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High Energy Propellants for Advanced Gun Ammunition Based on RDX, GAP and TAGN Compositions
Author(s) -
Damse Ramdas S.,
Singh Amarjit,
Singh Harihar
Publication year - 2007
Publication title -
propellants, explosives, pyrotechnics
Language(s) - English
Resource type - Journals
SCImago Journal Rank - 0.56
H-Index - 65
eISSN - 1521-4087
pISSN - 0721-3115
DOI - 10.1002/prep.200700007
Subject(s) - ammunition , propellant , burn rate (chemistry) , materials science , thermal stability , internal ballistics , composite material , thermal , nuclear engineering , chemical engineering , aerospace engineering , thermodynamics , metallurgy , engineering , physics
A number of gun propellant compositions based on RDX, GAP, TAGN and combinations thereof were formulated and studied with the aim to select the suitable composition for advanced gun ammunition in respect of processability and ballistic performance. Theoretical thermochemical properties of the compositions were computed using a ‘THERM’ programme and the ballistic performance was evaluated on the basis of closed vessel tests. In addition, sensitivity, thermal characterization, thermal stability and mechanical properties of the compositions were also determined for assessing the suitability for application. A composition containing 28% NC, 45% RDX, 20% TAGN, 6% GAP, 0.7% carbamite and 0.3% resorcinol was found to provide higher level of force constant at relatively lower flame temperature, reasonably good burning rate characteristics and mechanical properties.