In one or more embodiments, the present disclosure teaches a method for reconfiguring a solar array. The method involves providing, for the solar array, at least one string of solar cells. The method further involves deactivating at least a portion of at least one of the strings of solar cells of the solar array when power produced by the solar array reaches a maximum power allowance threshold. In addition, the method involves activating at least a portion of at least one of the strings of the solar cells in the solar array when the power produced by the solar array reaches a minimum power allowance threshold.
On-orbit reconfigurable solar array
14.11.2017
Patent
Elektronische Ressource
Englisch
IRS-1A Solar Array In-Orbit Performance
British Library Conference Proceedings | 1995
|IRS-1A Solar Array In-Orbit Performance
British Library Online Contents | 1995
|