Abstract: A system and method for on-demand retention, release, and positioning of structures including space structures (e.g., solar panels, probes, antennae, scientific instruments, fairings, etc.). The system allows for a lightweight and reliable deployment mechanism utilizing shape memory alloy (SMA) technology that allows for structure transition from a stowed to a deployed configuration. SMAs are used for both the active actuation members (e.g., wires) and passive connecting members (e.g., hinges). The retention and release (R&R) mechanism includes the SMA actuator, a static and detachable plate, a pin puller, and retaining latches/hooks. Once released, the deployment and positioning mechanism consists of SMA preloaded hinges and latches. The innovative system and method may be used for deployment of CubeSat and smallsats solar panels, antennae, and the like where volume and power resources are very limited.