The purpose of this Standard is to define the Factors Of Safety (FOS), Design Factor and additional factors to be used for the dimensioning and design verification of spaceflight hardware including qualification and acceptance
tests.
This standard is not self standing and is used in conjunction with the ECSS-EST-32, ECSS-E-ST-32-02 and ECSS-E-ST-33-01 documents.All current amendments available at time of purchase are included with the purchase of this document.