NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Nondestructive tests of regenerative chambersThe capabilities and limitations of nondestructive evaluation methods were studied to detect and locate bond deficiencies in regeneratively cooled thrust chambers for rocket engines. Flat test panels and a cylinder were produced to simulate regeneratively cooled thrust chamber walls. Planned defects with various bond integrities were produced in the panels to evaluate the sensitivity, accuracy, and limitations of nondestructive methods to define and locate bond anomalies. Holography, acoustic emission, and ultrasonic scan were found to yield sufficient data to discern bond quality when used in combination and in selected sequences. Bonding techniques included electroforming and brazing. Materials of construction included electroformed nickel bonded to Nickel 200 and OFHC copper, electroformed copper bonded to OFHC copper, and 300 series stainless steel brazed to OFHC copper. Variations in outer wall strength, wall thickness, and defect size were evaluated for nondestructive test response.
Document ID
19750003986
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Malone, G. A.
(Bell Aerospace Co. Buffalo, NY, United States)
Vecchies, L.
(Bell Aerospace Co. Buffalo, NY, United States)
Wood, R.
(Bell Aerospace Co. Buffalo, NY, United States)
Date Acquired
September 3, 2013
Publication Date
June 1, 1974
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
NASA-CR-134656
BAC-8654-953005
Report Number: NASA-CR-134656
Report Number: BAC-8654-953005
Accession Number
75N12058
Funding Number(s)
CONTRACT_GRANT: NAS3-16800
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available