Teams

Avionics Hardware is concerned with all the physical electronics onboard Halcyon. This includes the physical power and telemetry systems and the connections between all devices and their associated flight computers for data collection. Our team members gain vast knowledge in the workings of avionics systems in the rocket industry. This ranges from the process of designing and assembling wire harnesses to the design and manufacturing of batteries and their supportive components. The team also utilizes different software for CAD modeling, PCB design, and even testing. Members in the RF sub-team also gain a thorough understanding of radio communication and how to utilize it in different applications.

The AvSoftware team creates flight software that controls the vehicle in flight and Mission Control Software which monitors the vehicle from the ground. The team also develops the hardware-in-the-loop testing system used to validate the flight computer in simulated flight-like conditions. Our members gain experience with ground antennae and RF devices, and work primarily in Python and C++.

The Fins team is tasked with designing, manufacturing, and testing the fins aboard Halcyon. To do so, we work extensively with CFD and CADs to create fin geometries and use various manufacturing processes to bring those digital models to life. We also conduct a variety of tests to ensure that the designed and manufactured fins meet our specified criteria.

The Fluids team is responsible for designing a system capable of delivering cryogenic liquid oxygen, volatile RP-1, and highly pressurized helium gas from the ground system through Halcyon's COPVs to the engine in a safe, timely, and highly precise manner. This system interacts with several parts of the rocket and is continuous throughout all stages of Halcyon’s development. Our team members develop an understanding of how fluids behave and fluid dynamics which is applicable to wide variety of industries. We also work with advanced hardware, instrumentation, and CAD and gain hands-on experience assembling fluids systems.

The Payload will be housed in the nosecone of the rocket and supported by a lightweight chassis. At 100 km, the nosecone detaches from the rocket with the payload inside, from then on the Payload operates entirely autonomously. The Payload has two primary missions; Mesospheric UV Data Collection, and proving a rapid inflation neutral buoyancy meteorological balloon concept. The Payload is very compact and highly integrated, and our team comes from a very diverse suite of backgrounds. All Payload members get hands on experience with test engineering, design, and manufacturing.

Production fabricates the designs. Production uses the ME machine shop and various machining equipment to transform our CADs into a reality. Members of the production team take 3D drawings and focus on precision and detail when machining parts.

Propulsion is responsible for the design and analysis of TREL's engines and nozzles. Currently, the propulsion team's work is split between our two main engines; TXE-2 (manufactured by EOS and Elementum) and the flight-ready Havoc engine which will power the Halcyon rocket to the edge of space. When completed, Havoc's regeneratively cooled, pressure fed, additively manufactured design will be one the most advanced ever produced by a collegiate rocketry lab. Currently, the team has completed post-processing the TXE-2 engine and is beginning testing. Our members gain a holistic understanding of TREL’s engines and their testing procedures as well as experience in Python.

Recovery has several mission critical responsibilities including but not limited to the safe recovery of Halcyon. Our major projects include: 1) The design and fabrication of the nosecone and the rocket's only separation system. 2) The development of the 2-stage vehicle recovery system and nosecone recovery system. 3) The planning and execution of drop tests. Our members gain various experience - including the development and testing of relevant circuits and GPS tracking systems for our components.

The System Integrations Team (SIT) is a bridge between the admin team and design systems. SIT members act as a point of contact between systems and work on full rocket integration problems. With CAD and system engineering principles, SIT defines the integration of the virtual and physical vehicle assembly. SIT acts as a point of contact between subteams and works on full rocket integration problems. As a member, you'll work on projects that involve maintaining team-to-team communication and documentation or ones that involve multiple teams working together.

The Structures team’s role in TREL is to design the fuel tanks, airframe, and integration mounts the rocket. The fuel tanks are 3 composite overwrapped pressure vessels (COPVs) and comprise most of the volume of the rocket. The airframe is a carbon fiber composite sandwich structure that connects the fuel tanks together. They also design secondary structures for mounting avionics, sensors, fluid lines, valves, etc. as well as an engine mount that transfers thrust from the engine to the rest of the rocket.

TVC, or Thrust Vector Control is the primary system that controls Halcyon’s trajectory. More specifically, it's a two degree of freedom gimbal that attaches to the engine to redirect its thrust around the center axis. Currently, we are finalizing the design and running simulations to ensure both our system and test stand will be structurally sound while meeting all the actuation requirements. New members will experience mechanical design and prototyping, and hopefully manufacturing and testing integration as we transition out of our design cycle.