DIN EN 16603-31-02:2018 Edition

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Space engineering – Two-phase heat transport equipment

Published By	Publication Date	Number of Pages
DIN	2018-11	61

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Categories: 49.140 - Space systems and operations, DIN

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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.

Published Code	DIN
Published By	Deutsches Institut für Normung
Publication Date	2018-11
Pages Count	61
Language	English
Descriptors	Aerospace transport, Commissioning, Control equipment, Definitions, Equipment, Hardware, Heat transfer, Mechanical interfaces, Mechanics, Operation, Outer space, Performance, Performance tests, Properties, Quality assurance, Reliability, Safety, Space safety, Space technology, Space transport, Space vehicles, Spacecraft, Spacecraft instruments, Specification (approval), Surveillance (approval), Temperature, Testing, Thermal, Thermal environment, Thermal stress, Computer hardware
File Size	1.8 MB
ICS Codes	49.140 - Space systems and operations


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DIN EN 16603-31-02:2018 Edition

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