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Fire behavior and risk analysis in spacecraftPractical risk management for present and future spacecraft, including space stations, involves the optimization of residual risks balanced by the spacecraft operational, technological, and economic limitations. Spacecraft fire safety is approached through three strategies, in order of risk: (1) control of fire-causing elements, through exclusion of flammable materials for example; (2) response to incipient fires through detection and alarm; and (3) recovery of normal conditions through extinguishment and cleanup. Present understanding of combustion in low gravity is that, compared to normal gravity behavior, fire hazards may be reduced by the absence of buoyant gas flows yet at the same time increased by ventilation flows and hot particle expulsion. This paper discusses the application of low-gravity combustion knowledge and appropriate aircraft analogies to fire detection, fire fighting, and fire-safety decisions for eventual fire-risk management and optimization in spacecraft.
Document ID
19890000740
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Friedman, Robert
(NASA Lewis Research Center Cleveland, OH, United States)
Sacksteder, Kurt R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
January 1, 1988
Subject Category
Space Transportation
Report/Patent Number
E-4232
NASA-TM-100944
NAS 1.15:100944
Report Number: E-4232
Report Number: NASA-TM-100944
Report Number: NAS 1.15:100944
Meeting Information
Meeting: Winter Annual Meeting of the American Society of Mechanical Engineers
Location: Chicago, IL
Country: United States
Start Date: November 28, 1988
End Date: December 3, 1988
Accession Number
89N10111
Funding Number(s)
PROJECT: RTOP 323-53-6X
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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