HMX and RDX - Combustion mechanism and influence on modern double-base propellant combustion
- 1 July 1995
- journal article
- research article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Propulsion and Power
- Vol. 11 (4), 752-758
- https://doi.org/10.2514/3.23900
Abstract
No abstract availableThis publication has 8 references indexed in Scilit:
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- The Thermal Behavior of Cyclotrimethylenetrinitramine (RDX) and Cyclotetramethylenetetranitramine (HMX)Published by American Institute of Aeronautics and Astronautics (AIAA) ,1984
- Modeling Calculations for HMX Composite PropellantsAIAA Journal, 1982
- Structure of the Gas Phase Combustion Region of a Solid Double Base PropellantThe Journal of Physical Chemistry, 1955
- The Determination of the Thermal Structure of a Combustion Wave by Fine Thermocouples.The Journal of Physical Chemistry, 1950