The present invention relates to a semi-rigid solar panelv(100) for a spacecraft comprising a frame; and one or more solar power modules (103) placed within the frame; wherein at least one side of the one or more solar power modules (103) connects to the frame by a sliding connection, allowing the one or more solar power modules (103) to slide within the frame.
SEMI-RIGID SOLAR PANEL ARRAY
HALBSTARRE SOLARPANEELANORDNUNG
RÉSEAU DE PANNEAUX SOLAIRES SEMI-RIGIDE
25.06.2025
Patent
Elektronische Ressource
Englisch
IPC: | B64G Raumfahrt , COSMONAUTICS |
Deployment and Retraction of a Cable-Driven Rigid Panel Solar Array
Online Contents | 1996
|