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

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attention is drawn to the fact that safety systems or national and local regulations might specify requirements for either resistance to fire performance (e

and thermometers calibrated for partial immersion (designated A2 or B2) are included for each temperature range

Aerospace series. Space systems. Fluid characteristics, sampling and test methods - Nitrogen tetroxide propellants Ingestion-build-180956 chemical compositions1 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