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DIN EN 16603-31-02

Space engineering - Two-phase heat transport equipment; English version EN 16603-31-02:2018

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Organization: DIN
Publication Date: 1 November 2018
Status: active
Page Count: 61
ICS Code (Space systems and operations): 49.140
scope:

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 than 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-EST- 32-02 applicable to TPHTE qualification and acceptance.

This standard may be tailored for the specific characteristics and constraints of a space project in conformance with ECSS-S-ST-00.

Document History

DIN EN 16603-31-02
November 1, 2018
Space engineering - Two-phase heat transport equipment; English version EN 16603-31-02:2018
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...
February 1, 2017
Space engineering - Two-phase heat transport equipment; English version prEN 16603-31-02:2016
A description is not available for this item.
December 1, 2015
Space engineering - Two-phase heat transport equipment; English version EN 16603-31-02:2015
This standard defines requirements for two-phase heat transportation equipment (TPHTE), for use in spacecraft thermal control. This standard is applicable to new hardware qualification activities....
September 1, 2014
Space engineering - Two-phase heat transport equipment; English version FprEN 16603-31-02:2014
A description is not available for this item.

References

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