NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Plasma arc welding repair of space flight hardwareRepair and refurbishment of flight and test hardware can extend the useful life of very expensive components. A technique to weld repair the main combustion chamber of space shuttle main engines has been developed. The technique uses the plasma arc welding process and active cooling to seal cracks and pinholes in the hot-gas wall of the main combustion chamber liner. The liner hot-gas wall is made of NARloyZ, a copper alloy previously thought to be unweldable using conventional arc welding processes. The process must provide extensive heat input to melt the high conductivity NARloyZ while protecting the delicate structure of the surrounding material. The higher energy density of the plasma arc process provides the necessary heat input while active water cooling protects the surrounding structure. The welding process is precisely controlled using a computerized robotic welding system.
Document ID
19940011666
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hoffman, David S.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
January 1, 1993
Publication Information
Publication: Huntsville Association of Technical Societies, TABES 1993: 9th Annual Technical and Business Exhibition and Symposium
Subject Category
Mechanical Engineering
Report/Patent Number
TABES PAPER 93-603
Accession Number
94N16139
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available