This standard defines qualification and acceptance requirements for two-phase heat transportation equipment (TPHTE), for use in spacecraft thermal control. This standard is applicable to qualification and acceptance activities of new hardware. However, acceptance requirements of this Standard can be used for existing hardware, which has been qualified previously to other requirements then listed herein. Requirements for mechanical pump driven loops (MPDL) are not included in the present version of this Standard. This standard also includes definitions and part of the requirements of ECSS-E-ST-32-02 applicable to TPHTE qualification. This standard may be tailored for the specific characteristics and constrains of a space project in conformance with ECSS-S-ST-00.
DIN EN 16603-31-02:2018 Referenced Document
EN 9100:2009 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
DIN EN 16603-31-02:2018 history
2018DIN EN 16603-31-02:2018-11 Space engineering - Two-phase heat transport equipment; English version EN 16603-31-02:2018
2018DIN EN 16603-31-02:2018 Space engineering - Two-phase heat transport equipment; English version EN 16603-31-02:2018
2015DIN EN 16603-31-02:2015 Space engineering - Two-phase heat transport equipment; English version EN 16603-31-02:2015