Current Flow Capabilities
Propellant
Test Cell
Maximum Flow Capacity
Max. Operating Condition
Heated High Pressure Air
Rocket & Gas Turbine
15 lbm/sec
700 psi / 1,000 deg F
High Pressure Air
HPL Annex
50 lbm/sec
1,500 psi / ambient
Electric Heated Air or Nitrogen
Gas Turbine
1 lbm/sec
600 psi / 1,200 deg F
Nitrogen
Rocket / Gas Turbine
5 / 2 lbm/sec
5,000 psi
Nitrogen
HPL Annex
2 lbm/sec
5,000 psi
Liquid Aviation Fuel (kerosene)
Rocket / Gas Turbine
22 / 1 lbm/sec/tank
5,000 / 1,500 psi
Liquid Aviation Fuel (kerosene)
HPL Annex
0.5 lbm/sec
1,000 psi
Cooling Water
Rocket / Gas Turbine
600 / 25 gpm
5,000 / 400 psi
Liquid Oxygen
Rocket
15 lbm/sec
5,000 psi
Rocket Grade Hydrogen Peroxide
Rocket
100 lbm/sec
5,000 psi
Gaseous and Liquid Methane
Rocket
5.0 lbm/sec
1,300 psi
Natural Gas
Gas Turbine
1.0 lbm/sec
3600 psi
Gaseous Hydrogen
Rocket
3 lbm/sec
5,000 psi
Gaseous Heated Propane
HPL Annex
1 lbm/sec
300 psi