A thermal layer mechanism of combustion of solid composite propellants: Application to ammonium nitrate propellants
- 31 December 1959
- journal article
- Published by Elsevier in Combustion and Flame
- Vol. 3, 285-300
- https://doi.org/10.1016/0010-2180(59)90033-1
Abstract
No abstract availableKeywords
This publication has 5 references indexed in Scilit:
- A model describing combustion of solid composite propellants containing ammonium nitrateCombustion and Flame, 1959
- Absolute Thermal Decomposition Rates of Solids. Part II. The Vacuum Sublimation Rate of Molecular CrystalsThe Journal of Chemical Physics, 1955
- The The Theory of the Burning of Double-Base Rocket Powders.The Journal of Physical Chemistry, 1950
- The An Hypothesis for Propellant Burning.The Journal of Physical Chemistry, 1950
- The Theory of Moving Sources of Heat and Its Application to Metal TreatmentsTransactions of the American Society of Mechanical Engineers, 1946