Advanced Space Suit Insulation Feasibility Study

2000-01-2479

07/10/2000

Event
International Conference On Environmental Systems
Authors Abstract
Content
For planetary applications, the space suit insulation has unique requirements because it must perform in a dynamic mode to protect humans in the harsh dust, pressure and temperature environments. Since the presence of a gaseous planetary atmosphere adds significant thermal conductance to the suit insulation, the current multi-layer flexible insulation designed for vacuum applications is not suitable in reduced pressure planetary environments such as that of Mars. Therefore a feasibility study has been conducted at NASA to identify the most promising insulation concepts that can be developed to provide an acceptable suit insulation. Insulation concepts surveyed include foams, microspheres, microfibers, and vacuum jackets. The feasibility study includes a literature survey of potential concepts, an evaluation of test results for initial insulation concepts, and a development philosophy to be pursued as a result of the initial testing and conceptual surveys. The recommended focus is on microfibers due to the versatility of fiber structure configurations, the wide choice of fiber materials available, the maturity of the fiber processing industry, and past experience with fibers in insulation applications.
Meta TagsDetails
DOI
https://doi.org/10.4271/2000-01-2479
Pages
11
Citation
Trevino, L., and Orndoff, E., "Advanced Space Suit Insulation Feasibility Study," SAE Technical Paper 2000-01-2479, 2000, https://doi.org/10.4271/2000-01-2479.
Additional Details
Publisher
Published
Jul 10, 2000
Product Code
2000-01-2479
Content Type
Technical Paper
Language
English