1973
DOI: 10.1016/0019-1035(73)90014-6
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Preliminary results on the Venus atmosphere from the Venera 8 descent module

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Cited by 52 publications
(14 citation statements)
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“…We assume that the coefficient is proportional to atmospheric density, specific heat capacity at constant pressure, and wind speed (compare equations (6)–(8) in the work of Keszthelyi and Denlinger []). Griffiths and Fink [] provide density and heat capacity for the atmospheres of both Earth and Venus and winds speeds measured at the surface of Venus on the order of 1 m/s [ Avduevskij et al , ; Marov et al , ], and likely not larger than 2 m/s [ Lorenz , ]. This results in a forced convection coefficient h conv =208 W/(m 2 K).…”
Section: Model Of Eruption Thermal Emissionmentioning
confidence: 99%
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“…We assume that the coefficient is proportional to atmospheric density, specific heat capacity at constant pressure, and wind speed (compare equations (6)–(8) in the work of Keszthelyi and Denlinger []). Griffiths and Fink [] provide density and heat capacity for the atmospheres of both Earth and Venus and winds speeds measured at the surface of Venus on the order of 1 m/s [ Avduevskij et al , ; Marov et al , ], and likely not larger than 2 m/s [ Lorenz , ]. This results in a forced convection coefficient h conv =208 W/(m 2 K).…”
Section: Model Of Eruption Thermal Emissionmentioning
confidence: 99%
“…The Venus Monitoring Camera (VMC) [Markiewicz et al, 2007] on the ESA mission Venus Express [Svedhem et al, 2007] acquired 1 μm images of the nightside of Venus from 2006 to 2015. Shalygin et al [2015] report the observation of several transient bright spots at fixed locations visible through the clouds moving with the superrotating atmosphere.…”
Section: Introductionmentioning
confidence: 99%
“…The stated uncertainties in temperature measurements of the Venera probes is about + 1.5% or +2 K to +9 K [Kuzrnin and Maroy, 1974;Marov et al, 1973]. There are also significant altitude uncertainties discussed by Marov et al [1973] for Venera 8, +3 km, which in light of a lapse rate of-*8 K/km, could introduce temperature discrepancies of +25 K. These uncertainties, coupled with those stated earlier for the Pioneer Venus temperatures and altitudes, would appear capable of explaining discrepancies in static stability and differences in detailed shape of the temperature profiles. The large temperature differences between Venera 9 and 10 may also be due in part to measurement uncertainties.…”
Section: Temperature Differences Between the Venera And Pioneermentioning
confidence: 99%
“…The consistency of redundant radio observations Copyright ¸ 1980 by the American Geophysical Union. fled the assumption which had been used to infer wind speed profiles from the Doppler tracking of several Russian Venera spacecraft [Kerzhanovitch et al, 1972;Marov et al, 1973;Keldysh, 1977] that the wind direction remained westward from the cloud top to the surface. The fact that different Venera descents had yielded quite different wind speed profiles suggested, however, that there might be large (of the order of 100%) variations of the zonal winds in the lower atmosphere, possibly associated with changes in the local solar time.…”
Section: Introductionmentioning
confidence: 99%