Thermal decomposition of cured GAP-AP propellants containing catocene
- 22 March 1993
- journal article
- Published by Elsevier in Thermochimica Acta
- Vol. 216, 255-266
- https://doi.org/10.1016/0040-6031(93)80396-r
Abstract
No abstract availableKeywords
This publication has 11 references indexed in Scilit:
- Thermal decomposition of energetic materials 54. Kinetics and near-surface products of azide polymers AMMO, BAMO, and GAP in simulated combustionCombustion and Flame, 1991
- Energetics of Nitro/Azide PropellantsPropellants, Explosives, Pyrotechnics, 1991
- Thermal characteristics of GAP, GAP/BDNPA/BDNPF and PEG/BDNPA/BDNPF and the energetic composites thereofThermochimica Acta, 1991
- Burning rate characteristics of GAP propellantsJournal of Propulsion and Power, 1990
- Combustion Mechanism of Azide PolymerPropellants, Explosives, Pyrotechnics, 1988
- Fracto-emission accompanying adhesive failure between rocket propellent constituentsJournal of Applied Physics, 1987
- Correlation between fracture properties and dynamic mechanical relaxations in composite propellantsPolymer, 1987
- Effects of Additives on the Ignition of AP-Based Propellants at subatmospheric pressuresPropellants, Explosives, Pyrotechnics, 1985
- Combustion studies on ammonium perchlorate/trimethylammonium perchlorate mixturesCombustion and Flame, 1982
- Effect of Transition Metal Oxides on Decomposition and Deflagration of Composite Solid Propellant Systems: A SurveyAIAA Journal, 1979