SBIR/STTR Research Award

Orbital Pump for Microgravity Applications

Award identifier 30bb386b30f0ae7b583fd97a27d135def9935d9f345b543777ef0d67b52af023Awarding agency National Aeronautics and Space Administration

Award amount

$69,990

Program and phase

SBIR · Phase I

Award year

2003

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Award details

Awarding agency
National Aeronautics and Space Administration
Branch
Not reported
Recipient company
Fluid Flow Technologies, LLC
Proposal award date
Not reported
Contract end date
Not reported
UEI
Not reported
Solicitation number
Not reported
Topic code
Not reported

Research abstract

This proposed work will develop a new pump design, which is based on a uniquely generated orbital motion. The pump is intrinsically sealed and mechanically balanced, resulting in quiet, safe operation. The pump design has no seals, valves, bearings, complex mechanical linkages, or drive motor. Its simplicity promises to provide a pump, which is compact and reliable, has low mass, and possesses quiet, safe operation, ideal for long-term, space-based, microgravity applications.

Technology keywords

Not reported

Agency intelligence

National Aeronautics and Space Administration

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