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NASA NTRS · 19780036760

Auto-ignition of hydrazine by engineering materials

Abstract

Hydrazine, being a monopropellant, can explode and/or detonate in contact with some materials. This has been generally recognized and minimized by testing the compatibility of engineering materials with hydrazine at ambient temperature. Very limited tests have been done at elevated temperatures. To assess the potential hazard of hydrazine leakage into a propulsion compartment (boattail), autoignition characteristics of hydrazine were tested on 18 engineering materials and coatings at temperatures of 120 C to over 330 C. Furthermore, since hydrazine can decompose violently in nitrogen or helium, common purging cannot assure safety. Therefore tests were also made in nitrogen. Detonations occurred on contact with five materials in air. Similar tests in nitrogen did not lead to ignition.

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BibTeXRIS

Perkins, J. H., Riehl, W. A.. 1978-01-01. Auto-ignition of hydrazine by engineering materials. https://ntrs.nasa.gov/citations/19780036760

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