Space systems. Launch-vehicle-to-spacecraft interfaces1 Scope This International Standard specifies the interfaces between a launch vehicle (LV) and the spacecraft (SC) being launched, to provide LV and SC organizations with the necessary format for presenting the required technical data on existing and future interfaces. Its intended purpose is to minimize costs and reduce the risks from errors resulting from miscommunication. It does not limit the ability of LV or SC organizations to specify unique

The particular cable standard dictates the tests which need to be performed on the relevant cable type

Although some of the terms have wide general usage and may be applicable to many materials and products

and their interfaces

its legal and policy requirements

BS EN 62417 provides a wafer-level test procedure to determine the amount of positive mobile charge in oxide layers in metal-oxide-semiconductor field-effect transistors

BS EN IEC 62923-2 helps you in providing harmonized machine-readable alert identifiers that are used to facilitate the implementation of responsibility transfer

4 Disinfection of storage cisterns and distributing pipes

compatibility and non-interference with other RF systems

Automatic deceleration test

BS EN 16603-10-02 can be applied to different products at different levels from a single equipment to the overall system

This method has been validated for citrinin in red yeast rice and in the formulated food supplements in the range of 2

BS IEC 60183:2015 will be of relevance to: