Propulsion
Liquid rocket engine development for our launch vehicle — and cryogenic engineering expertise you can hire
Our Engine Program
We are developing a liquid rocket engine burning LOX and methane (LCH4) for our own launch vehicle. Engine design, injector work, and test campaigns all happen in-house — this program is the engine (literally) behind our cryogenic expertise.
- LOX/LCH4 liquid propulsion
- Combustion chamber and injector design
- In-house test and iteration
Cryogenic Propellant Systems
Storing and moving cryogenic propellants safely is half the propulsion problem. We design and build the tanks, lines, valves, and insulation our engine program needs — and offer that engineering to others working with cryogenic fluids.
- Cryogenic storage and transfer system design
- Insulation and thermal management
- Safety systems and handling procedures
Propellant Pressurisation
Our propellant pressurisation work produced a commercial product: the triple metal diaphragm gas compressor, delivering high-purity gas at up to 40 bar. It runs in our own test operations and is available for your lab or process line.
- Pressurisation system design for propellant feed
- Gas compressor: 40 bar / 580 PSI, high-purity service
- See the gas compressor →
Cryo Engineering Services
The same team that keeps our propellants liquid works on customer problems: cryogenic system design, thermal analysis, and hardware for research and industrial applications.
- Consulting and system design
- Thermal and flow analysis
- Custom cryogenic hardware