
EN 16603-31-02:2015
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

Space engineering - Two-phase heat transport equipment
22-04-2022
23-09-2015
European foreword
Introduction
1 Scope
2 Normative references
3 Terms, definitions and abbreviated terms
4 TPHTE qualification principles
5 Requirements
Annex A (normative) - Technical requirements specification
(TS) - DRD
Annex B (normative) - Verification plan (VP) - DRD
Annex C (normative) - Review-of-design report (RRPT) - DRD
Annex D (normative) - Inspection report (IRPT) - DRD
Annex E (normative) - Test specification (TSPE) - DRD
Annex F (normative) - Test procedure (TPRO) - DRD
Annex G (normative) - Test report (TRPT) - DRD
Annex H (normative) - Verification report (VRPT) - DRD
Bibliography
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.Requirements for mechanical pump driven loops (MPDL) are not included in the present version of this Standard.This standard includes definitions, requirements and DRDs from ECSS-E-ST-10-02, ECSS-E-ST-10-03, and ECSS-E-ST-10-06 applicable to TPHTE qualification. Therefore, these three standards are not applicable to the qualification of TPHTE.This standard also includes definitions and part of the requirements of ECSS-E-ST-32-02 applicable to TPHTE qualification.ECSS-E-ST-32-02 is therefore applicable to the qualification of TPHTE.This standard does not include requirements for acceptance of TPHTE.This standard may be tailored for the specific characteristic and constrains of a space project in conformance with ECSS-S-ST-00.
Committee |
CEN/CLC/JTC 5
|
DocumentType |
Standard
|
PublisherName |
Comite Europeen de Normalisation
|
Status |
Superseded
|
Standards | Relationship |
PN EN 16603-31-02 : 2015 | Identical |
BS EN 16603-31-02:2015 | Identical |
NBN EN 16603-31-02 : 2015 | Identical |
BS EN 16603-31-02:2018 | Identical |
NF EN 16603-31-02 : 2017 | Identical |
I.S. EN 16603-31-02:2015 | Identical |
SN EN 16603-31-02 : 2015 | Identical |
CEI UNI EN 16603-31-02 : 1ED 2016 | Identical |
NS EN 16603-31-02 : 2015 | Identical |
PN EN 16603-31-02:2018 | Identical |
NEN-EN 16603-31-02:2018 en | Identical |
I.S. EN 16603-31-02:2018 | Identical |
DIN EN 16603-31-02:2015-12 | Identical |
UNI CEI EN 16603-31-02 : 2016 | Identical |
CEI UNI EN 16603-31-02:2019 | Identical |
UNE-EN 16603-31-02:2015 | Identical |
ONORM EN 16603-31-02 : 2016 | Identical |
NEN EN 16603-31-02 : 2015 | Identical |
DIN EN 16603-31-02:2018-11 | Identical |
PNE-FprEN 16603-31-02 | Identical |
I.S. EN 16603-10-03:2014 | SPACE ENGINEERING - TESTING |
BS EN 16603-10-03:2014 | Space engineering. Testing |
EN 16603-10-03:2014 | Space engineering - Testing |
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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