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The Phoretic Motion Experiment (PME) definition phaseThe aerosol generator and the charge flow devices (CFD) chamber which were designed for zero-gravity operation was analyzed. Characteristics of the CFD chamber and aerosol generator which would be useful for cloud physics experimentation in a one-g as well as a zero-g environment are documented. The Collision type of aerosol generator is addressed. Relationships among the various input and output parameters are derived and subsequently used to determine the requirements on the controls of the input parameters to assure a given error budget of an output parameter. The CFD chamber operation in a zero-g environment is assessed utilizing a computer simulation program. Low nuclei critical supersaturation and high experiment accuracies are emphasized which lead to droplet growth times extending into hundreds of seconds. The analysis was extended to assess the performance constraints of the CFD chamber in a one-g environment operating in the horizontal mode.
Document ID
19820019453
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Eaton, L. R.
(TRW Defense and Space Systems Group Redondo Beach, CA, United States)
Neste, S. L.
(GE Philadelphia, United States)
Date Acquired
September 4, 2013
Publication Date
May 14, 1982
Subject Category
Ground Support Systems And Facilities (Space)
Report/Patent Number
NASA-CR-162038
NAS 1.26:162038
Report Number: NASA-CR-162038
Report Number: NAS 1.26:162038
Accession Number
82N27329
Funding Number(s)
CONTRACT_GRANT: NAS8-34319
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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