Comparative Analysis of Potassium Nitrate-Based Solid Propellant Rockets: Sucrose vs. Sorbitol

Abstract

This studies paper gives a comprehensive comparative analysis of two strong propellant rocket fuels: potassium nitrate blended with sucrose (sugar) and potassium nitrate mixed with sorbitol. The number one goal of this examine is to assess the performance, performance, and practicality of these  propellant combinations through a sequence of static and dynamic exams. The research starts offevolved with the instruction and characterization of each propellant combinations, ensuring consistency in composition and production procedures. The static checks involve measuring the thrust produced by means of each propellant the use of a precision gauge instrument, supplying designated thrust-time profiles. These profiles are then visualized thru superior 3-D graphical representations generated the usage of MATLAB software program, highlighting the variations in burn characteristics and thrust output through the years. In addition to static exams, the studies consists of live rocket launches designed and simulated the usage of CREO software program. Each propellant is examined in equal rocket designs to ensure honest evaluation. The altitude carried out by using each rocket is meticulously measured and calculated using hooked up aerodynamic and propulsion formulation, taking into consideration an correct evaluation of the overall performance in real-international conditions. The results segment provides an intensive analysis of the thrust and altitude data, evaluating the two propellants in terms of maximum thrust, burn period, and usual efficiency. The dialogue delves into the practical implications of the findings, thinking about factors which includes fuel stability, ease of practise, price-effectiveness, and protection. Ultimately, this take a look at objectives to perceive the advanced propellant aggregate for small-scale strong propellant rockets, providing treasured insights for hobbyists, educators, and professionals within the subject of amateur rocketry. The conclusions drawn from this research will guide future developments and optimizations in strong propellant technology, contributing to safer and greater green rocket designs.