PROPULSION ENGINEERING & SPACE TECHNOLOGY
ALULA: Liquid Engine Rocket
STATUS
Flown with 6,126 ft Apogee
TEAM
UC Berkeley Space Technologies and Rocketry (STAR)

SYSTEM OVERVIEW
ALULA is a bi-propellant liquid rocket engine using LOX and ethanol, developed for integration into a flight-ready vehicle. The project spans ground support equipment, cryogenic feed systems, structural integration, and thermal management, with iterative hotfire testing driving design decisions.
MY CONTRIBUTIONS
- 01
Designed and built portable, modular ground support structures for liquid engine hotfire operations, using perforated sheet metal, wood framing, and off-the-shelf hardware to enable low-cost iteration and rapid reconfiguration
- 02
Conceptualized and developed a custom high-pressure LOX exhaust solenoid valve (>450 psi), including mass optimization and CNC-machined components, to reduce cost and improve flow control precision
- 03
Led design reviews for the custom valve and supported the transition to a servo-actuated ball valve when system complexity exceeded program maturity, prioritizing test readiness over ideal performance
- 04
Redesigned thruster mounts and LOX/ethanol tank mounts, enabling a carbon-rod load-bearing structure to carry tank mass during transport and airframe integration
- 05
Supported structural integration and machining planning for tank mounts using 1-inch-thick, 8-inch-diameter 6061 aluminum stock
- 06
Integrated cryogenic insulation into engine infrastructure using thermal calculations to mitigate heat leak and ensure safe handling
- 07
Developed and tested quick-disconnect fill systems, resolving reliability issues through extensive iteration on connector orientation, angle, and microcontroller interfacing
RESULTS
Hit 6,126 ft apogee!
Enabled repeatable liquid engine hotfire operations through portable ground infrastructure
Delivered structurally integrated tank and thruster mounting concepts suitable for flight hardware
Demonstrated pragmatic system decision-making by pivoting from complex custom hardware to robust, testable solutions
Identified key reliability sensitivities in cryogenic quick-disconnect systems through hands-on testing
PROJECT GALLERY

HOTFIRE STILL
HOTFIRE TEST

ENGINE CAD ASSEMBLY

GROUND SUPPORT EQUIPMENT

SYSTEM STORAGE DESIGN

RECOVERED HARDWARE

CRYOGENIC PLUMBING