NASA NTRS · 19910036966
Reusable surface insulations for reentry spacecraft
Abstract
A family of ceramic, reusable surface insulations developed for the thermal protection of reentry vehicles is discussed. Their thermal properties are summarized and their thermal capabilities are compared. The insulation requirements for the Personnel Launch System are evaluated.
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Chiu, S. Amanda, Pitts, William C.. 1991-01-01. Reusable surface insulations for reentry spacecraft. https://ntrs.nasa.gov/citations/19910036966
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