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- (Nov. 6, 1997) Sense wire tensions in Superlayer 2 for 0, 500, and 1300 hours after
installation as a histogram and scatter plot
- (Nov. 6, 1997) Tension measurements from superlayer QC using the 32-pin twanger for
Superlayer 1, 2, 3, 4, 5,
6, and 7
- (Sep. 12, 1997) Graph of drift chamber stringing progress
(or "integrated stringosity"). Updated frequently.
- New study of annealing temperature dependence for
elongation of 80 micron aluminum wire. From C. Lu (Aug. 6, 1997)
- New study of annealing temperature dependence for
yield of 80 micron aluminum wire. From C. Lu (Aug. 6, 1997)
- Summary of annealing temperature dependence for
yield, creep, and elongation properties of aluminum wire. From C. Lu (Aug. 6, 1997)
- Failure tension as a function of crimp size for pre-tension values of 300 and 265 grams for 120 mu aluminum. From P. Bloom
(Aug. 6, 1997)
- Failure tension as a function of crimp size for pre-tension values of 225 and 0 grams for 120 mu aluminum. From P. Bloom (Aug.
6, 1997)
- Procurement of Gold-Plated
Aluminum Wire for the BABAR Drift Chamber, K. McDonald (10kB, Sept. 19, 1996)
- Directory of QC/QA software for stringing (31 Oct 1996). This
directory replaces proto_qc/, and contains source code, Make file, etc., for the
QC/QA data collection software to be used during stringing, M. Kelsey (Nov 4, 1996)
- Draft version of stringing procedure for
prototype II. See also TNDC-96-30. From C. Hearty (Aug. 22, 1996)
- Draft description of automated tooling for DCH review from N.
Ferroni (June 21, 1996)
- Arguments in favour of stringing with the outer wall
in place by Adam Boyarski (August 30, 1995)
- Wire loads for former baseline hex4 design with
40:46:86 gram tensions on sense and field wires by C. Hearty (September 26, 1995)
- Wire loads for former baseline hex4 design with
nominal 40:61:118 gram tensions on sense and field wires by C. Hearty (August 28, 1995)
- Concept for quality control presented at December 1995
collaboration meeting by M. McDougald (Dec 1995)
For comments, questions or changes to this page contact David MacFarlane
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