EN 14607 Part 1 of Space engineering - Mechanical specifies requirements for the discipline of thermal engineering.This document specifies the requirements for the definition, analysis, design, manufacture, verification and in-service operation of thermal control subsystems of spacecraft and other space products.This document applies to the thermal engineering activities of all spacecraft and space related products for all thermal aspects and temperature levels for space products.For this document, the complete temperature scale is divided into three ranges defined as follows: Cryogenic temperature range, below 120 K; Conventional temperature range, between
EN 14607-1:2004 history
2004EN 14607-1:2004 Space engineering - Mechanical - Part 1: Thermal control