SBIR/STTR Research Award

High Capacity Multi-Stage Scroll Compressor for Mars Atmosphere Acquisition

Award identifier 99962e7ab07da0b20cec577fd54e50f160d6296d28a7b9b054751476a31d5763Awarding agency National Aeronautics and Space Administration

Award amount

$124,673

Program and phase

SBIR · Phase I

Award year

2017

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Air Squared, Inc.
Proposal award date
2017-06-09
Contract end date
2017-12-08
UEI
N71MUPCNM3J1
Solicitation number
Not reported
Topic code
H1.01

Research abstract

There are several ways to capture and pressurize CO2, including freezing at cryogenic temperatures, mechanical compression, and absorption. Completed studies on each approach, have generally favored cryogenic temperature and mechanical compression solutions. Recently, mechanical compression has gained momentum through the Mars Oxygen ISRU Experiment (MOXIE), which utilizes an Air Squared compressor for mechanical compression of CO2. If this approach is pursued further for a larger system, there are still several questions concerning reliability over 10,000 hours of autonomous operation in Mars environment and scalability. Air Squared plans on addressing these issues as part of Phase I. Air Squared proposes the development of a Multi-Stage Scroll Compressor (MSSC) that will be configured to support a store-and-utilize strategy (high pressure) or a collection-only strategy (high flow). If a store-and-utilize approach is required, the MSSC will be set up to pressurize the gas over the triple point (>77 PSIA), which provides the ability to liquefy CO2 downstream of the MSSC as it cools, while N2 and Ar remain a gas. If only collection is necessary, the MSSC will be configured to maximize flow at a pressure above 15 PSIA. There will be two ?types? of MSSCs pursued during the Phase I, an orbiting and spinning MSSC. The orbiting MSSC has the advantage of longer design heritage and lowers associated risk, as this scroll configuration is widely used at Air Squared and the compressor industry as a whole. The spinning MSSC has the advantage of achieving an aggressive size and weight target but has little design heritage. The orbiting MSSC and spinning MSSC both have substantial advancement over state of the art mechanical compression technologies, such as high-speed turbo-compressors. Size, weight, and power requirements are all reduced. Reliability is also improved, as both MSSCs operate at significantly lower speeds than turbo-compressors.

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

31 SBIR/STTR records share this UEI (2013–2023). Reported award amounts total $14,325,465. Reported amounts are not federal obligations.

Phases: Phase I, Phase II

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

Agency intelligence

National Aeronautics and Space Administration

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