BRAZE ALLOY STUDIES FOR REFRACTORY METAL SANDWICH STRUCTURES Space Systems Division--Martin Company Baltimore 3, Maryland

Format:

Conference/Event

Author/Creator:

McCown, J. W., author.

Conference Name:

National Aero-Nautical Meeting

Language:

English

Physical Description:

1 online resource

Place of Publication:

Warrendale, PA SAE International 1963

Summary:

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

Notes:

Vendor supplied data

Publisher Number:

630252

Access Restriction:

Restricted for use by site license