TG studies of a composite solid rocket propellant based on HTPB-binder
- 1 September 2004
- journal article
- Published by Springer Nature in Journal of Thermal Analysis and Calorimetry
- Vol. 77 (3) , 803-813
Abstract
No abstract availableKeywords
This publication has 14 references indexed in Scilit:
- Non-isothermal degradation of a thermoset powder coating in inert and oxidant atmospheresJournal of Thermal Analysis and Calorimetry, 2003
- TA on Mo(W)/Cu(Ag)/S clusters derived with [Cp*MS3]- Kinetics of [PPh4]2[Cp*WS3(CuBr)3]2 and [PPh4]2[Cp*MoS3(CuBr)3]2Journal of Thermal Analysis and Calorimetry, 2002
- Kinetic Analysis of Dissociation of Smithsonite from a Set of Non-isothermal Data Obtained at Different Heating RatesJournal of Thermal Analysis and Calorimetry, 2001
- Thermal decomposition kinetics of PBAN-binder and composite solid rocket propellantsCombustion and Flame, 1999
- Effect of fuel binder and oxidiser particle diameter on the combustion of ammonium perchlorate based propellantsFuel, 1998
- Thermal decomposition study of hydroxyl-terminated polybutadiene (HTPB) solid fuelThermochimica Acta, 1996
- Thermal decomposition of phase-stabilised ammonium nitrate (PSAN), hydroxyl-terminated polybutadiene (HTPB) based propellants. The effect of iron(III) oxide burning-rate catalystThermochimica Acta, 1995
- Chemistry and kinetics of hydroxyl-terminated polybutadiene (HTPB) and diisocyanate-HTPB polymers during slow decomposition and combustion-like conditionsCombustion and Flame, 1991
- Kinetic analysis of derivative curves in thermal analysisJournal of Thermal Analysis and Calorimetry, 1970
- Kinetic analysis of thermogravimetric dataJournal of Applied Polymer Science, 1961