Controlled Deployment of Multi-Panel Structures
Honeybee Robotics developed the preliminary design of a solar array deployment mechanism for Bigelow Aerospace’s Genesis I spacecraft which launched in 2006.
The pantographic mechanism deployed five solar panels from a stacked configuration to a flat configuration in a synchronized, controlled fashion using only one actuator.
- Compact: The stowed 5-panel stack height was less than 8 inches and deployed to an array length of 115 inches.
- Low Mass: The deployment mechanism hardware was to weigh less than 5 lbs.
- Latching Design: The mechanism incorporated a latching feature to prevent closing once the solar array was deployed.
- Versatile: Use for controlled deployment of solar arrays, radiators, sun shades, antennas and other structural appendages