19 February 1982 Mass Loss Parameters For Typical Shuttle Materials
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Proceedings Volume 0287, Shuttle Optical Environment; (1982) https://doi.org/10.1117/12.932002
Event: 1981 Technical Symposium East, 1981, Washington, D.C., United States
The weight loss of twenty different typical Shuttle materials was measured with a thermogravimetric analyzer as the material temperature was increased from ambient to 300°C. An additional ten tests were performed where conditioning of the material varied. The materials were selected from each general grouping such as adhesives, coatings, lubricants, encapsulants, elastomers, and resins. Care was taken in the preparation, curing, and preconditioning of the materials to simulate flight use. Making the assumption that the weight loss follows first order rate theory, the source outgassing parameters for these thirty materials is presented.
© (1982) COPYRIGHT Society of Photo-Optical Instrumentation Engineers (SPIE). Downloading of the abstract is permitted for personal use only.
J. A. Muscari, J. A. Muscari, T. O'Donnell, T. O'Donnell, } "Mass Loss Parameters For Typical Shuttle Materials", Proc. SPIE 0287, Shuttle Optical Environment, (19 February 1982); doi: 10.1117/12.932002; https://doi.org/10.1117/12.932002

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