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RADIATIVE ENERGY TRANSFER ON ENTRY INTO MARS AND VENUSQUARTERLY REPORT NO. 4The emissivity of carbon dioxide in the 2.7 4 µ region has been measured at temperatures from 2000°K to 3500°K, for optical densities less than 5 atm-cm. The high temperatures were obtained by passing a shock wave through the test gas. A total gas pressure of one atm was maintained by varying the carbon dioxide concentration in an inert gas. Emissivities obtained from absorption and emission measurements are in agreement. results are compared to an approximate method for calculating emissivity, The which considers the molecular population concentrated in a single band whose center is temperature dependent. A comparison with previous results suggests that this single band model will overestimate the peak and underestimate the width of the observed values. The observed and calculated emissivities are in agreement if the intensities of the (n1 +1,n2, n3 + 1 n1, n2, n3) and (n1,n2 +2, n3 + 1 n1, n2, n3) transitions are assumed proportional to (n1 +1) (n3 +1) and (n2 +1)(n3 +1)/2. The use of this single band model which was originally intended to provide a rough prediction of emissivity, indicates that the use of the appropriate terms of the electric dipole expansion is satisfactory for the (n1 +1,n2, n3 + 1 n1, n2, n3) transition, but is not for (n1,n2 +2, n3 + 1 n1, n2, n3) transition.
Document ID
19630005445
Acquisition Source
Legacy CDMS
Document Type
Contractor or Grantee Report
Authors
William O. Davis
(Illinois Institute of Technology Chicago, Illinois, United States)
Date Acquired
August 1, 2013
Publication Date
March 1, 1963
Subject Category
Space Radiation
Report/Patent Number
ARF-A200-A/Quarterly Report No. 4
Report Number: ARF-A200-4
Accession Number
63N15321
Funding Number(s)
CONTRACT_GRANT: NASR-65(00)
Distribution Limits
Public
Copyright
Public Use Permitted.
Keywords
radiative heat transfer
emission
high temperature
carbon dioxide
energy transfer
Mars /planet
Venus
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