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Lightweight Solar Power for Small SatellitesThe innovation targets small satellites or CubeSats for which conventional deployable arrays are not feasible due to their size, weight and complexity. This novel solar cell array includes a thin and flexible photovoltaic cell applied to an inflatable structure to create a high surface area array for collecting solar energy in a lightweight, simple and deployable structure. The inflatable array, with its high functional surface area, eliminates the need and the mechanisms required to point the system toward the sun. The power density achievable in these small arrays is similar to that of conventional high-power deployable/pointable arrays used on large satellites or space vehicles. Although inflatable solar arrays have been previously considered by others, the arrays involved the use of traditional rigid solar cells. Researchers are currently working with thin film photovoltaics from various suppliers so that the NASA innovation is not limited to any particular solar cell technology. NASA has built prototypes and tested functionality before and after inflation. As shown in the current-voltage currents below, deployment does not damage the cell performance.
Document ID
20150002932
Acquisition Source
Marshall Space Flight Center
Document Type
Other
Authors
Nabors, Sammy A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
March 13, 2015
Publication Date
January 1, 2015
Subject Category
Spacecraft Design, Testing And Performance
Spacecraft Propulsion And Power
Report/Patent Number
M15-4377
Report Number: M15-4377
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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