Current Use: Active; Load and heat testing of structural components and complete flight vehicles. Calibrate and evaluate flight loads instrumentation under conditions expected in flight.
Capacities: High bay 120’D x 164’W; reinforced concrete floor with tie-down slots in floor and 136’W x 40’H hangar door. Total high bay area 19,680 ft2; 10,000 ft2 useable area for aircraft.
Unique Capabilities: High bay test area with adjacent laboratory, office, and storage area. Data acquisition and test control room overlooking test area. 5-ton rail crane, 39′ max height. Carbon-carbon and titanium test capabilities. Thermal and cryogenic systems. Power output range from 1,000 to 20,000 kW and testing temperature range from -100 to 3,000 °F.
Availability: As needed
Point of Contact
NASA Armstrong Public Affairs
(661) 276-4447