ISO 15859-6:2004
Current
The latest, up-to-date edition.
Space systems Fluid characteristics, sampling and test methods Part 6: Monomethylhydrazine propellant
Hardcopy , PDF , PDF 3 Users , PDF 5 Users , PDF 9 Users
English, French
08-06-2004
ISO 15859-6:2004 specifies limits for the composition of monomethylhydrazine and establishes the sampling and test requirements applicable for the verification of the monomethylhydrazine (MMH) composition.
ISO 15859-6:2004 is applicable to monomethylhydrazine propellant, used as a fuel in propellant systems of space systems as well as in both flight hardware and ground facilities, systems, and equipment, of Grade A (98,0 % pure) and Grade F (98,5 % pure).
ISO 15859-6:2004 is applicable to influents only within the specified limits herein.
ISO 15859-6:2004 is applicable to any sampling operation required to ensure that, when the fluid enters the launch vehicle or spacecraft, the fluid composition complies with the limits provided hereafter or with any technical specification agreed to for a particular use.
DevelopmentNote |
Supersedes ISO/DIS 15859-6 (06/2004)
|
DocumentType |
Standard
|
Pages |
6
|
PublisherName |
International Organization for Standardization
|
Status |
Current
|
Standards | Relationship |
BS ISO 15859-6:2004 | Identical |
GOST R ISO 15859-6 : 2010 | Identical |
ISO 14624-5:2006 | Space systems — Safety and compatibility of materials — Part 5: Determination of reactivity of system/component materials with aerospace propellants |
BS ISO 14624-5:2006 | Space systems. Safety and compatibility of materials Determination of reactivity of system/component materials with aerospace propellants |
ISO 9000:2015 | Quality management systems — Fundamentals and vocabulary |
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