The evaluation of the P-HEMT technology PH25 according to the European Spac
e Agency requirements is presented. The reliability assessment plan feature
s high temperature storage tests, DC life-tests and RF life-tests, performe
d on a set of evaluation test vehicles specifically defined for this purpos
e. The results of these tests evidence a temperature activated wear-out mec
hanism, a very low sensitivity of PH25 on strong RF stress and no sensitivi
ty on hydrogen. Failure rates calculations are in line with the space progr
amme requirements. (C) 1999 Elsevier Science Ltd. All rights reserved.