High Temperature Metallic Fabric for Re-Entry Applications

620337

01/01/1962

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
Materials used in expandable structures for aerospace missions must be flexible, have high temperature resistance, and show high strength-weight ratios. This article discusses the development and technology of such materials and their use with the various categories of space vehicles.
Meta TagsDetails
DOI
https://doi.org/10.4271/620337
Pages
6
Citation
Harris, J., "High Temperature Metallic Fabric for Re-Entry Applications," SAE Technical Paper 620337, 1962, https://doi.org/10.4271/620337.
Additional Details
Publisher
Published
Jan 1, 1962
Product Code
620337
Content Type
Technical Paper
Language
English