ZAPHOD CubeSat Structure Range

The AAC Clyde Space ZAPHOD CubeSat Structure range, 1U to 12U, is extensively tested and qualified to all major launch vehicle standards. Our flight proven best-in-class range of CubeSat structures are designed with a high level of modularity, supporting even the most bespoke payload configuration.

These lightweight and robust CubeSat structure solutions have been designed specifically with adaptability and ease of integration in mind and are some of the more user-friendly structures on the market. The modular chassis design can easily be customized to your specific mission requirements.

Available off-the-shelf with a choice of shear panel or standard cut-out pattern, the structures can be customized including bespoke cut-outs and deployable panels.

The ZAPHOD structure range simplifies modification and can be assembled around the avionics stack and payload, increasing accessibility during integration and testing. Mounting holes are provided for a variety of stack and payload configurations.

Implementing user-definable locating elements, the structure can accommodate several avionic and payload configurations enabling a high level of customization without the need for expensive redesign. Complying with NASA’s General Environmental Verification Standard (GEVS) requirements each structure is fitted with anodized rails and deployment switches, all proven on orbit.

Compatible

Compatible with all rail-deployers. Deployment switches ensure this range is compatible with manned flights and ISS compatible.

Modular

Designed with a high level of modularity, supporting even the most bespoke payload configuration. Lightweight, qualified design which maximizes internal volume. With ease of access during integration and customizable internal stack layout.

Scalable

Offering 1U, 2U, 3U & 6U form factors the ZAPHOD structure range offers scalability in your mission requirements.

Our ZAPHOD CubeSat structures are compatible with AAC Clyde Space PHOTON solar panels, meeting ISS Manned Flight design requirements when combined.