Leak detection of the Space Station Freedom U.S. Lab vacuum system using reverse flow leak detection methodologyA vacuum system leak detection technique (reverse flow leak detection) under development for use aboard Space Station Freedom is presented. The technique will be applied to the Vacuum System (VS) and Waste Gas Management Subsystem (WGMS) of the U.S. Lab Module. These two systems contain over 45.7 m of distributed vacuum tubing located in remote utility runs. Fluid flow calculations which utilize known system geometry and measured steady state pressure measurements from the VS and WGMS can be used to identify leak sites within +/- 38 cm. Exact leak position can then be pinpointed by conventional tracer gas leak detection in the identified region. Tests have been performed using a simple, unrestricted 12.8 m length of vacuum tubing with a calibrated air leak attached.
Document ID
19920048749
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Moore, Jeffrey D. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Shepherd, James E. (NASA Marshall Space Flight Center Huntsville, AL, United States)
Masden, Darrell E. (Teledyne Brown Engineering Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Subject Category
Man/System Technology And Life Support
Report/Patent Number
SAE PAPER 911456Report Number: SAE PAPER 911456
Meeting Information
Meeting: International Conference on Environmental Systems