01 / Propulsion
Liquid rocket
engine
Engine designer 2026 — present
A Python toolchain that sizes a pressure-fed liquid engine end to end: chamber and nozzle, regenerative cooling, injector, feed system and test stand. It produces cited, automated reports. The first case is a 1 kN N₂O/ethanol engine.
- Thrust
- 1 kN SL
- Propellants
- N₂O / ethanol
- Chamber
- 20 bar
- Feed
- N₂ pressure-fed
- Cooling
- Ethanol regen
- Build
- AlSi10Mg SLM
02 / Avionics
EXO
Flight Computer
Hardware designer 2026 — present
An RP2350B flight computer on a 42 × 140 mm board with an IMU, dual barometers, GNSS, LoRa telemetry and pyro channels. Python scripts generate the schematic, placement and fab outputs.
- MCU
- RP2350B
- Board
- 42 × 140 mm
- Sensors
- IMU · 2× baro · GNSS
- Radio
- LoRa
- EDA
- KiCad, scripted
- Routing
- Freerouting
03 / Systems
100 km
avionics
Systems design 2026
A redundant avionics architecture for a 100 km-apogee liquid rocket. It covers requirements, the interface control document, CAN-FD to the engine controller, remote arming, and a verification plan for vacuum, thermal and shaker testing.
Scroll to fly ↓
- T+
- 000.0 s
- Altitude
- 000.0 km
- Velocity
- 0000 m/s
Nominal drag-free profile, illustrative only
04 / Experience
Where I've
been
UNSW Rocketry
Student team designing and launching rockets for the Australian Universities Rocketry Competition and Spaceport America Cup.
- Vice PresidentExecutive
- TreasurerExecutive
- Propulsion Co-LeadTechnical
- Propulsion EngineerTechnical
- Aerodynamics EngineerTechnical
UNSW Sydney
Bachelor of Engineering (Honours), Aerospace Engineering.
- Casual Academic & TutorTeaching
- Student AmbassadorOutreach
Toolkit
05 / Contact
Let's
talk.
Have a project, a role or a question? My inbox is open.