@article{Dave_Ram_Chaturvedi_2024, title={Ti-alloys: Potential nano-modifier for Rocket Propellants}, volume={7}, url={https://oiccpress.com/international-journal-of-nano-dimension/article/ti-alloys-potential-nano-modifier-for-rocket-propellants/}, DOI={10.7508/ijnd.2016.02.009}, abstractNote={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.}, number={2}, journal={International Journal of Nano Dimension (Int. J. Nano Dimens.)}, publisher={OICC Press}, author={Dave, Pragnesh N. and Ram, Parvin N. and Chaturvedi, Shalini}, year={2024}, month={Feb.}, keywords={Burning rate, Propellants, Thermal decomposition, Activation Energy, Ammonium perchlorate} }