SBIR/STTR Research Award

Sunflake Extra Linear

Award identifier fc180e353b1ebc68b6ee8218982ad5f8d428c46601fc7cf89bf3b7955ee262e7Awarding agency National Aeronautics and Space Administration

Award amount

$899,612

Program and phase

SBIR · Phase II

Award year

2024

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Gendell Associates P.A. DBA Folditure DBA Folditure Space
Proposal award date
2024-07-05
Contract end date
2026-07-04
UEI
FWP5NCLAVK31
Solicitation number
SBIR_23_P2
Topic code
H5

Research abstract

Combining our proprietary Pyramid Hinge Array, with other novel mechanical and geometric solutions, we propose a disruptively compact, robust structure for Lunar Solar Power Generation ndash; The Sunflake XL array, and Ultra Compact Quad Tower (UC4T) nbsp; Sunflake XL delivers a 175msup2; ultra compact Lunar Surface Solar Array, capable of delivering 50kW of power. The solar array raises up to 10 meters off the ground (achieving a total height of 17m). Sunflake XL rotates for optimal sun tracking, while the UC4T provides a stable vertical structure. nbsp; Combined together with the tower and rover-deployment system, the entire package will deliver a performance of 113 W/kg and 26 kW/m3. The system is ultra compact, lightweight, stable, and retractable. nbsp; Most important, it is based on our proven pyramid hinge technology, making it a reliable and robust solution. The novel design combines the strength, compactness, and durability of the Pyramid Hinge, with linear expanding array elements, adding a new dimension of scalability to our Sunflake solutions. The novel mechanisms can also be re-configured for different deployable solutions: antennas, reflectors, or radiators. nbsp; With a linear arm segment measuring only 2.6 m, the new design opens a new spectrum of opportunities for pyramid-hinge based designs. nbsp; In Phase I Folditure validated the design, packing efficiency, scalability, and retractability of the mechanism, through detailed mechanical drawings, analysis, and a functional prototype. nbsp; In Phase II we propose to fully develop the kinematics and structure. We plan to engineer, and build a very large-scale high fidelity kinematic prototype, while further developing, and applying the best available technologies. The design will be also proven through FEM analyses, and environmental testing. We also propose to field test the prototype deployment, with anbsp;lunar rover. This project is very well aligned with our area of expertise: developing super-compact novel folding solutions.

Technology keywords

Not reported

Other awards by this recipient

Verified by the same UEI. These are other public SBIR/STTR award pages, not a merged company record.

Research funding history

4 SBIR/STTR records share this UEI (2021–2024). Reported award amounts total $1,973,024. Reported amounts are not federal obligations.

Phases: Phase II, Phase I

Agencies: National Aeronautics and Space Administration

Agency intelligence

National Aeronautics and Space Administration

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