The RCL includes a low-flow ignition rig, a high-temperature thermal shock test bed for testing rocket materials, a low-thrust chemical rocket altitude facility, an air-breathing combustor rig, and several sea-level test stands.
Description The Research Combustion Laboratory (RCL) develops aerospace propulsion technology by performing tests on propulsion components and materials. Altitudes up to 137,000 feet can be simulated. The Small Multi-Purpose Research Facility, or SMiRF, evaluates the performance of the thermal protection systems required to provide long-term storage (of up to 10 years) of cryogenic propellants in space.
Name:
Research Combustion Laboratory
RCL-11 Cell:
A low thrust (50 lbf maximum) combustion facility with altitude simulation capability
RCL-21 Cell:
Altitude facility for conducting small chemical propulsion research
RCL-22 Cell:
A sea-level test stand, typically used as a high temperature thermal shock rig
RCL-24C Cell:
Currently being upgraded to provide testing of Regenerative Fuel Cells