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Droplet combustion at reduced gravityThe current work involves theoretical analyses of the effects identified, experiments in the NASA Lewis drop towers performed in the middeck areas of the Space Shuttle. In addition, there is laboratory work associated with the design of the flight apparatus. Calculations have shown that some of the test-matrix data can be obtained in drop towers, and some are achievable only in the space experiments. The apparatus consists of a droplet dispensing device (syringes), a droplet positioning device (opposing, retractable, hollow needles), a droplet ignition device (two matched pairs of retractable spark electrodes), gas and liquid handling systems, a data acquisition system (mainly giving motion-picture records of the combustion in two orthogonal views, one with backlighting for droplet resolution), and associated electronics.
Document ID
19890010942
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Dryer, F. L.
(Princeton Univ. NJ, United States)
Williams, F. A.
(Princeton Univ. NJ, United States)
Date Acquired
September 5, 2013
Publication Date
October 1, 1988
Publication Information
Publication: NASA, Washington, Microgravity Science and Applications Flight Programs, January - March 1987, Selected Papers, Volume 2
Subject Category
Materials Processing
Accession Number
89N20313
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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