Aerospace series. Space systems. Fluid characteristics, sampling and test methods - Hydrazine propellant1 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

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This European Standard does not cover hazards related to:

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a small portion of the sample is thermally vapourized through the erosion of an electric spark