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Miniaturized Sensor Array Platform for Monitoring Calcium, Conductivity, and pH in Urine Brine

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX16CJ24P
Agency Tracking Number: 156341
Amount: $124,127.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: H3.01
Solicitation Number: N/A
Timeline
Solicitation Year: 2016
Award Year: 2016
Award Start Date (Proposal Award Date): 2016-06-10
Award End Date (Contract End Date): 2016-12-09
Small Business Information
220-3 Reservoir Street
Needham Heights, MA 02494-3133
United States
DUNS: 000000000
HUBZone Owned: No
Woman Owned: Yes
Socially and Economically Disadvantaged: No
Principal Investigator
 Ranganathan Shashidhar
 Senior Vice President
 (781) 449-2284
 rshashidhar@polestartech.com
Business Contact
 Karen Carpenter
Title: CEO
Phone: (781) 449-2284
Email: kcarpenter@polestartech.com
Research Institution
N/A
Abstract

In response to NASA SBIR Topic H3.01, Polestar Technologies Inc. proposes to develop a miniaturized sensor array platform for simultaneous monitoring of calcium, conductivity and pH in urine brine suitable for the international space station (ISS). The sensor platform will incorporate three different types of sensors: i) molecular recognition sensor elements incorporated onto nano-architecture for calcium detection, ii) Doped electronic material for pH measurement, and iii) a suitably designed microelectrode structure for conductivity determination. Phase I project will involve design and fabrication of the first generation sensor platform consisting of an electrochemical part (for calcium studies) and electronic part (for both pH and conductivity measurements). The capability of this platform to measure calcium in the range of 50-400mg/L, pH in the range of 0.5-5.0 and conductivity in the range of 10-250mS/cm will be demonstrated. In Phase II all the three types of sensor modalities will be integrated into a common platform. In addition, a handheld electronic readout unit will also be designed and fabricated in Phase II. This will serve as a basis for the development of a rugged detection system for applications on ISS.

* Information listed above is at the time of submission. *

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