A. Wehry1 - H. Krüger2 - E. Grün2,3
1 - SAP AG, Neurottstrasse 16, 69190 Walldorf, Germany
2 -
Max-Planck-Institut für Kernphysik, Saupfercheckweg 1,
69117 Heidelberg, Germany
3 - Hawaii Institute of Geophysics and Planetology, HIGP,
University of Hawaii, 1680 East West Road, Honolulu, HI 96822, USA
Received 3 November 2003 / Accepted 18 February 2004
Abstract
The objective of this paper is to illustrate the influence of the
radiation pressure and the
electromagnetic force on dust particles in interplanetary space.
Between 1990 and 2001 62 so-called
-meteoroids (
describes the ratio of the radiation
pressure force to gravity) were detected as dust particles coming
from the inner solar system on hyperbolic orbits. 24 of them were
detected shortly after the launch of Ulysses within the ecliptic and 38 of
them were recorded primarily passing the Solar poles. Furthermore
high speed particles not coming from the direction of the Sun
were ejected from the solar system by electromagnetic forces. For
the time period until the end of 2008 the effective area for
particles coming from the direction of the Sun has been determined.
The particles'
perihelion distances indicated that they originated
within a region of
from the Sun.
For the second orbit of Ulysses the flux of
-meteoroids was
determined using the same method as during its first
revolution.
Because of the more
defocusing phase during the first orbit of Ulysses the production
rate of
-meteoroids has been estimated to be nearly twice
of that for the second revolution. On the other hand, an
imbalance of the identified
-meteoroids between the north
and south pole could not be explained by the solar cycle.
Key words: meteors, meteroids - solar system: general - ISM: dust, extinction
After the Ulysses spacecraft was launched in October 1990 the
flyby of Jupiter caused the spacecraft to move into an orbit which
is nearly perpendicular to the ecliptic plane. The first flight
through perihelion occurred on March 1995 at a solar distance of
,
whereas the second one happened in May 2002. On board the
spin-stabilized Ulysses spacecraft there is the Ulysses dust
detector with a sensor area of
.
This detector,
described in detail in Grün et al. (1992a,b), is a multi-coincidence impact ionization
detector with its spin axis pointing towards the Earth. The
detection geometry of this detector is determined by a viewing
cone of
relative to the sensor axis. The sensor
axis is mounted at
to the spin axis. The measured
particles are within a mass range of 10-18 to
with impact speeds from 2 to
(Grün et al.
1992b). The uncertainty of the mass determination
amounts to a factor of 10 whereas the uncertainty of the speed is
a factor of 2.
Based on measurements on board the Pioneer 8 and 9 spacecraft, dust
particles in hyperbolic orbits moving away from the solar
direction have been identified by Berg & Grün (1973) and
by Zook & Berg (1975) for the first time. These particles
are called -meteoroids and are escaping from the Solar
system in unbound orbits when the repelling force from the solar
radiation becomes similar in strength to the solar gravity. The
detection of
-meteoroids from the data set of the Ulysses
dust experiment has been investigated by Wehry & Mann
(1999). In the data set from Krüger et al.
(1999, 2001), we identified
-meteoroids from the remaining interplanetary particles
after subtracting Jovian dust streams and interstellar dust
particles.
-meteoroids are formed whenever small particles
are generated in interplanetary space. This can occur through
sublimation within 20 solar radii of the Sun or through
collisions as a result of
fragmentation of bigger particles. If these fragments are small
enough they will escape from the gravitation field of the Sun on
hyperbolic orbits. Using these assumptions concerning the origin
of
-meteoroids as well as the detector sensitivity we
identified
-meteoroids from the interplanetary dust
component in accordance with the criterion that was
developed in Wehry & Mann (1999). During the first 100 days of the Ulysses mission as well as during the south and north
polar passage 46
-meteoroids were detected with perihelion
distances smaller than
.
Apart from these
-meteoroids coming from the direction of the Sun the
influence of the radiation pressure force also causes
-meteoroids to come from a region further than
from the Sun. In this case the influence
of the electromagnetic force cannot be neglected.
In the current
paper we will concentrate on the following time periods: for the
time up to the end of 2001 we will show how many
-meteoroids have been identified using the above-mentioned
criterion. We will investigate the connection between the
occurrence of
-meteoroids and the solar magnetic field.
Using the number of identified
-meteoroids during the first
orbit of Ulysses we will give an estimate for the flux of
-meteoroids for this time period. Furthermore, we will
determine the effective area of the detector until the end of
2008 in order to present the time span in
which
-meteoroids can be identified.
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Figure 1:
Radiation pressure coefficient ![]() ![]() ![]() ![]() ![]() ![]() ![]() |
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Because of the solar gravitational attraction force
,
interplanetary particles move on Keplerian orbits around the
Sun. Additionally, the dynamics of small particles is influenced by
the radiation pressure force
which is in the opposite direction to
.
The so-called
-value or the radiation
pressure coefficient, shown in Fig. 1, describes the
ratio of the radiation pressure
to gravity
.
counteracts the solar attraction and
leads to an effective force
describing this reduced gravitation field.
From the orbital energy we obtain the escape velocity
is needed
for a particle to leave the bound orbit (
is the reduced
mass, r the solar distance and a the semimajor axis). Taking
the radiation pressure force into account, the escape velocity
decreases with increasing
proportional
to
compared to the case when only gravity applies.
The value of
,
shown in Fig. 1, is independent
of the solar distance r and depends only on the physical
properties, e.g. on the mass, material, composition and structure,
as well as on the size of the dust particle. Particles within the
mass range of 10-18 to
have
-values of from 0.3 to 1.7 and
are the source of
-meteoroids.
For dust particles the effective gravitational force decreases
with the solar distance proportional to r-2, whereas the
azimuthal magnetic field and the Lorentz force
(Q: charge, c: speed of
light,
:
relative velocity between particle
and solar wind
,
:
magnetic
field) decreases proportional to r-1.
The charge on a spherical particle is given by
with permittivity
,
surface
potential U and grain radius a.
The solar wind velocity,
which amounts to nearly
,
is radial and for
the greater part of the particle orbits
,
whereas
the Lorentz force is primarily normal to the orbit.
A comparison between the gravitational force
and the Lorentz force
acting on a dust particle under typical
interplanetary conditions at
is shown in Table 1.
Small particles are mainly
dominated by the magnetic force whereas bigger particles are
dominated by the gravitational force.
For dust particles with
radii smaller than
the influence of the Lorentz force
beyond a solar distance of
is greater
than that of the gravitational force.
So the Lorentz force is responsible for the occurrence of
-meteoroids at higher solar latitudes.
Table 1:
The gravitational force
and the
Lorentz force
acting on a dust particle with a radius a have been compared under typical interplanetary conditions
(at
,
solar wind with
,
magnetic field
B = 5 nT, particles charged to
;
forces are given in Newton).
Because of an alternating magnetic polarity near the ecliptic plane and because of a single polarity at high ecliptic latitudes the average force on particles close to the ecliptic is much smaller than that on high-latitude particles. The flux of interstellar dust grains, which is continuously monitored by Ulysses, began to decrease in mid-1996. The observed decrease by a factor of 3 was interpreted to be the result of the electro-magnetic interaction of the grains with the solar wind magnetic field (Landgraf 2000). The polarity of the solar wind magnetic field changes with the 22-year solar cycle. During the solar maximum in 1991 the field polarity became north-pointing. The azimuthal component of the corresponding radially expanding (Parker 1958) spiral field deflects interstellar grains in the northern hemisphere to the north and in the southern hemisphere to the south. Thus, the net effect of the interplanetary magnetic field during the 1991 polarity cycle was to divert interstellar dust out of the solar system. During the 2000/2001 solar maximum the field polarity reversed again. Then, interstellar grains in the northern hemisphere were deflected to the south and grains in the southern hemisphere to the north. This focusing effect increased the flux of interstellar grains in the inner Solar System significantly, starting in 2002 (Landgraf et al. 2003). This means that positively charged particles will be carried out of the ecliptic primarily during the defocusing time period from 1991 to 2002 whereas during the focusing time period (from 2002 to 2013) they will be focussed to the ecliptic (Hamilton et al. 1996).
Micron-sized particles are assumed to move in Keplerian orbits around
the Sun. Furthermore, we assume that -meteoroids are
produced from bigger particles at the perihelion of their orbit.
The perihelion velocity of the fragment is assumed to be the same
as the velocity of its parent body. For different perihelion
distances within 1 AU from the Sun and for different
-values
the speed of the newly-formed
-meteoroid and the
deviation from the direction of the Sun have been determined. Table 2 gives an example of the model calculation for the
eccentricity and the perihelion distance of the orbit of the
parent body and the assumed
-value of the fragment. This
-value is the lowest possible value for which the new particle
can be in an unbound orbit. For example, assuming a circular orbit
of the parent body at
and a
-value of 0.5
the heliocentric speed of the new particle is
at
and the direction differs by
from the radial direction. Comparing this
to the detection cone of the experiment, which
amounts to
,
such a flux of particles can be assumed
as directed radially outward. The same is the case for particles
with higher
-values or for particles with higher perihelion
velocities, when the orbits of the parent bodies are not longer circular.
Depending on the solar distance we determined a minimum speed of 20 to
as well as a maximum deviation of
from the direction of the Sun (cf. Fig. 2).
Table 2: Model calculations to find the minimum speed and maximum deviation of the ejected particle from the solar direction. The parent objects are moving on circular orbits (cf. Wehry & Mann 1999).
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Figure 2:
Detection geometry for the identification of ![]() ![]() ![]() ![]() ![]() |
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To know the time period over which particles with different
speeds can be seen from the direction of the Sun we determined the
relative velocity to the spacecraft as well as the angle between
the relative velocity to the spacecraft and the spin axis.
This allows us to calculate the effective area from the
periods of time during which -meteoroids can be identified.
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Figure 3: The effective detection area of the dust experiment for particles incoming from the radial direction of the Sun is shown as a function of time until the end of 2008. This area is high in 1991 directly after launch and again shortly before and after the passage through the ecliptic plane during the perihelion of the Ulysses trajectory. |
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In particular, the numerical imbalance of the identified
-meteoroids between the northern and southern hemisphere
has been conspicuous. During the first revolution of Ulysses
around the Sun 22
-meteoroids are identified, 18 of them within the
northern hemisphere and 4 of them within the southern hemisphere.
During the second revolution 16 particles are
detected as
-meteoroids, all of them within the northern
hemisphere.
For the time period of 16 August 1995-19 October 2001 Fig. 4 shows the speed of the interplanetary particles vs.
the angle of the sensor axis to the Sun. The dotted lines
characterize the criterion used to identify the 16
-meteoroids; they are shown in the upper left quadrant.
Furthermore, in the upper right quadrant in Fig. 4
there are many of particles with a speed higher than
.
These particles are escaping from the ecliptic region on
unbound orbits.
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Figure 4:
The speed of the interplanetary particles vs.
the angle of the sensor axis to the Sun provides the
identification of ![]() ![]() ![]() |
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To obtain information concerning the place and mechanism of their
origin we determined the perihelion distance of the identified
-meteoroids. Taking the velocity and the position of the
spacecraft into account, the resulting distribution for the
average perihelion distances, including the uncertainty in the
speed determination, is shown in Fig. 5. The
perihelion distances determined
(cf. Wehry & Mann 1999). We concluded that the place
of origin of
-meteoroids is within a region of
from the Sun. Because sublimation only occurs
at distances of up to 20 solar radii, these particles are probably
formed through collisions.
![]() |
Figure 5:
The distribution of the perihelion distances of
![]() |
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In a limited distance range from 1.3 AU to
the Ulysses
spacecraft passed from close to the solar south pole through the
ecliptic plane to close to the solar north pole. During 360 days of
the first pole-to-pole passage an rate of 0.33 impacts per day
or a total of 117 impacts of
interplanetary dust particles was detected (Grün et al.
1997, 2001). Compared to
this, during the first revolution of Ulysses only 22
-meteoroids were detected within a time period of 130 days
which corresponds to an impact rate of 0.16 impacts per day. For
the second revolution of Ulysses only 16
-meteoroids within
a time period of 118 days correspond to an impact rate of 0.14
impacts per day. Because of the small numbers of detected dust
particles the statistical significance
is relatively small so that new observations are required to confirm
this result.
The event rate of the Pioneer 8 and 9 impacts reached a maximum
peak just past the direction of the Sun. From this observation Whipple
(1975) concluded that the direction of the impact center,
which is strongly in the direction of the Sun, constrained that
-meteoroids on the whole are produced in orbits outside
.
Whipple (1975) assumed a constant value
for the angular momentum of a
-meteoroid that is released at
zero velocity at perihelion. He varied the perihelion and
aphelion distance to get information about the
heliocentric distances at which the collisions occur. Even for an
initial orbit that is parabolic, the minimum perihelion
distance is
.
This means that
-meteoroids
are formed outside
(Whipple 1975).
Though both analyses refer to the defocusing period of the
magnetic field, the result of Whipple (1975) does
not contradict our conclusion that the place of origin of
-meteoroids is within a region of
to the Sun.
According to Hamilton et al. (1996) grains of radius
remain bound for initial orbits between
and
.
Particles both interior
and exterior to this disk escape from the ecliptic during the
defocusing period. During the pole-to-pole passage of Ulysses the
particles from the interior can be detected as
-meteoroids. The beginning of the Ulysses mission corresponds
to the end of the focusing period of the magnetic field.
At this time particles did not escape from the ecliptic
according to Hamilton et al. (1996). Therefore,
the place of origin of
-meteoroids can be determined to be
within a region of
to the Sun during the beginning of
the Ulysses mission.
The detection of -meteoroids at high latitudes near the
solar poles requires that the dust particles are deflected from
their orbital motion within the ecliptic. Both interplanetary and
interstellar particles suffer from this deflection which is caused
only by the Lorentz force (Landgraf et al. 2000).
Small interplanetary dust
particles are ejected from a bigger particle which is moving in a
bound orbit. On the other hand, small interstellar dust particles
which are moving nearly perpendicularly to the Ulysses trajectory
leave their initial orbit and reach the solar pole region due to the
electromagnetic influence of the Lorentz force.
The detection of -meteoroids within the northern hemisphere
occurred for both orbits of Ulysses within a time range of nearly
4 months. During the first orbit 22
-meteoroids
were identified in a distance range of 1.8 to
.
Assuming an average speed of
for these
-meteoroids their time of flight corresponds to a range of
3.7 to 5 months. Taking a time of nearly 4 months for the
detection of these 22
-meteoroids into account, the time
range in which these
-meteoroids were generated could be
estimated to be 3 months. During the second orbit 16
-meteoroids were detected in a distance range of 1.3 to
.
This corresponds to a time of flight between 2.5 and
3.7 months, i.e. 16
-meteoroids were generated in a time
range of 4 months. From this we conclude that during the first
orbit of Ulysses the production rate for
-meteoroids was
nearly twice as high as during the second orbit.
The identification of
-meteoroids that
occurred during the first orbit of Ulysses at higher latitudes
confirms this conclusion. Because the defocusing field was much
more developed in 1995 during the first orbit than in 2002 during
the second orbit, we can conclude that the defocusing magnetic
field is responsible for this phenomenon. In 2002 the
reversal of the polarity of the magnetic field caused the new
focusing cycle to start. The difference in number of
detected
-meteoroids between northern and southern
hemisphere is remarkable. The quality of the observation of the
dust detector, which can be characterized by the effective area, is
similar for both hemispheres, as are the observing conditions
relative to the magnetic cycle. So we cannot give any clear
explanation for this asymmetry.
The high number of particles with velocities above
in the upper right quadrant in
Fig. 4 is notable. Obviously, it is a matter of
particles on hyperbolic orbits far outside the solar region.
During the time period from 16 August 1995 to 19 October 2001 we
had a defocusing field. At this time the density of grains at higher
latitudes increases as more grains are deflected away from the
ecliptic into this region. In this context Hamilton et al.
(1996) argued that the electromagnetic influence of
the solar magnetic field, i.e. the Lorentz force
,
is
responsible for the motion of these dust particles, which are
called electromagnetic
-meteoroids. At the end of the
defocusing cycle in 2002 the regions of enhanced density move
downstream and a focusing cycle begins to concentrate grains
around the plane of the solar equator.
The flux of -meteoroids was determined according to the
following equation
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Figure 6:
The flux of ![]() ![]() ![]() ![]() ![]() ![]() ![]() ![]() |
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As shown in Fig. 6 the flux of -meteoroids
during the first revolution around the Sun equals
between 1.0 and
in the ecliptic plane, and amounts to
between 1.8 and
at solar ecliptic latitudes between
and
during
the north polar passage. Up to a solar distance of nearly
the decay of the flux of
-meteoroids with increasing solar distance
can be approximated by a
-dependence with
.
At greater solar distances probably the decreasing
solar latitude leads to a lower flux of
-meteoroids.
To estimate the flux for the second orbit
of Ulysses we compare the effective area of the
first with that of the second revolution. The flux of
-meteoroids is proportional to the number of
-meteoroids and inversely proportional to the
effective sensor area.
Comparing the maximum value of the effective area during the
first revolution to the value during the second revolution of Ulysses
within the northern hemisphere we find that they are of the same
order of magnitude. Within the southern hemisphere
the maximum value of the effective area during the second
revolution of Ulysses reaches nearly
of the value
during the first revolution. Because nearly the same number of
-meteoroids was detected during both orbits, we expect a
similar flux of
-meteoroids for the second revolution of
Ulysses.
The influence of the radiation pressure force and of the
influence of the Lorentz force on the motion of dust particles has
been investigated on the basis of the analysis of the Ulysses
data. For the time period during the second revolution of Ulysses
(16 August 1995-19 October 2001)
the identification of -meteoroids which are coming from a
direction near to the Sun is based upon a criterion developed by
Wehry & Mann (1999). During this time period we
identified 16 particles within the northern hemisphere as
-meteoroids coming from the Sun. An asymmetry between the
detected
-meteoroids within the northern and the southern
hemisphere could not be explained. The origin of the detected
-meteoroids has been determined to lie within a region of
from the Sun. Because of different assumptions this result
does not contradict to a study of Whipple
(1975) who concluded that the origin was outside this region. The
production rate of
-meteoroids during the first orbit of
Ulysses has been estimated to be nearly twice of that during the
second revolution. This is probably a result of the greater
defocusing phase during the first orbit of Ulysses. Furthermore,
we identified high-speed particles like the so-called
electromagnetic
-meteoroids which do not come from the
region near to the Sun. We estimated a similar flux of
-meteoroids for the second orbit of Ulysses. Until the end
of 2008 we determined the expected effective area for particles which are
coming on hyperbolic orbits from the direction of the Sun. This
effective area lies high above the Solar poles.