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International Journal of Energetic Materials and Chemical Propulsion
ESCI SJR: 0.149 SNIP: 0.16 CiteScore™: 0.29

ISSN Print: 2150-766X
ISSN Online: 2150-7678

International Journal of Energetic Materials and Chemical Propulsion

DOI: 10.1615/IntJEnergeticMaterialsChemProp.v4.i1-6.1050
pages 1146-1156

NONLINEAR TRANSIENT BURNING OF COMPOSITE PROPELLANTS: THE EFFECT OF SOLID PHASE REACTIONS

Jeroen Louwers
Research Group Rocket Technology, TNO Prins Maurits Laboratory, Lange Kleiweg 137, 2288 GJ Rijswijk, The Netherlands
G. M. H. J. L. Gadiot
Research Group Rocket Technology, TNO Prins Maurits Laboratory, Lange Kleiweg 137, 2288 GJ Rijswijk, The Netherlands

ABSTRACT

The phenomenon of transient burning of solid propellants is a topic which still contains a large number of questions. In this paper the transient burning of AP composite propellants is calculated within the QSHOD approach (Quasi Steady gas phase, Homogeneous One-Dimensional condensed phase). This paper focuses on the effect of the condensed phase on the transient burning of solid propellants by showing the effect of temperature dependent thermal properties, phase transitions and chemical reactions in the solid phase. Nonlinear effects are conserved, as governing equations are solved numerically.


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