Space systems. Format for spacecraft launch environment test report1 Scope This International Standard provides a specific format to report the test process and results of spacecraft (SC) qualification to the launch environment. The following types of tests are considered: static load; modal survey; sine vibration; acoustic noise; random vibration; shock; and electromagnetic compatibility (EMC). The definition of test specifications and test requirements are derived from launch vehicle (LV) users manuals as defined

so that direct comparison may be made between the technical performance of different equipment for the DAT cassette system

designed for use in smoke and heat control systems

The object of this report is to enhance the protection of persons from laser radiation and other associated hazards by providing guidance on how to establish safety procedures

within enclosed parts of the wind turbine

The drift of the axis drives

These should be used

These devices can be used in an explosive atmosphere if they also comply with IEC 60079-11

is to be used for testing connectors within the scope of IEC technical committee 48

BS EN 660-1 is not appropriate for comparing the wear resistance of dissimilar materials

1 Test methods

with the recommendation that the score is divided into four categories with a qualitative interpretation for each category

2 Capability