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Pressure Dependence, Propellant Composition, Particle Size and Effect of Catalyst on Burn Rate Study of AN-HTPB based Composite Solid Propellants


Aniket Manash , Vidya Vihar Institute of Technology,Purnea; Rahul Kumar, VVIT,Purnea; Prabin Kumar, VVIT,Purnea


Pressure Dependance; Propellant Composition; Particle Size; Burn Rate; AN; HTPB; Fe2O3


In the present investigation, an effort has been made to study pressure dependence, propellant composition, particle size and effect of catalyst on the burn rate of AN based composite solid propellant. The variation of oxidizer has been made 70%, 75% and 80% based on earlier experience of the loading of HTPB on the combustion characteristics of AN based composite solid propellants. The particle size of the oxidizer in the present formulation is taken to be 44 μm and 149 μm respectively. The bimodal AN taken with mess size 150 and 300.

Other Details

Paper ID: IJSRDV6I60150
Published in: Volume : 6, Issue : 6
Publication Date: 01/09/2018
Page(s): 157-159

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