TEST CELL #1:
- Thrust stand capability to 50K lbf
- Current flow and thrust measurement capability up to 30K lbf
- Chamber pressures to 1000 psi
- 200 gallon LOX run tank (1500 psi)
- 200 gallon cryogenic liquid fuel run tank (1500 psi)
- Gaseous igniter propellants
- GN2 and GHe for purges and pressurization