Light-Weight, Flexible, High Efficiency Vacuum Photo-Thermo-Voltaic Solar Cells

Award Information
Agency: National Aeronautics and Space Administration
Branch: N/A
Contract: NNX15CC66P
Agency Tracking Number: 154907
Amount: $124,999.00
Phase: Phase I
Program: SBIR
Solicitation Topic Code: H8.03
Solicitation Number: N/A
Timeline
Solicitation Year: 2015
Award Year: 2015
Award Start Date (Proposal Award Date): 2015-06-17
Award End Date (Contract End Date): 2015-12-17
Small Business Information
127 Greyrock PL, Suite 1212, Stamford, CT, 06901-3111
DUNS: 078778247
HUBZone Owned: N
Woman Owned: N
Socially and Economically Disadvantaged: N
Principal Investigator
 Elie Track
 Principal Investigator
 (914) 953-2069
 elie.track@nvizix.com
Business Contact
 Elie Track
Title: Business Official
Phone: (914) 953-2069
Email: elie.track@nvizix.com
Research Institution
N/A
Abstract
Conventional solar cells are limited in efficiency, require heavy weight for high power applications, and tend to degrade rapidly in the harsh radiation environment in space. nVizix LLC proposes to demonstrate a novel concept for high-efficiency solar cells (patent pending), based on the phenomenon of vacuum photoemission (with thermionic enhancement). Recent advances in the technology of optical detectors for high-energy physics (such as photomultiplier tubes), together with manufacturing techniques for flat-panel displays, have enabled a breakthrough in microfabricated solar cell arrays that are broadband and highly efficient, extremely lightweight, as well as extremely resistant to radiation damage and degradation with time. Efficiencies up to 50% are expected (80% theoretical) for space-based solar power. A prototype array of solar panels is proposed, consisting of 8 panels, each the size of a 3U nanosatellite (10 cm x 30 cm). Such an array would provide 150 W of power, while weighing only 100 grams, and being easily stowed, before deployment, inside a small portion of the 3U package. Phase I will demonstrate efficiency and low weight in a small research-scale cell, and project a deployable design for a 120 W array. Phase II will fabricate a prototype array and demonstrate performance at an appropriate NASA laboratory.

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

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