Materials and Structures Optimization / Process Development for the Mega-ROSA / ROSA Solar Array

Deployable Space Systems, Inc. (DSS), in collaboration with the University of California, Santa Barbara (UCSB), Department of Mechanical Engineering, will focus the proposed NASA STTR Phase 2 program on the materials optimization, structures optimization, creep / relaxation phenomena characterization and analytical modeling, and manufacturing process optimization/development for the Mega-ROSA/ROSA solar array. The ROSA technology (termed for: Roll-Out Solar Array) is a new/innovative mission-enabling solar array system that offers maximum performance in all key metrics and unparalleled affordability for NASA's Space Science & Exploration missions. ROSA will enable NASA's emerging Solar Electric Propulsion (SEP) Space Science & Exploration missions through its ultra-affordability, ultra-lightweight, ultra-compact stowage volume, high strength/stiffness, and its high voltage and high/low temperature operation capability within many environments. Multiple identified end-users provide strong commercial infusion paths for the ROSA solar array upon the successful execution of the proposed Phase 2 program technology advancements.

NASA space applications are comprised of practically all Exploration, Space Science, Earth Science, Planetary Surface, and other missions that require high-efficiency photovoltaic power production through deployment of an ultra-lightweight and highly-modular structural system. The technology is particularly suited for NASA's SEP missions and other missions that require game-changing performance in terms of affordability, ultra-lightweight, compact stowage volume, and superior structural performance. The technology is also well suited for applications requiring scalability/modularity, high deployed strength/stiffness, operability within high radiation environments, high voltage operation, and operation in LILT and HIHT environments.

Non-NASA space applications are comprised of practically all missions that require high-efficiency photovoltaic power production through deployment of an ultra-lightweight and highly-modular structural system. The technology is particularly suited for SEP missions that require game-changing performance in terms of affordability, ultra-lightweight, compact stowage volume, and superior structural performance. Applicable non-NASA space missions include: LEO surveillance, reconnaissance, communications and other critical payload/equipment satellites, LEO commercial mapping and critical payload/equipment satellites, MEO satellites & space-tugs, GEO commercial communications and critical payload/equipment satellites, and GEO communications and payload/equipment satellites. The proposed technology also has tremendous dual-use non-space commercial private-sector applicability including fixed-ground and deployable/retractable mobile-ground based systems.

This is early/mid-stage (TRL 5) — the most realistic path in is NASA SBIR/STTR, which funds small businesses and research institutions to develop technology aligned with NASA's needs (equity-free, phased funding). Check whether a current SBIR/STTR solicitation topic overlaps with this project's technology area, or contact the project directly (above) to ask.

None of these are guaranteed paths for this specific project — TechPort itself doesn't have an "apply" button. Reaching out to the contact(s) above with a specific question is usually the fastest way to find out what's actually open.