The deployment mechanisms are suitable for a variety of small and microsatellites from 2U up to satellites of many tens of kg, and utilize specialized torsion springs or vortex springs.
Deployment mechanisms can be used for solar arrays.
Weight | ≤6.3g |
Dimensions(mm) | 20x33x7.3 |
Platform Compatibility | 6U, 8U 12U cubesat |
Operating Temperature | -90℃ to +100℃ |
Other remarks | Fully customizable deployment angle, optional MoS2 coating |