The optical isolation and stabilization technology developed through this research is targeted for insertion into near-term NASA programs such as the Laser Communications Relay Demonstration Mission (LCRD) and as an upgrade for the Optical Payload for LAsercomm Science (OPALS). The capability is considered a "Push Technology" enabling new missions or enhancing missions already planned in for Deep Space Planetary Missions, the Space Communications and Navigation (SCaN) Program, and the Deep Space Optical Terminal (DOT) Project. Design geometry is readily customized to specific payload applications. As such, the design can be scaled for a 10cm telescope (e.g., Lunar Lasercom Space Terminal), a 30.5cm telescope (e.g.,Mars Laser Communications Demonstration), or larger telescopes for deep space missions. For small telescopes, the platform can be used for isolation, stabilization, and beam tracking, thus eliminating the need for the Fine Steering Mirror and its associated cost, mass, power and volume.