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ISO 14624-5:2006

Superseded

Superseded

A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.

View Superseded by

Space systems — Safety and compatibility of materials — Part 5: Determination of reactivity of system/component materials with aerospace propellants

Available format(s)

Hardcopy , PDF 1 User , PDF 3 Users , PDF 5 Users , PDF 9 Users

Superseded date

01-06-2023

Superseded by

ISO 14624-5:2023

Language(s)

English

Published date

19-04-2006

$118.72
Including GST where applicable

ISO 14624-5:2006 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid.

ISO 14624-5:2006 may be used to determine the reactivity of system and component materials with aerospace fluids. It is applicable for determining interactive reactions between propellants and materials used in the design, construction, and operation of propellant storage, transfer, and flight systems. While this procedure is an excellent quick screen test for long-term propellant compatibility, it is semi-qualitative, and (if exposures exceed twelve months) long-term tests need to be used to quantify degradation as a function of time under use conditions.

Committee
ISO/TC 20/SC 14
DevelopmentNote
Supersedes ISO/DIS 14624-5 (04/2006)
DocumentType
Standard
Pages
11
PublisherName
International Organization for Standardization
Status
Superseded
SupersededBy

Standards Relationship
BS ISO 14624-5:2006 Identical
GOST R ISO 14624-5 : 2010 Identical

ISO 14951-7:1999 Space systems Fluid characteristics Part 7: Hydrazine propellant
ISO 15859-6:2004 Space systems Fluid characteristics, sampling and test methods Part 6: Monomethylhydrazine propellant
ISO 15859-5:2004 Space systems Fluid characteristics, sampling and test methods Part 5: Nitrogen tetroxide propellants
ISO 15859-7:2004 Space systems Fluid characteristics, sampling and test methods Part 7: Hydrazine propellant
ISO 14951-6:1999 Space systems Fluid characteristics Part 6: Monomethylhydrazine propellant
ISO 14951-5:1999 Space systems Fluid characteristics Part 5: Nitrogen tetroxide propellant
ISO 15859-3:2004 Space systems Fluid characteristics, sampling and test methods Part 3: Nitrogen
ISO 4954:1993 Steels for cold heading and cold extruding

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