Manson model [14], Eyring model [6,23,24], Humidity model [8], TDDB [15,16], Hot Carrier Injection [17,18], Hydrogen poisoning [9,[19][20][21], Thermo-mechanical stress [22], NBTI [23], etc…) are generally expressed by a function of stress parameter multiplying the exponential activation energy factor [10]. These expressions may not look much like a multiple-stress model but in fact it is as we have shown in paper presented at the 2013 IEEE Aerospace Conference [4]:…”