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Fixed-point or spark-plug discharge systems are challenging to set up and maintain, often suffering from performance degradation or failure as repeated discharges damage and alter contact points. Similarly, contact-based solutions like slip rings can introduce torque drag and create contamination particles over time as materials wear down. The SAG system eliminates these problems with its innovative contactless design, proven to cycle reliably tens of thousands of times without failure. In testing, this system survived approximately 25,000 times the expected mission charge cycles. The SAG system consists of a flexure, discharge point, and bleed circuit that controls the voltage, location and current at which a discharge occurs. The flexure is electrically isolated from the rest of the stationary body forcing the discharge current to go through the bleed circuit. This provides the ability to protect sensitive electronics from a sudden field collapse or ground plane disturbance. The flexure is able of taking different forms depending on the application and desired characteristics allowing for a scalable system, modifiable for various mission parameters. Additionally, the SAG system is passive until needed, requiring no active electronics unless used as a sensor. Due to its contactless nature, the SAG system simplifies live wear testing, significantly lowering costs compared to traditional mechanisms. Unlike fixed-point systems, it does not require precise dynamic clearances, making it more tolerant to launch loads and reducing the severity of electrical discharge events. Although designed for space and planetary exploration applications, the SAG system may also be valuable for terrestrial use cases for monitoring charging of electrically isolated components where charge buildup may occur or where grounding isn’t possible. The SAG System is at technology readiness level (TRL) 6 (system demonstration in relevant environment) and is available for patent licensing.