BRAZE ALLOY STUDIES FOR REFRACTORY METAL SANDWICH STRUCTURES

630252

01/01/1963

Event
Pre-1964 SAE Technical Papers
Authors Abstract
Content
This paper reviews studies to develop vacuum brazing procedures for fabricating D-36 (Cb-10% Ti-5% Zr) columbium and TZM (Mo-0. 5% Ti-0. 07% Zr) molybdenum honeycomb sandwich structures. Braze alloy flow temperatures ranged from 1800° to 3300° F. Higher remelt temperature braze alloy systems, as well as conventional brazing alloys, were investigated. The higher temperature remelt systems show promise but require additional development. Honeycomb sandwich panels which simulate application on an aerospace vehicle, either as hot monocoque structure or as modular heat shields for a double-walled structural concept, were fabricated for evaluation by structural and thermal testing.
Meta TagsDetails
DOI
https://doi.org/10.4271/630252
Pages
14
Citation
McCown, J., Wilks, C., and Gagola, L., "BRAZE ALLOY STUDIES FOR REFRACTORY METAL SANDWICH STRUCTURES," SAE Technical Paper 630252, 1963, https://doi.org/10.4271/630252.
Additional Details
Publisher
Published
Jan 1, 1963
Product Code
630252
Content Type
Technical Paper
Language
English