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Evaluation of Containment Boxes as a Fire Mitigation Method in Elevated Oxygen ConditionsNASA performed testing to evaluate the efficacy of fire containment boxes without forced ventilation. Configurational flammability testing was performed on a simulation avionics box replicating critical design features and filled with materials possessing representative flammability characteristics. This paper discusses the box's ability, under simulated end-use conditions, to inhibit the propagation of combustion to surrounding materials. Analysis was also performed to evaluate the potential for the fire containment box to serve as an overheat/ignition source to temperature sensitive equipment (such as items with lithium-ion batteries). Unrealistically severe combustion scenarios were used as a means to better understand the fire containment mechanism. These scenarios were achieved by utilizing materials/fuels not typically used in space vehicles due to flammability concerns. Oxygen depletion, during combustion within the fire containment boxes, drove self-extinguishment and proved an effective method of fire containment
Document ID
20160001180
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Juarez, Alfredo
(Jacobs Engineering Group, Inc. Las Cruces, NM, United States)
Harper, Susana
(NASA White Sands Test Facility NM, United States)
Perez, Horacio
(Lockheed Martin Corp. Houston, TX, United States)
Date Acquired
January 26, 2016
Publication Date
April 13, 2016
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
JSC-CN-35121
STP-2015-0079
Report Number: JSC-CN-35121
Report Number: STP-2015-0079
Meeting Information
Meeting: International Symposium on Flammability and Sensitivity of Materials in Oxygen-Enriched Atmospheres
Location: San Antonio, TX
Country: United States
Start Date: April 13, 2016
End Date: April 15, 2016
Sponsors: ASTM International
Distribution Limits
Public
Copyright
Public Use Permitted.
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