Completed Projects
LRE Gen-II | Ablatives Engine
A 3kN liquid rocket engine made from wood composite ablative material - a leap towards sustainable rocket propulsion.
High Altitude Payload Gen-I
The first-generation flight computer and RF payload, sent to 27km in altitude and retrieved 250km from the launch site.
Liquid Rocket Engine Gen-I
SFU Rocketry’s first Liquid Rocket Engine - a 3kN heatsink engine with supporting fluids systems.
Test Stand Structure
The structural system that safely supports rocket engines and fluids systems, while bracing against large forces.
LRE Gen-I | Engine Control System
The electronics, firmware, and software that controls the safe and successful ignition and firing of a Propulsion System.
