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Auto-ignition of hydrazine by engineering materialsHydrazine, 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.
Document ID
19780036760
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Perkins, J. H.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Riehl, W. A.
(NASA Marshall Space Flight Center Huntsville, Ala., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Propellants And Fuels
Report/Patent Number
AIAA PAPER 78-72
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Huntsville, AL
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
78A20669
Distribution Limits
Public
Copyright
Other

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