Innovators have developed the C-Gauge, a non-invasive tension measurement device for axial loaded cords. Cordage-based flexible structure systems are used by NASA as parachutes and inflatable structures. For engineers to fully design, develop, and test these types of systems, they must understand the tension and loading of the structural components including the load-carrying cords.
Traditional in-line load cells require cords to be severed and attached to a metallic interface. The C-Gauge attaches to the cord without any severing of the cord and can measure the structural response without affecting the dynamics of the system, providing engineers a non-invasive way to test cordage-based structures with a small, low-profile, and lightweight device.
The C-Gauge is made of a 3D-printed aluminum body with strain gauges attached to the inner and outer walls of the connecting beam. The legs of the gauge attach firmly to the cord. When the cord is stretched, the tension in the cord goes through the legs and into the beam, causing it to bend. This bending creates a tension and compression stress in the bottom and top surface of the beam, respectively. The strain gauges capture the tension and compression, which are then used to determine the tension in the cord. The use of multiple strain gauges mitigates any torsion loading of the gauge and provides a direct measurement of the axial tension load of the cord.
The C-Gauge can be installed onto an existing cord in a system (e.g., the suspension, reefing, or riser lines in a parachute) without the need to remove or reinstall the cord. It is small and lightweight and does not add stiffness or weight to the cord and thus does not affect the dynamics of the parachute or the structural response of the system. The C-Gauge can be scaled to larger and smaller sizes to measure larger and smaller load capabilities, dependent on the cord.
NASA is actively seeking licensees to commercialize this technology. Please contact NASA's Licensing Concierge at