Paper Title
Instrumented Test Stand For Green Monopropellant Propulsion Performance Evaluation

Abstract
This paper presents the architectural design of instrumentation employed in a test stand dedicated to liquid propulsion systems with a thrust capacity of up to 20N. The proposed test stand addresses three primary objectives. Firstly, it aims to validate the performance parameters of the propulsion system, including force, specific impulse, chamber pressure, and chamber temperature. Secondly, it seeks to qualify the synthesized liquid propellant, ensuring its compatibility and efficacy within the propulsion system. Lastly, the test stand is designed to facilitate the safe manipulation of the propulsion system for educational purposes. The recorded data from these measurements serve a crucial role in designing future propulsion models. By employing an instrumented propulsion system, the data allows for the design of propulsion models tailored to various forces and configurations, contributing to advancements in the field of liquid propulsion technology. Keywords - PDS, MTTR, Propulsion System, Liquid Propellant