International Journal of Microgravity Science and Application
Online ISSN : 2188-9783
Cool Flame Spread Behavior near Spontaneous Ignition Limit along n-Decane Droplet Array under Microgravity by a TEXUS Rocket
Masanori SAITO Yusuke SUGANUMAKazuki IEMURAYusei TAKAHATANoelia MARTÍNEZ FIGUEIRAFlorian MEYERChristian EIGENBRODHiroshi NOMURAMitsuaki TANABE
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JOURNAL OPEN ACCESS

2025 Volume 42 Issue 3 Pages 420302-

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Abstract
A microgravity experiment to elucidate the cool flame dynamics in a multi-droplet system was conducted using the TEXUS-60 sounding rocket. The cool flame position was successfully observed through formaldehyde chemiluminescence. This allowed the study of cool flame propagation speed along n-decane droplet arrays, with droplet spacings of 8 mm (nine droplets) and 16 mm (five droplets). The spread speed was analyzed at an ambient temperature of 570 K and a pressure of 0.1 MPa, using air as the ambient gas. For both droplet configurations, the cool flame occurred from nearly the same position 4.7 s after the droplet was inserted and settled at the combustion position. The cool flame spread speeds decreased from around 250 mm/s to approximately 100 mm/s after the spontaneous ignition, and then increased. The maximum speed reached around 600 mm/s for the 16 mm droplet spacing case. Under these experimental conditions, the results suggest that in the first stage the cool flame spread follows the premixed propagation mode, while in the latter stage the acceleration may be driven by the sequential spontaneous ignition.
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© 2025 The Japan Society of Microgravity Application

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