The separation device is intended to attach separable items to primary spacecrafts and then, after transportation and launch, to separate the items with specified velocity vectors.
The separation device is structurally based on the attach ring on which the separation device components are mounted. The ring is attached to a primary spacecraft.

• Separation with specified velocity vector;
• Separation with minimum angular rate;
• High reliability;
• No magnetic disturbances;
• Minimum power consumption;
• Compact size.

• Separation telemetry available;
• No gas emission;
• Modular design minimizes customization.