Space systems. Spacecraft-to-launch-vehicle interface control document Ingestion-build-71203 low-temperature testing of aviation and

low-temperature testing of aviation and electronic components

BS EN 60079-14:2014 replaces BS EN 60079-14:2008

It also covers the setting of limit (upper and lower) hydrogen supply pressures and limit voltages

Hospitality industry

Some markings are accompanied with a note(s) where appropriate

Space systems. Spacecraft-to-launch-vehicle interface control document Ingestion-build-71203 low-temperature testing of aviation and1 Scope The purpose of this International Standard is to provide spacecraft (SC) and launch vehicle (LV) organizations with the general format for presenting the interface control document (ICD) that verifies and controls the compatibility between SC and LV for a dedicated mission. This International Standard addresses the definition of the mission, the compatibility of the SC with the LV environment, including all mechanical, electrical, radio