The NASA large flexible solar array space shuttle flight experiment is described. The 32 x 4 m wing is deployed from the shuttle bay, and experiments in electrical output, multiple deployment, and structural dynamics are planned. Both 2 x 4 cm and 5.9 x 5.9 cm cell assemblies on the array blanket are evaluated. Safety/hazards provisions are described, including emergency jettison provisions. Ground testing and hardware fabrication are summarized.
NASA solar array flight experiment
1982-06-01
Conference paper
No indication
English
NTIS | 1985
|Solar Array Flight Experiment (SAFE)
NTRS | 1982
|Solar array flight dynamic experiment
NTRS | 1986
|Solar array flight dynamic experiment
NTRS | 1987
|Solar Array Flight Dynamic Experiment
NTIS | 1986
|