NASA NTRS · 19750010360
High temperature polyimide foams for shuttle upper surface thermal insulation
Abstract
Polyimide foams developed by Monsanto Company were examined for use as upper surface space shuttle thermal insulation. It was found that postcured polyimide foams having a density of 64 kg/cu m (4 lb/cu ft) had acceptable physical properties up to and exceeding 700 K (800 F). Physical tests included cyclic heating and cooling in vacuum, weight and dimensional stability, mechanical strength and impact resistance, acoustic loading and thermal conductivity. Molding and newly developed postcuring procedures were defined.
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Ball, G. L., III, Leffingwell, J. W., Salyer, I. O., Werkmeister, D. W.. 1974-11-01. High temperature polyimide foams for shuttle upper surface thermal insulation. https://ntrs.nasa.gov/citations/19750010360
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