Engineering PapersSearch

NASA NTRS · 19940006918

Polyimide based amorphous silicon solar modules

Abstract

Requirements for space power are increasingly emphasizing lower costs and higher specific powers. This results from new fiscal constraints, higher power requirements for larger applications, and the evolution toward longer distance missions such as a Lunar or Mars base. The polyimide based a-Si modules described are being developed to meet these needs. The modules consist of tandem a-Si solar cell material deposited directly on a roll of polyimide. A laser scribing/printing process subdivides the deposition into discrete cell strips which are series connected to produce the required voltage without cutting the polymer backing. The result is a large, monolithic, blanket type module approximately 30 cm wide and variable in length depending on demand. Current production modules have a specific power slightly over 500 W/Kg with room for significant improvement. Costs for the full blanket modules range from $30/Watt to $150/Watt depending on quantity and engineering requirements. Work to date focused on the modules themselves and adjusting them for the AMO spectrum. Work is needed yet to insure that the modules are suitable for the space environment.

Keep this discovery

Explore connections, maps & timelines

BibTeXRIS

Jeffrey, Frank R., Grimmer, Derrick P., Martens, Steven A., Abudagga, Khaled, Thomas, Michael L., Noak, Max. 1993-05-01. Polyimide based amorphous silicon solar modules. https://ntrs.nasa.gov/citations/19940006918

Cite the original work for its findings. Save a collection to share your selection of sources.