Modification to Making Advancements in Commercial Hypersonics (MACH).

The NASA Armstrong Flight Research Center (AFRC) is seeking a modern, safe, modular servo-hydraulic load-control system to support structural ground testing of aerospace components, wings, and full-scale assemblies. The system should have a 32-channel closed-loop load control system integrated with an independent Controlled Load Abort System (CLAS) using Controlled Load Abort Manifolds (CLAMs). The system will replace an older load control system from Moog. • The system must be software compatible with the legacy Moog platform. • The system must have controlled load abort capability. • The system will be used for complex load tests of unique test articles and flight vehicles. • The system must provide precise control, test article protection, and safe emergency handling.