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Radiometer experiment for the aeroassist flight experimentA forthcoming NASA flight experiment is described that provides an opportunity to obtain a large base of radiometric data for high-altitude, high-velocity thermochemically nonequilibrated-flow conditions. As a preliminary to the design of a radiometer for this experiment, an approximate method for predicting both equilibrium and nonequilibrium radiative surface fluxes is described. Spectral results for one trajectory state, a velocity of 10 km/sec at an altitude of 85 km, are presented. These results are then used to develop some of the instrument parameters that will be needed for designing of the three genre of radiometers that are proposed for this experiment.
Document ID
19850056792
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Davy, W. C.
(NASA Ames Research Center Moffett Field, CA, United States)
Park, C.
(NASA Ames Research Center Moffett Field, CA, United States)
Arnold, J. O.
(NASA Ames Research Center Moffett Field, CA, United States)
Balakrishnan, A.
(Eloret Institute Sunnyvale, CA, United States)
Date Acquired
August 12, 2013
Publication Date
June 1, 1985
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 85-0967
Accession Number
85A38943
Distribution Limits
Public
Copyright
Other

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