Wafer Scale Spacecraft

Design, Fabrication and Characterization of Initial Prototype Interstellar Robotic Systems       


Project Overview

Initial interstellar missions will require a complete reevaluation and redesign of the space systems of today. The objective of the Wafer Scale Spacecraft Development program (WSSD) at the University of California Santa Barbara (UCSB) is to design, develop, assemble and characterize the initial prototypes of these robotic platforms in an attempt to pave a path forward for future innovation and exploration. This program, which is just one venture of the UCSB Experimental Cosmology Group’s Electronic and Advanced Systems Laboratory (UCSB Deepspace EAS), focuses on leveraging continued advances in semiconductor and photonics technologies to recognize and efficiently address the many complexities associated with long duration autonomous interstellar mission.


System Evolution


Evolution of Wafer Scale Spacecraft

As with any complex system, whether natural or man-made, wafer scale spacecraft technology can be projected to follow a steady evolutionary path. Through continuous iterations, both functionality and efficiency of the system will increase over time, while size and mass will decrease. Initial prototypes have been based off of commercially available components and conventional printed circuit board (PCB) construction techniques, however as these technologies are pushed to their limits a transition to partial and eventually full wafer scale integration will be necessary. At this stage inorganic nanostructures and other various nanotechnologies will be utilized to reconstruct individual elements of the system onto a custom wafer. After much optimization and testing these wafers will then have the ability to be mass manufacture using preexisting techniques developed and employed by the semiconductor industry. This evolutionary structure will produce a spacecraft which can be manufacture by the thousands at an incredibly low cost.


Current Work & Next Generation Systems:

3U Cubesat System Capable of Launching 100 Wafer Scale Spacecraft – Currently Under Development

Silicon On Insulator (SOI) Wafer With Tessellated Hex-Cell Pattern Prior to Etching


Current Research & Development

Initial generations of Wafer Scale Spacecraft were constructed with off the shelf semiconductor devices bonded to standard technology printed circuit board substrates. These units allowed for rapid, cost effective prototyping and the development of the baseline electronic systems needed for long duration deep space missions. With these baseline systems now in place, focus has shifted to system wide optimization, advanced sensor integration and further reduction of mass. The second generation of WSS will see thin circuitry (< 500um) bonded to ultra low mass pocketed wafer substrates, and will adopt a large portion of the semiconductor devices currently in use.


Second Generation Wafer Scale Spacecraft Model A

Second Generation Wafer Scale Spacecraft Model A

Assembly of the second generation Wafer Scale Spacecraft system (Model A).

This page is currently being updated.

Please check back soon for more details.



Previous Generation Printed Circuit Board Craft:


Initial Wafer Scale Spacecraft Prototype Model A (left), Model B (middle),
Model D (right) and a US Quarter


Initial Prototype Wafer Scale Spacecraft Model B



WSS Model A

The WSS Prototype Model A is the test bed on which all technologies and systems are initially employed. The unit has an Intel based embedded Linux system for ease of use and flexibility. After testing, optimization and miniturization each device is then transitioned to the smaller Model B for final implementation.




WSS Model B

The WSS Model B is the platform which will be utilized for initial low earth orbital flights, and eventually will make the transition onto a wafer substrate (Model C) Due to its small size and low mass, many units can fit into a single  cubesat deployer, and thus “swarms”can be deployed in unison. This will allow for collection of large amounts of data and characterization of the craft on a more distributed scale.



Funding for this program comes from NASA grants NIAC Phase I DEEP-IN – 2015 NNX15AL91G and NASA NIAC Phase II DEIS – 2016 NNX16AL32G and the NASA California Space Grant NASA NNX10AT93H as well as a generous gift from the Emmett and Gladys W. fund.
For more information please contact:
Nic Rupert
Experimental Cosmology Group
Department of Physics,
University of California,
Santa Barbara, CA 93106-9530