Our lightweight CubeSat structure range is one of the most user-friendly on the market. Designed with adaptability and ease of integration in mind, it can support even the most bespoke payload configuration.
The AAC Clyde Space ZAPHOD CubeSat Structure range, 3U 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. 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 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.
Why the ZAPHOD CubeSat Structure?
TRL 9
12-14 Week Lead Time
Flown Since 2014
3U, 6U & 12U form factors available
Compliant with CubeSat design specification
Compatible with all rail-deployers
Deployment switches ensure this range is compatible with manned flights
ISS compatible, lightweight, qualified design
Maximizes internal volume
Ease of access during integration with customisable internal stack layout
Technical Specification
General
Aluminium 7075 & 6082 used for primary structures
All other materials comply with typical outgassing requirements
Temperature range -40˚C to +80˚C
Four deployment switches - two on the -Z end plate and two on the rails
Size and Weight
Structure
3U
6U
12U
Length
100 mm
100 mm
226.3 mm
Width
100 mm
226.3 mm
226.3 mm
Height
340.5 mm
340.5 mm
340.5 mm
Weight
394 g
674 g
1386 g
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