Propulsion and Test
The Propulsion and Test team within the THRUST student project is responsible for one of the most critical aspects of the rocket’s performance: the design and optimization of the propulsion system. Their primary focus is the combustion chamber, where fuel and oxidizer mix to produce the powerful thrust needed for launch. The team designs this chamber with precision, ensuring it can withstand the extreme temperatures and pressures generated during combustion while maximizing efficiency. They utilize advanced simulation tools and testing data to refine the chamber’s design, pushing the boundaries of what is possible in small-scale rocket engines.
In addition to the combustion chamber, the Propulsion and Test team also works on the interstage assembly, which is the structural link between the rocket’s propulsion system and its upper stages. This assembly must not only provide a secure connection but also facilitate the transfer of forces and separation during stage transitions. The team carefully engineers the interstage to meet these demands, ensuring it is lightweight yet robust enough to handle the mechanical stresses of flight. Its design plays a key role in ensuring the smooth and reliable operation of multi-stage rockets.
Testing is another crucial responsibility of this team, as they lead the validation of the propulsion system through rigorous ground tests. This process involves building test stands, monitoring engine performance, and analyzing data to verify that the combustion chamber and interstage assembly function as intended. The Propulsion and Test team is dedicated to refining every detail through iterative testing, ensuring the propulsion system meets safety and performance standards before it ever reaches the launch pad.