Publication Date:
2019-07-13
Description:
Characterization of the smoke from pyrolysis of common spacecraft materials provides insight for the design of future smoke detectors and post-fire clean-up equipment on the International Space Station. A thermal precipitator was designed to collect smoke aerosol particles for microscopic analysis in fire characterization research. Information on particle morphology, size and agglomerate structure obtained from these tests supplements additional aerosol data collected. Initial modeling for the thermal precipitator design was performed with the finite element software COMSOL Multiphysics, and includes the flow field and heat transfer in the device. The COMSOL Particle Tracing Module was used to determine particle deposition on SEM stubs which include TEM grids. Modeling provided optimized design parameters such as geometry, flow rate and temperatures. Microscopy results from fire characterization research using the thermal precipitator are presented.
Keywords:
Fluid Mechanics and Thermodynamics
Type:
E-18543
,
GRC-E-DAA-TN6021
,
31st Annual American Association for Aerosol Research {AAAR) Conference; Oct 08, 2012 - Oct 12, 2012; Minneapolis, MN; United States
Format:
application/pdf
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