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Solar Sail Tubular Mast

Active
NASA-SBIR-158601SBIR / STTR

Contract Overview

Solicitation details, issuing organization, response deadlines, documents, and interested companies for this government contract opportunity.

General Info

Agency

National Aeronautics and Space Administration → NASA SBIR/STTR ProgramView Agency

NAICS

541715 - Research and Development in the Physical, Engineering, and Life Sciences (except Nanotechnology and Biotechnology)View NAICS

Place of Performance

Hampton, CO, 23681, USA

Set-Aside

SBA

Documents

(1)

T5.05-2204 Solar Sail Tubular Mast Briefing Chart

PDFbriefing-chart

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Timeline

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Organization & Contact Information

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AgencyNational Aeronautics and Space Administration → NASA SBIR/STTR Program
Contacts4 people available
OfficeUSA
Organization / Agency
National Aeronautics and Space Administration → NASA SBIR/STTR Program
View Agency Profile
Office AddressUSA
Contacts
Jerry E WarrenProject Manager
Thomas MurpheyPrincipal Investigator
Jason L KesslerProgram Director
Carlos TorrezProgram Manager

Interested Companies (2)

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University of Colorado Denver
Denver, CO

Full Description

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Opterus and the University of Colorado, Boulder propose Solar Sail Tubular Mast (SSTM), a lightweight version of our patented High Strain Composite (HSC) Trussed Collapsible Tubular Mast. SSTM represents a paradigm shift in deployable boom technology, poised to set high standards of structural efficiency, deployment simplicity, and cost-effectiveness for deployable boom systems. The SSTM represents a significant advancement in structural capabilities, transitioning from the modest structural efficiency of an open cross-section TRAC boom to the high performance of a trussed tape-spring boom. SSTM enables simple, low-risk solar sails up to the 10,000 m scale and mitigates the need for complex guywire systems, spin-tensioning, or elaborate deployment mechanisms. SSTM also achieves an exceptional mass-to-area ratio of 5 g/m for both the sail and boom components. SSTM booms are also inherently low cost because they are fabricated using automated and mold-based processes that greatly reduce manual/touch labor. SSTM draws from Opterus' rich history of engineering ingenuity and sets a new standard for scalable and efficient space technologies. Through the SSTM, Opterus is equipped to transform large-scale sail systems, for enhanced mission profiles and extended space exploration capabilities. SSTM enables the next generation of large class solar sails for multiple heliophysics missions. SSTM is a lower risk solution because the simplified design minimizes the risk of malfunctions during deployment, ensuring a higher degree of mission success and reliability. The SSTM's inherently stable truss design eliminates the need for other complex stabilization methods and mechanisms, streamlining the deployment process and substantially reducing associated costs. The inherent cost-saving and risk-reducing attributes of an SSTM based system make it both a mass efficient and financially efficient innovation, furthering Opterus' commitment to enabling space missions through advanced engineering solutions. Technical objectives for the Phase II will build off of the accomplishments of the completed Phase I. The program had many successes in analysis, boom rolling and structural tests demonstrating high structural mass efficiency. The boom design achieved in Phase 1 exceeds current system load requirements and has a mass of 88 grams per meter (gpm). For Phase II, we will employ mass optimization algorithms in combination with the analysis process to drive boom mass down into the 50 gpm range. Additional objectives include further development of system level structural models demonstrating the use of SSTM in practical solar sail architectures and tailoring recirculating belt deployer technologies for solar sail systems up to 10,000 sqm, though a smaller 2000 sqm class sail will be the priority for the Phase II effort. The program will consist of an iteration of analysis, design, build, and test tasks. Fabrication and testing of is an important part of the proposed work and Opterus will demonstrate a 30 meter boom as well as methods for testing and characterization of that boom. While the boom design, analysis and testing cycle for a solar cruiser scale system is the primary priority, other priorities include further development of Opterus’ recirculating belt deployer, integrated deployer system level design, thermal system considerations, and scalability to larger solar sail systems.
Benefits: Possible NASA mission infusion includes Solar Cruiser, High Inclination Solar Mission, and Solar Polar Imager. Each NASA solar sail mission concepts require 30m rollable boom systems. The closed cross section SSTM provides higher structural performance than open boom variants or bi-stable closed cross section booms which enable Solar Cruiser and the larger 10,000sqm solar sail mission concepts. The fundamental technology is also readily applied to high power solar arrays required for SEP and moon to mars objectives. Non-NASA applications include high power solar arrays, tensioned planar arrays, and other large area deployable space structures that required large aperture areas and low mass structures. High power solar arrays are a key market fit and the company is developing space solar power beaming structures concepts using similar boom technologies with defense customers.

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