Citation

Kleinhenz J, Ferkul P, Pettegrew R, Sacksteder KR, T'Ien JS. Fire Mater. 2005; 29(1): 27-37.

Copyright

(Copyright © 2005, John Wiley and Sons)

DOI

unavailable

PMID

unavailable

Abstract

As an experimental necessity. past flame spread studies have relied on fast burning cellulosic papers.. For the longer duration tests planned for the International Space Station a 50% fiberglass. 50% cotton composite fabric is better suited for the novel fuel feeding system in the compact hardware design of a Current microgravity combustion experiment. The fabric's combustion characteristics in normal gravity include unexpected cases where a flame can be sustained on one side of the fuel. One-sided flames are smaller in size than their two-sided counterparts, and propagate at half the speed. Surface temperatur distributions were measured using infrared imaging and indicated a high temperature region caused by the non-flammable fiberglass. Breaching the fiberglass matrix made it possible for the flame to transfer to the other side of the fuel. suggesting that the fiberglass matrix acts as a flame arrester.