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PREN 16603-31-02 : DRAFT 2016

Current

Current

The latest, up-to-date edition.

SPACE ENGINEERING - TWO-PHASE HEAT TRANSPORT EQUIPMENT

Published date

14-12-2016

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European Foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 TPHTE verification principles
5 Requirements for qualification activity
6 Requirements for acceptance activity
Annex A (normative) - deleted
Annex B (normative) - deleted
Annex C (normative) - deleted
Annex D (normative) - deleted
Annex E (normative) - deleted
Annex F (normative) - deleted
Annex G (normative) - deleted
Annex H (normative) - deleted
Bibliography

Specifies qualification and acceptance requirements for two-phase heat transportation equipment (TPHTE), for use in spacecraft thermal control.

Committee
TC 5
DocumentType
Draft
PublisherName
Comite Europeen de Normalisation
Status
Current

Standards Relationship
NF EN 16603-31-02 : 2017 Identical
16/30352063 DC : 0 Identical
16/30352063 DC : DRAFT DEC 2016 Identical

EN 9100:2009 Quality Management Systems - Requirements for Aviation, Space and Defense Organizations
EN 16603-32-01:2014 Space engineering - Fracture control
EN 16602-70:2016 Space product assurance - Materials, mechanical parts and processes
EN 16603-31:2014 Space engineering - Thermal control general requirements
EN 16601-00-01:2015 Space systems - Glossary of terms
EN 16603-32:2014 Space engineering - Structural general requirements
EN 16603-10-03:2014 Space engineering - Testing
EN 16603-10-06:2014 Space engineering - Part 10-06: Technical requirements specification
EN 16603-32-02:2014 Space engineering - Structural design and verification of pressurized hardware

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