BS ISO 14624-5:2006
Superseded
A superseded Standard is one, which is fully replaced by another Standard, which is a new edition of the same Standard.
View Superseded by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 Determination of reactivity of system/component materials with aerospace propellants
Hardcopy , PDF
08-06-2023
English
31-05-2006
Committee |
ACE/68
|
DevelopmentNote |
Supersedes 03/312637 DC (05/2006)
|
DocumentType |
Standard
|
Pages |
20
|
PublisherName |
British Standards Institution
|
Status |
Superseded
|
SupersededBy | |
Supersedes |
This part of ISO14624 specifies test equipment and techniques used to identify interactions resulting from exposure of a material to an aerospace fluid.
This part of ISO14624 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 12months) long-term tests need to be used to quantify degradation as a function of time under use conditions.
Standards | Relationship |
ISO 14624-5:2006 | 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 5725:1986 | Precision of test methods Determination of repeatability and reproducibility for a standard test method by inter-laboratory tests |
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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