Space projects. Programme management. Dependability assurance requirements Ingestion-build-177197 maximum weight to be tested

maximum weight to be tested when using Method A

— battery chargers and supply units for electronic flash apparatus for photographic purposes (IEC 60491)

for the purposes of demonstrating compliance with aircraft noise certification limits established by relevant national aviation authorities and for the measurement system

BS EN 14730-1:2006+A1:2010

Flooring Contractors

Space projects. Programme management. Dependability assurance requirements Ingestion-build-177197 maximum weight to be tested1 Scope This International Standard presents the requirements for a dependability (reliability, availability and maintainability) assurance programme for space projects. It defines the dependability requirements for space products as well as for system functions implemented in software, and the interaction between hardware and software. The provisions of this International Standard apply to all programme phases.