Hostname: page-component-586b7cd67f-2brh9 Total loading time: 0 Render date: 2024-11-23T12:31:53.102Z Has data issue: false hasContentIssue false

Space Shuttle Main Engine Hydrogen Pump Impeller Residual Stress Measurements Using Pars (Portable Apparatus for Measurement of Residual Stress)

Published online by Cambridge University Press:  06 March 2019

E. B. S. Pardue
Affiliation:
Technology for Energy Corp. Knoxville, TN 37922
M. V. Mathis
Affiliation:
Technology for Energy Corp. Knoxville, TN 37922
R. W. Hendricks
Affiliation:
Technology for Energy Corp. Knoxville, TN 37922
E. M. Stangeland
Affiliation:
Rockwell International Rocketdyne Division Canoga Park, CA 91304
Get access

Extract

X-ray residual stress analysis was performed on four space shuttle hydrogen pump impellers made from Ti-5Al-2,5Sn alloy. Five locations on the outer rim, near the vanes, were measured on each impeller, identified as #1, #2,#3, and #4. Impellers #1 and #4 were test-fired impellers, impeller #2 was a new impeller that had been spin tested, and impeller #3 was a new impeller that had not teen spin tested. The measurement locations on these impellers corresponded to areas of critical stress importance. The purpose of the measurements was to compare the stresses at these locations as a function of impeller processing variables. A description of the Impellers, the test parameters and procedures, stress analysis results, and a technical discussion of these results are presented in this report.

A description of the Impellers, the test parameters and procedures, stress analysis results, and a technical discussion of these results are presented in this report.

Type
Research Article
Copyright
Copyright © International Centre for Diffraction Data 1985

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)