High Pressure Lab- ZL3
Building Infrastructure
- Two major test cells classed to 10,000 lbf thrust levels
- Laser laboratory
- Tools for Stainless Tube Fabrication
Research Focus Areas:
- Gas turbine combustion stability
- Gas turbine emissions
- Gas turbine high temperature fuel
- Large liquid rocket engine combustion
- Supersonic combustion
HOMEE 7-element injector on 10K Rocket Stand
PDE
Simulations
Supersonic Combustion After Burning Rig
