TY - EJOUR
AU - Dave, Pragnesh N.
AU - Ram, Parvin N.
AU - Chaturvedi, Shalini
PY - 2024
DA - February
TI - Ti-alloys: Potential nano-modifier for Rocket Propellants
T2 - International Journal of Nano Dimension (Int. J. Nano Dimens.)
VL - 7
L1 - https://oiccpress.com/international-journal-of-nano-dimension/article/ti-alloys-potential-nano-modifier-for-rocket-propellants/
DO - 10.7508/ijnd.2016.02.009
N2 - Composite solid propellants were prepared with and without nano-alloys (Ti-Co, Ti-Ni, Ti-Zn), where nano-alloys used as catalyst. These nano-alloys are prepared by hydrazine reduction method. Catalytic properties of these nanomaterials were measured on Ammonium perchorate/hydroxyterminatedpolybutadiene propellant by thermogravimetery analysis and differential thermal analysis. Both experimental results show enhance in the thermal decomposition of propellants in presence of nano-alloys. In this differential thermal analysis method experiments had done in 3 heating rate â1=5, â2=10, â3=15 degree on minute. Independent to model free; calculation of activation energy of high temperature decomposition step was done by using following kissinger equation. Burning rate of propellants is also calculated.
IS - 2
PB - OICC Press
KW - Activation Energy, Ammonium perchlorate, Burning rate, Propellants, Thermal decomposition 
EN -