NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
The thermal decomposition of 1,3,5-trinitrohexahydro-1,3,5-triazine (RDX) and RDXd6 at high temperaturesThe ballistics behavior of nitramine propellants containing RDX in an inert binder was examined. It is shown that at 2000 to 5000 psi, depending on the particle size, a slope break or discontinuity in the log burning rate versus log pressure curve occurs. It is shown that at higher pressures the nitramine decomposition proceeds predominately by C-N bond rupture and gives CH2 and N20. At still higher pressures (after the slope break) the decomposition proceeds by N-N rupture. The decomposition of RDX was investigated from 170 to 800 C at atmospheric pressure. The major decomposition products were CH2, CO, CO2, N20, N2, and H20. The ratio of the products varied with the pyrolysis rate and temperature.
Document ID
19810007787
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Miller, P. J.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Nauflett, G. W.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Carlson, D. W.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Brasch, J. W., Sr.
(Naval Surface Weapons Center Silver Spring, MD, United States)
Date Acquired
August 11, 2013
Publication Date
November 1, 1980
Publication Information
Publication: NASA. Langley Res. Center The 17th JANNAF Combust. Meeting, Vol. 2,
Subject Category
Propellants And Fuels
Accession Number
81N16303
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available