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A User's Guide for the Spacecraft Fire Safety FacilityThe Spacecraft Fire Safety Facility (SFSF) is a test facility that can be flown on NASA's reduced gravity aircraft to perform various types of combustion experiments under a variety of experimental conditions. To date, this facility has flown numerous times on the aircraft and has been used to perform experiments ranging from an examination of the effects transient depressurization on combustion, to ignition and flame spread. A list of pubfications/presentations based on experiments performed in the SFSF is included in the reference section. This facility consists of five main subsystems: combustion chamber, sample holders, gas flow system, imaging system, and the data acquisition/control system. Each of these subsystems will be reviewed in more detail. These subsystems provide the experiment operator with the ability to monitor and/or control numerous experimental parameters.
Document ID
20000120369
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Goldmeer, Jeffrey S.
(National Academy of Sciences - National Research Council Cleveland, OH United States)
Date Acquired
September 7, 2013
Publication Date
August 1, 2000
Subject Category
Space Processing
Report/Patent Number
E-12429
NASA/TM-2000-210375
NAS 1.15:210375
Report Number: E-12429
Report Number: NASA/TM-2000-210375
Report Number: NAS 1.15:210375
Funding Number(s)
PROJECT: RTOP 101-42-0B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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