Vibroacoustic and thermal environment data gathered from the first three flights of the space shuttle are presented. The characterization of the particulate, gaseous, and electromagnetic emissions associated with the shuttle flight is emphasized. Measurements of vehicle glow light emissions and material effects (mass loss) due to the low Earth environment interactions with the shuttle vehicle are presented.
Introductory comments
01.02.1983
Aufsatz (Konferenz)
Keine Angabe
Englisch
Online Contents | 2001
|Plansee/JPL/Ceramatec TIM Introductory Comments
NTRS | 2016
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