Case Study: Xometry Helps UC Irvine Rocket Team Prepare for Spaceshot

The UC Irvine Rocket Project is the first endeavor of its kind at the University of California, Irvine. This team of 31 students has taken on the challenge of designing and building a liquid-fueled rocket that will launch into space by 2021, in preparation for the FAR-Mars Launch Contest and the Base 11 Space Challenge. Their first and biggest challenge is to build a fuel injector that will subsequently lead to the development of an engine with the capability of sending a rocket to a height of 100 km above Earth’s sea level.

Over the past few quarters, the team has developed a strong base design for the rocket that meets the requirements of the FAR-Mars competition. They’ll create a liquid bipropellant rocket that uses liquid methane and liquid oxygen as its propellants. This chain of chemical reactions will allow the engine to thrust upwards at a force of 1,300 lbs for a duration of approximately 7.5 seconds. The maximum total impulse allowed is 9,208 lbf-seconds and a total rocket mass under 155 lbs. For the rocket to perform at maximum efficiency within these parameters, “everything is contingent on the fuel injector working,” says Chief Engineer Mitchell Martinez.

When Martinez brought the preliminary fuel injector design to injector specialists at NASA Marshall Space Flight Center, his internship mentors told him the design would likely cause the injector to fail in a matter of microseconds. Undeterred, the UC Irvine team iterated until they reached a final prototype that has a less efficient, but more stable burn. In consultation with local and on-campus professional machinists, they designed their injector features to be manufactured in two steps. The first would use CNC machining with standard tooling and the second would use wire EDM for the injector elements.

Several design considerations were involved in the creation of the UC Irvine team’s injector parts, which Xometry manufactured using its CNC Machining Services.

• Engine stability: The student team chose a showerhead injector design with straight throughholes. This design allows for less fuel mixing but increased stability.
• The UC Irvine team designed these critical tight tolerances to ensure the injector creates a uniform burn, which will allow the flow to evenly exit the engine so the rocket launches perpendicular to the ground.
• Precision Fitment: Xometry manufactured the injector fitments at the tightest tolerance range of +/- 0.001. The UC Irvine team designed these critical tight tolerances to allow the components to be assembled freely while still providing some level of sealing in case of an O-Ring failure.
• Precise assembly: The team designed a groove in the end plate, so Xometry manufactured the end plate with a specific surface area smoothness of 16uin/0.4um Ra in which to place an O-ring.

Cryogenic shock-resistant material: The team’s choice of material was aluminum 6061 because when this metal is exposed to cryogenics like liquid methane and liquid oxygen, it will not experience detrimental effects from cryogenic shock.

The UC Irvine Rocket Project team was excited to receive their parts in pristine shape and exactly to specification.

Since the fuel injector was manufactured exactly to spec, the team is confident the rocket’s engine should perform as they designed it and without any error introduced from the manufacturing process. They can now design the rest of the rocket components confidently, from the structure to the control and recovery system to the plumbing.