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Propagation of detonations in hydrazine vaporIn the range of greater hydrazine vapor pressure, detonation speed depends exclusively on the extent of the ammonia decomposition in the second reaction stage. As vapor pressure decreases, the ammonia disintegration speed becomes increasingly slower and the reaction reached in the reaction zone increasingly decreases until finally, in the vapor pressure range between 53 and 16 Torr, the contribution of the second stage to detonation propagation disappears, and only the first stage remains active. Since the disintegration speed of the hydrazine in this pressure range has decreased markedly as well, no level, but rather only spinning, detonations occur. Temporary separations of the impact front and the reaction zone in the process lead to fluctuations of the detonation speed.
Document ID
19860016255
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Heinrich, H. J.
(NASA Headquarters Washington, DC United States)
Date Acquired
September 5, 2013
Publication Date
September 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-TM-77922
NAS 1.15:77922
Report Number: NASA-TM-77922
Report Number: NAS 1.15:77922
Accession Number
86N25727
Funding Number(s)
CONTRACT_GRANT: NASW-4006
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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