Estimation of Ideal Specific Impulse of Paraffin Wax-Fueled Lab-Scale Hybrid Rocket Motor Using Chebyshev Method

Author(s)	Sreehari Kambrath, Aswini M.G
Country	India
Abstract	This paper investigates the theoretical specific impulse of lab-scale hybrid rocket motors using paraffin wax fuels. It analyzes area ratios (2.0–5.0), combustion reactions with gaseous oxygen, and specific heat ratios. Numerical methods solve non-linear exit Mach functions. Specific impulse predictions for four waxes under static tests aid hybrid propulsion optimization
Keywords	exit mach number, area ratio, specific impulse numerical methods, paraffin wax,
Field	Engineering
Published In	Volume 7, Issue 1, January-February 2025
Published On	2025-01-19
Cite This	Estimation of Ideal Specific Impulse of Paraffin Wax-Fueled Lab-Scale Hybrid Rocket Motor Using Chebyshev Method - Sreehari Kambrath, Aswini M.G - IJFMR Volume 7, Issue 1, January-February 2025. DOI 10.36948/ijfmr.2025.v07i01.35495
DOI	https://doi.org/10.36948/ijfmr.2025.v07i01.35495
Short DOI	https://doi.org/g82gmt

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