High Pressure Lab- ZL3

Building Infrastructure

Rocket Stand

  • 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

HOMEE 7-element injector on 10K Rocket Stand

PDE
Simulations
 

PED - Simulations

Supersonic Combustion After Burning Rig

Supersonic Combustion After Burning Rig