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Flame Extinguishment Experiment-2J (FLEX-2J)


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The FLEX-2J experiment is a joint effort between NASA and the Japanese Space Agency, JAXA, as well as Nihon University and Yamaguchi University.  Derived from the JAXA Group Combustion Experiment science objectives, the FLEX-2J will complement those goals using the NASA FLEX-2 hardware and combustion facilities on ISS.  FLEX-2J will observe and measure fuel droplet motions during flame spreading along a one-dimensional droplet array.  Three droplets will be deployed to fixed positions upon ceramic beads on a silicon carbide fiber.  Then an additional three to ten movable droplets are positioned to the fiber at known locations.  The first fixed droplet is ignited and the flame is propagated down the array from droplet to droplet.  The subsequent burning and motions of the unpinned droplets are recorded; particularly the velocities of the free droplets before and after flame spread are measured.  In addition, the experiment will obtain the history of flame leading edge position, flame spread limit span, and the growth process of the group flame along the fuel droplet array.  Specifically, the experiment will measure burning rate, burning time, flame spread and droplet motion as a function of inter-droplet spacing, ambient pressure and gas composition.

The FLEX-2J experiment will employ the Combustion Integrated Rack (CIR), part of the ISS Fluids and Combustion Facility (FCF).  Installed within the CIR, a chamber insert assembly, called the Multi-user Droplet Combustion Apparatus (MDCA), will contain the FLEX-2J specific hardware necessary for the experiment.  Some hardware and diagnostics left over from the FLEX-2 experiment may be employed or retained as reserve hardware, such as the FLEX-2 Radiometers.  Hardware specific to FLEX-2J that will need to be procured or manufactured and sent to ISS are a SiC fiber kit containing 6 fibers (supplied by JAXA), 2 pairs of igniter tips, two heptane fuel reservoirs, 2 CIR manifold bottles for diluent gasses, one pair of fuel deployment needles, and two adsorber cartridges (manifest subject to change). 


Contact Information:


Principal Investigator Team

Masao Kikuchi, JAXA
Hiroshi Nomura, Nihon University
Masato Mikami, Yamaguchi University
           
Project Scientist
Dr. Daniel Dietrich, NASA GRC

Project Manager
 J. Mark Hickman, NASA GRC

Engineering Team Lead

Marty O’Toole, ZIN Technologies, Inc.

 

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