SBIR/STTR Research Award

Lunar Articulating Mirror Array

Award identifier 9881099ef1788b9958d0a9442ba248298ef6932ac573955e8f5fcdabcd89f586Awarding agency National Aeronautics and Space Administration

Award amount

$899,698

Program and phase

SBIR · Phase II

Award year

2023

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
BLUESHIFT LLC
Proposal award date
2023-05-12
Contract end date
2025-05-11
UEI
JX78FHVFSHY3
Solicitation number
SBIR_22_P2
Topic code
Z14

Research abstract

Blueshift, LLC d/b/a Outward Technologies proposes to continue development of a Lunar Articulating Mirror Array (LAMA) for enabling lunar surface construction of large-scale infrastructure. The technology utilizes concentrated solar power to heat lunar regolith at a distance of meters to tens of meters from the mirror array. The configuration of the design allows for precise control over the solar flux and solar flux density delivered to the target surface. Phase I demonstrated feasibility of this technology through fabrication, assembly, and control of a physical prototype demonstrating the translation of a spot of highly concentrated solar energy across a receiver surface; ray tracing models matched to Phase I prototype results confirming validity of these models; extension of the ray tracing models to mid- to large-scale LAMA systems for solar conditions found on the Moon; generation of selectively solar melted and liquid-phase sintered surfaces of a lunar highlands regolith simulant; evaluation of performance of selectively solar melted surfaces for bearing loads equivalent to those that would be imposed by a lander footpad; and evaluation of reducing ejecta from selectively solar sintered regolith surfaces when exposed to a simulated plume-surface interaction. These efforts will be extended in Phase II to develop a medium-fidelity LAMA prototype and evaluate its performance in a relevant test environment to advance the TRL from 4 to 5. Selectively solar melted and sintered regolith surfaces will be produced in air and in vacuum conditions. Specimens generated from selective solar melting will be exposed in controlled thermal pulse tests representing impingement by superheated gases from an 80 ton lunar lander. Plume-surface interactions of selective solar sintered surfaces will be explored in vacuum conditions. Finally, a demonstration Landing/Launch Pad measuring 1m in diameter will be evaluated through multiple hot-fire tests from a large solid rocket motor.

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.

Awards with the same topic code

Verified by an exact topic code match. This is not a text-similarity match.

Research funding history

23 SBIR/STTR records share this UEI (2019–2025). Reported award amounts total $9,887,089. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

Agencies: National Aeronautics and Space Administration, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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