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Analytical support for SPAR experiment 76-36The apparatus, materials, and procedures used in an analysis of thermal, convective, and rotational fluid flow for a second series of rocket experiments of dendrite growth are described. A constitutive supercooling criterion was calculated from the thermal data. A convection analysis was made of the various cases to ensure that convective velocities will not exceed about .01 cm/sec in the low-g tests. Damping times for fluid flow generated by rocket spin-up and spin-down were also determined, so that the conditions for this experiment are generally the same as those for the SPAR experiment 74-21 study of ammonium chloride low-g crystallizations.
Document ID
19770025996
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Bourgeois, S. V.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Grodzka, P. G.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Pond, J. E.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Spradley, L. W.
(Lockheed Missiles and Space Co. Huntsville, AL, United States)
Date Acquired
September 3, 2013
Publication Date
August 1, 1977
Subject Category
Solid-State Physics
Report/Patent Number
LMSC-HREC-TR-D497400
NASA-CR-150389
Report Number: LMSC-HREC-TR-D497400
Report Number: NASA-CR-150389
Accession Number
77N32940
Funding Number(s)
CONTRACT_GRANT: NAS8-32401
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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