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Aerospace series. Space systems. Fluid characteristics, sampling and test methods - Nitrogen tetroxide propellants Ingestion-build-180956 value-added

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Aerospace series. Space systems. Fluid characteristics, sampling and test methods - Nitrogen tetroxide propellants Ingestion-build-180956 value-added1 Scope This part of ISO 15859 specifies limits for the chemical composition and physical properties of propellants based on nitrogen tetroxide (N2O4) based propellants and establishes the sampling and test requirements applicable for the verification of the nitrogen tetroxide composition. This part of ISO 15859 is applicable to N2O4 based propellants, used as oxidizers in propellant systems of space systems as well as in both flight hardware and

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