This is a closed form solution for the longitudinal oscillation of the Solar Array Flight Experiment (SAFE) blanket for all phases of deployment. The frequency response shows that the blanket frequency increases shortly before full deployment. That fact causes a coupling between the mast and the blanket frequency but, because of the relatively high speed of deployment, a buildup of resonance is unlikely.
Solar Array Flight Experiment
1985
17 pages
Report
No indication
English
Solar Array Flight Experiment (SAFE)
NTRS | 1982
|NASA solar array flight experiment
NTRS | 1982
|Solar Array Flight Dynamic Experiment
NTIS | 1987
|Solar array flight dynamic experiment
NTRS | 1986
|Solar array flight dynamic experiment
NTRS | 1986
|