Accession Number:

AD0862749

Title:

Temperature Shock Test of a Two-Inch Bolted Flange Joint.

Descriptive Note:

Technical rept.,

Corporate Author:

AIR FORCE ROCKET PROPULSION LAB EDWARDS AFB CA

Personal Author(s):

Report Date:

1969-05-01

Pagination or Media Count:

33.0

Abstract:

The Battelle Memorial Institute-developed flange design procedure was converted for use with the IBM 7040 computer. The flange design program was used to design a two flanged fluid tubing joint for use with a line mounted liquid fluorine shutoff valve. The flange was fabricated, prepared for test, and subjected to a series of temperature shocks. No measurable leakage was noted after five temperature shocks averaging 131Fminute with a maximum temperature gradient of 350Fminute. Author

Subject Categories:

  • Couplers, Fasteners and Joints

Distribution Statement:

APPROVED FOR PUBLIC RELEASE