1 Scope
This document specifies requirements for the implementation of spacecraft level micro-vibration
tests on space systems to be considered by test providers, including test designers
and test engineers. It also gives guidance for spacecraft designers and interested
parties.
The spacecraft level micro-vibration test is applicable to space systems which contain
payload equipment sensitive to the micro-vibration environment which only induced by the internal disturbance sources on-orbit, e.g. for the purpose
of earth observation, space telescopes, optical experiments, telecommunication.