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Information Journal Paper

Title

TI-ALLOYS: POTENTIAL NANO-MODIFIER FOR ROCKET PROPELLANTS

Pages

  168-173

Abstract

 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 b1=5, b 2=10, b 3=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.

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    Cite

    APA: Copy

    DAVE, PRAGNESH N., RAM, PRAVIN N., & CHATURVEDI, SHALINI. (2016). TI-ALLOYS: POTENTIAL NANO-MODIFIER FOR ROCKET PROPELLANTS. INTERNATIONAL JOURNAL OF NANO DIMENSION (IJND), 7(2), 168-173. SID. https://sid.ir/paper/322308/en

    Vancouver: Copy

    DAVE PRAGNESH N., RAM PRAVIN N., CHATURVEDI SHALINI. TI-ALLOYS: POTENTIAL NANO-MODIFIER FOR ROCKET PROPELLANTS. INTERNATIONAL JOURNAL OF NANO DIMENSION (IJND)[Internet]. 2016;7(2):168-173. Available from: https://sid.ir/paper/322308/en

    IEEE: Copy

    PRAGNESH N. DAVE, PRAVIN N. RAM, and SHALINI CHATURVEDI, “TI-ALLOYS: POTENTIAL NANO-MODIFIER FOR ROCKET PROPELLANTS,” INTERNATIONAL JOURNAL OF NANO DIMENSION (IJND), vol. 7, no. 2, pp. 168–173, 2016, [Online]. Available: https://sid.ir/paper/322308/en

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