2019
DOI: 10.1051/0004-6361/201834316
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Interstellar dust in the solar system: model versus in situ spacecraft data

Abstract: In the early 1990s, contemporary interstellar dust penetrating deep into the heliosphere was identified with the in-situ dust detector on board the Ulysses spacecraft. Later on, interstellar dust was also identified in the data sets measured with dust instruments on board Galileo, Cassini and Helios. Ulysses monitored the interstellar dust stream at high ecliptic latitudes for about 16 years. The three other spacecraft data sets were obtained in the ecliptic plane and cover much shorter time intervals. We comp… Show more

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Cited by 22 publications
(19 citation statements)
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“…However, in addition to gravity and radiation pressure, dust particles in this size range also respond to electromagnetic forces, as they carry a positive charge and react on interplanetary magnetic fields, resulting in temporal variability of the ISD flux with solar cycle, alternating between periods of focusing toward and away from the ecliptic plane (Landgraf 2000;Sterken et al 2012Sterken et al , 2015Strub et al 2019). While the basic interactions of ISD within the heliosphere appear to be well understood, our current models (calibrated using Ulysses data) can only reproduce the measurements of all spacecraft data of the variability of their flux measured to date within a factor of 2−3 (Krüger et al 2019). Hence, the question arises whether or not SDC detected ISD during its 15 yr cruise across the solar system.…”
Section: Isd Contributionmentioning
confidence: 96%
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“…However, in addition to gravity and radiation pressure, dust particles in this size range also respond to electromagnetic forces, as they carry a positive charge and react on interplanetary magnetic fields, resulting in temporal variability of the ISD flux with solar cycle, alternating between periods of focusing toward and away from the ecliptic plane (Landgraf 2000;Sterken et al 2012Sterken et al , 2015Strub et al 2019). While the basic interactions of ISD within the heliosphere appear to be well understood, our current models (calibrated using Ulysses data) can only reproduce the measurements of all spacecraft data of the variability of their flux measured to date within a factor of 2−3 (Krüger et al 2019). Hence, the question arises whether or not SDC detected ISD during its 15 yr cruise across the solar system.…”
Section: Isd Contributionmentioning
confidence: 96%
“…Hence, according to Equation (2), the much smaller and faster ISD will be assigned a larger IDP mass. With an expected size of 0.3 μm, speed of ;26 km s −1 , and ecliptic longitude of λ ISD ; 259°shown in Figure 3, we can predict what size SDC would mistake these ISD impacts as (Frisch et al 2009;Landgraf et al 2003;McComas et al 2012;Krüger et al 2015Krüger et al , 2019. The top panel of Figure 7 shows the anticipated impact speed of a 0.3 μm ISD compared to the assumed speed used in the IDP conversion from charge to mass in Figure 4.…”
Section: Isd Contributionmentioning
confidence: 96%
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“…The large depletion of iron from the gas phase of LISM clouds requires that most of the iron is resident in dust grains that are likely olivene silicates (Redfield & Linsky 2008;. In situ measurements of interstellar dust by experiments on Ulysses and other spacecraft sample dust grains with sizes larger than about 0.3 µm, because solar radiation pressure and heliospheric magnetic fields filter out most of the smaller grains (Mann 2010;Krüger et al 2019). Larger grains are expected to reach the inner solar system without significant changes in direction or speed.…”
Section: Sightlines To Nearby Starsmentioning
confidence: 99%
“…The spacecraft were equipped with two in situ dust sensors each, which measured the distribution of interplanetary dust in the inner Solar System for the first time (Grün et al 1980;Grün 1981). Altobelli et al (2006) re-analysed the Helios dust data searching for interstellar impactors (Grün et al 1994;Krüger et al 2019b). The authors recognised a cluster of seven impacts in a very narrow range of the spacecraft's true anomaly angle.…”
Section: Introductionmentioning
confidence: 99%