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High Pressure Lab- ZL3

Rocket Stand 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