Aerospace series. Space systems. Fluid characteristics, sampling and test methods - Hydrazine propellant algolia-search-ignore

Aerospace series. Space systems. Fluid characteristics, sampling and test methods - Hydrazine propellant algolia-search-ignore1 Scope This part of ISO 15859 specifies limits for the composition and physical properties of anhydrous hydrazine (N2H4) and establishes the sampling and test requirements applicable for the verification of the anhydrous hydrazine composition. This part of ISO 15859 is applicable to anhydrous hydrazine propellant, intended for use as fuel in propellant systems of space systems as well as in both flight hardware and ground facilities, systems, and

requirements for which are contained in IEC 60034

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These properties help the users to avoid cracks or flaws and delamination from the substrate

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not merely between two standards such as ISO 9001 and ISO 14001 (environment) but as part of an overall system for the organization

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BS ISO 21460 does not specify:

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