PROJECT

MOCH4

MOCH4

UCI’s second liquid bi-propellant rocket

Project Timeline (2-year cycle)

After launching our Preliminary Test Rocket (PTR) in April 2023 after 6 years of design and development, our goal is to reduce our cycle time to 2 years with our next rocket, MOCH4

Fall 2023

Conceptual & preliminary design review(s) of new system

Winter 2024

Prototyping & testing new components/systems

Spring 2024

Feed system integration & prep for cold flow testing

Fall 2024

System optimization for cold flows & vertical test fire

Winter 2025

Vehicle manufacturing and integration & cold flow testing

Fall & Spring 2025

Full system integration & launch in the Mojave Desert, CA

TESTING UPDATES: COLD FLOWS 1 - 5

The first five cold flow tests were challenging. While vent closures, pressurization, and COPV refills ran smoothly, issues arose when opening MVAS to release LN2. Initially taking over four hours, the process became significantly more efficient by the fifth test.

TESTING UPDATES: COLD FLOWS 6 - 10

Cold flows 6–10 yielded significantly improved results compared to the initial five. When we opened the MVAS to release LN2 from the tanks through the injector, the system operated smoothly; however, the desired data was not being captured. Fortunately, as VTF approached, both our cold flow performance and data output showed continuous improvement.

TESTING UPDATES: VTF #1

Our first vertical test fire did not go as planned, despite the success of our final cold flows. The engine failure was due to our ablative material not being rated for the conditions it was exposed to. Instead of burning as expected, it accumulated at the nozzle inlet, obstructing the flow. This blockage caused combustion to cease while pressure built up in the chamber until the material was forcibly dislodged, ultimately leading to an explosion.

MOCH4 BREAKDOWN

NOSE CONE

AVIONICS

MID PLUMBING

LOWER PLUMBING

UPPER PLUMBING

RECOVERY

COPV

LNG TANK

COMBUSTION CHAMBER

LOX TANK