Ground testing of the boron carbide-enhanced propulsion system was successfully conducted. The test stand performance represents the highest achievement to date. This was the culmination of years of development work. The progression from HTP monopropellant to IWFNA bipropellant to boron-enhanced systems brought significant performance improvements at each step. The test stand was equipped with a larger thruster using IWFNA as the oxidizer and boron carbide-enhanced morpholine-TEA as the fuel. The thruster was designed for a burn time of about 25 seconds. The test sequence proceeded smoothly. At ignition, the thruster fired and ignited. The thrust was strong and consistent. The test stand recorded steady, stable performance throughout the burn. The test was smooth and stable. There were no vibrations or instabilities. The thrust profile remained consistent throughout the test. Post-test inspection of the thruster showed no signs of damage or degradation. The combustion chamber was clean, and the nozzle was in good condition. The boron oxide and carbon dioxide products in the exhaust did not cause any damage. The test data was excellent. Thrust, pressure, temperature, and combustion characteristics were recorded throughout the test. The data shows that the thruster performed exactly as predicted. Specific impulse was 275 seconds, which is outstanding. This represents a 169% improvement compared to the baseline IWFNA system. This ground test validates the entire boron-enhanced approach. Boron additives successfully demonstrated dramatic performance improvement of the propulsion system. The system is safe, reliable, and effective. Looking back at the development journey, significant progress had been made. The program started with HTP monopropellant in 2012. Transition to IWFNA bipropellant occurred in 2019. Boron hydride was added in 2023. Record performance with boron carbide was achieved in 2025. Each step brought new challenges and new solutions. Failures and setbacks were encountered, but lessons were learned and progress continued. New materials, procedures, and understanding of propulsion chemistry were developed. The next phase of the development program was being planned. Hybrid boron formulations, advanced combustion chamber designs, and new fuel blends were being explored. Additional ground testing with boron carbide-enhanced fuel was planned. Thruster size and test stand configurations would be varied for future tests. This represents a major achievement. The performance envelope of the propulsion system was pushed to new levels. With careful engineering and scientific understanding, exceptional performance was achieved.