This Standard applies to all parties involved at all levels in the realization of space segment hardware and its interfaces.
To this end, the following are specified:
- Load ratios or limits to reduce stress applied to components;
- Application rules and recommendations.This standard may be tailored for the specific characteristics and constraints of a space project, in accordance with ECSS-S-ST-00
Md5 checksum .doc file = 08503C9375253CC87ECDD2652854E166
Md5 checksum .pdf file = D9B4FC65C14C549744237457D2591881
This Standard cancels and replaces ECSS-Q-ST-30-11C(31 July 2008).
This standard is supported by ECSS Technical Memorandum: ECSS-Q-TM-30-12A – End-of-life parameters – EEE components (12 October 2010).