SBIR/STTR Research Award

A Path to Low-Cost Space Solar Arrays Based on Si Blankets and In-Orbit Array Construction

Award identifier 85e637cab1617a33db1e27707a046c300f55e65bc8a3dcec9ac5ff7ab70490c0Awarding agency National Aeronautics and Space Administration

Award amount

$124,743

Program and phase

SBIR · Phase I

Award year

2019

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
SOLESTIAL, INC.
Proposal award date
2019-08-19
Contract end date
2020-02-18
UEI
DBWMUS4BBNP1
Solicitation number
SBIR_19_P1
Topic code
S3

Research abstract

NASA has vital interest in photovoltaic power system developments for high-power solar electric propulsion missions. Technology Roadmaps state a need for 25-150 kW to 1 MW space solar arrays for electric propulsion systems and planetary surface elements. Target performance metrics include gt;100W/kg specific power and gt;40kW/m3 stowed volume efficiency.nbsp;The problem of realizing such arrays are twofold: (i) High cost. Solar cell/array technologies can deliver such power density, but at unacceptable $1,000/W cost. (ii) Deployment of very large solar arrays. The largest array in space on the ISS consists of eight 15 kW units totaling 120kW power. Space Shuttle was used for installation and stowed volume efficiency was only 12 kW/m3.nbsp;In this project Regher Solar and ldquo;Made In Spacerdquo; propose a novel approach to large space solar arrays, that reduces system cost 10X, and delivers 100kW/m3 stowed volume efficiency by combining a solar blanket based on Regherrsquo;s ultrathin silicon solar cells and robotic system, that manufactures solar array frame on-orbit from raw materials and deploys solar blankets on the frame.nbsp;Advantages compared to baseline solar blanket/deployment technologies include: (1) decoupled solar blanket design from the array design and automated mass production of solar blanket, that fits a variety of arrays; (2) high stowed volume efficiency gt;100 W/m3 due to no need in mechanical deployment systems.nbsp;Phase I will validate modular solar blanket technology. A prototype mini-blanket will be designed, fabricated and tested by Regher. Made-in-Space will identify the materials suitable for in-situ solar array frame construction, design the frame for different array sizes, estimate the final array cost.nbsp;Phase II will (i)fabricate full-size blankets and demonstrate in-situ manufacturing of the array prototype in the Lab on Earth, (ii)plan the experiment in space, (iii)partner with customers for alpha testing in space.

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

12 SBIR/STTR records share this UEI (2018–2025). Reported award amounts total $5,024,850. Reported amounts are not federal obligations.

Phases: Phase I, Phase II, Phase II – Direct to Phase II

Agencies: National Aeronautics and Space Administration, Department of Defense, National Science Foundation

Agency intelligence

National Aeronautics and Space Administration

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