1989
DOI: 10.1038/341585a0
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Television observations of Phobos

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Cited by 42 publications
(7 citation statements)
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“…Using the theory of Woolard [1944], Sharpless [1945] estimated an along‐track acceleration of (1.82 ± 0.17) × 10 −3 deg/yr 2 . Subsequent observations have refined the estimate and models generated in support of the Russian Phobos mission [ Sagdeev and Zakharov , 1989; Avensov et al , 1989; Morley , 1989] all give concordant estimates, as indicated in Table 1. Given the long time span of the observations, and relatively high accuracy of the models, it might be supposed that little additional progress would occur.…”
Section: Introductionmentioning
confidence: 86%
“…Using the theory of Woolard [1944], Sharpless [1945] estimated an along‐track acceleration of (1.82 ± 0.17) × 10 −3 deg/yr 2 . Subsequent observations have refined the estimate and models generated in support of the Russian Phobos mission [ Sagdeev and Zakharov , 1989; Avensov et al , 1989; Morley , 1989] all give concordant estimates, as indicated in Table 1. Given the long time span of the observations, and relatively high accuracy of the models, it might be supposed that little additional progress would occur.…”
Section: Introductionmentioning
confidence: 86%
“…We adopt C ej =0.3 and ν =1.2. Using equation (1) and a Phobos density of 1.9 g cc −1 (refs 42 , 43 ), the mass ejected within each velocity bin is calculated. For the Stickney impact, of the 1.5 × 10 13 kg ejected faster than the Phobos escape velocity, only 1.2 × 10 12 kg (8%) is ejected faster than 100 m s −1 .…”
Section: Methodsmentioning
confidence: 99%
“…We adopt = 0.3 and = 1.2. For Phobos' density we use 1.9 g/cc (Avanesov et al, 1989;Rosenblatt et al, 2008;Schmedemann et al, 2014). From (11), the mass ejected within each velocity bin is calculated ( Figure 6).…”
Section: Mass Transfer Between Martian Satellitesmentioning
confidence: 99%