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Fire suppression in human-crew spacecraftFire extinguishment agents range from water and foam in early-design spacecraft (Halon 1301 in the present Shuttle) to carbon dioxide proposed for the Space Station Freedom. The major challenge to spacecraft fire extinguishment design and operations is from the micro-gravity environment, which minimizes natural convection and profoundly influences combustion and extinguishing agent effectiveness, dispersal, and post-fire cleanup. Discussed here are extinguishment in microgravity, fire-suppression problems anticipated in future spacecraft, and research needs and opportunities.
Document ID
19910011869
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Friedman, Robert
(NASA Lewis Research Center Cleveland, OH., United States)
Dietrich, Daniel L.
(Sverdrup Technology, Inc., Brook Park OH., United States)
Date Acquired
September 6, 2013
Publication Date
May 1, 1991
Subject Category
Space Transportation
Report/Patent Number
E-6100
NASA-TM-104334
NAS 1.15:104334
Report Number: E-6100
Report Number: NASA-TM-104334
Report Number: NAS 1.15:104334
Meeting Information
Meeting: Halon Alternatives Technical Working Conference
Location: Albuquerque, NM
Country: United States
Start Date: April 30, 1991
End Date: May 1, 1991
Sponsors: New Mexico Univ., Center for Global Environmental Technologies
Accession Number
91N21182
Funding Number(s)
PROJECT: RTOP 323-53-62
CONTRACT_GRANT: NAS3-25266
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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