Facility Capabilities
Test Stand 115 is used for the testing of small-scale combustion devices including injectors, combustion chambers, and nozzles. Testing serves to validate new combustion designs, CFD models, and propulsion efficiencies on a wide range of combustion devices.
NASA
- Ambient Test Capability
- Propellants: GH2, LH2, LOX, GCH4, LCH4, & RP
- Maximum Thrust – 7.5K lbf
- Designed for testing small scale combustion devices including injectors, combustion chambers, and nozzles
Other Test Facilities at Marshall Space Flight Center
Marshall Space Flight Center houses a comprehensive set of testing facilities for propulsion systems.