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Astron. Astrophys. 360, 729-741 (2000)
2. Solar energetic particles
The 1996 July 9, 9:10 UT flare occurred in the NOAA region 7978 on
the western hemisphere of the Sun, S
W , about
eastward of the nominal
interplanetary magnetic flux tube connected to the SoHO spacecraft
(solar wind speed was
km s-1
according to SWE/Wind observations). Gamma-ray signatures of energetic
ions and relativistic electrons at the Sun were recorded with the
Compton Telescope instrument (Schönfelder et al. 1993) aboard the
Compton Gamma-Ray Observatory spacecraft (COMPTEL/CGRO).
2.1. Gamma-ray observation of the flare impulsive phase
Observations at HXR/ -ray energies
of the 1996 July 9 flare event could be obtained by COMPTEL/CGRO until
about 9:16 UT when CGRO entered orbital night. The COMPTEL instrument
measured a signal in the Compton-telescope configuration which is
sensitive to -ray photons of 0.75-30
MeV, as well as in the two single burst detectors which detect photons
in the energy range 100-600 keV and 600-11000 keV,
respectively. Fig. 1 gives the measured time profiles and allows
to compare the timing of different energy ranges.
![[FIGURE]](img13.gif) |
Fig. 1. Observations of the impulsive phase of the 1996 July 9 flare event with COMPTEL/CGRO. The plotted data are corrected for detector life time effects, background is subtracted, and the data sets have been scaled relative to each other. The different energy channels have been obtained with COMPTEL's two burst detectors, high and low range burst module (HRBM and LRBM, respectively), and with the Compton telescope configuration. The peak times measured by the BATSE large area detectors are also indicated.
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Both burst detectors register the maximum of the emission at about
9:09:40 UT followed by two smaller emission peaks. The times agree
very well with the peak times measured by the BATSE large area
detectors for energies 25-100 keV (denoted t1,
t2, and t3 in Fig. 1). All three emission
curves originate from bremsstrahlung of electrons with an energy in
the range of roughly 50 to a few 100 keV.
The signal in the 3-7 MeV channel originates from nuclear line
emission which is emitted when protons and/or ions with an energy of
about 10-20 MeV/nucleon interact with ambient material in the
chromosphere. As can be seen in Fig. 1 the main emission in this
energy range coincides with the third peak at t3 of the
electronic emission. A faint signal can be seen also for the first
peak at t1, but no significant emission is seen during the
second peak at t2. A signal of the 2.2 MeV line was
detected well before t3. The emission in the 2.2 MeV
neutron capture line is produced with a time delay of about one minute
and requires reactions of protons and/or ions with an energy in the
range of about 10-100 MeV/nucleon. The detection of this signal
confirms that the emission during the first peak stems indeed from
nuclear lines, and that protons and/or ions accelerated up to energies
of at least 10 MeV have to be present.
It is known that the ratio of accelerated electrons to protons can
vary from flare to flare, or within flares (e.g., Chupp et al. 1993;
Marschhäuser et al. 1994; Miller et al. 1997). Here, the ratio is
highly variable for the three observed peaks: the emission at
t1 and t3 includes nucleonic signatures, while
during the peak at t2 it appears to be dominated by the
electron bremsstrahlung.
From the perspective of the particle injection times the COMPTEL
measurements show that the main HXR emission caused by
100 keV electrons occurred at
9:09:40 UT, while the main -ray line
emission caused by 10 MeV protons
appeared somewhat later at 9:10:20 UT. However, high-energetic protons
are present from the beginning of the event.
2.2. Overview of the SEP event
The solar energetic particle event was observed with the energetic
particle detectors ERNE (Torsti et al. 1995) and COSTEP
(Müller-Mellin et al. 1995) aboard SoHO. The interplanetary
proton event was weak enough for ERNE to be able to record nearly
every individual particle as pulse height data. For the goals of
present analysis, the ERNE recorded protons have been divided into six
energy channels: 1.6-3 MeV, 3-6 MeV, 6-12 MeV, 12-15 MeV, 15-20 MeV
and 20-30 MeV. The lowest channel has a geometrical factor of 0.260
and the next two 0.915
, thus the statistics are lower on
these channels compared to the three highest energy channels
possessing geometric factors of .
The time versus inverse-velocity scatter plot is shown in the top
panel of Fig. 2. The horizontal lines mark the energy channel
limits. Velocity dispersion is seen in the beginning of the event
indicating arrival of particles from the Sun. The observed solar wind
velocity of nearly 400 km s-1 implies the
interplanetary magnetic line length of
. The oblique line A in the
figure corresponds to this distance traveled from the reference time
9:12 UT - 500 s, the soft X-ray maximum time. We have
attempted to estimate first injection time and the distance traveled
also from our proton data using a kind of velocity-dispersion
technique described by Torsti et al. (1999). However, in 3-12 MeV
channels there was also contribution of the previous flare observed on
the same day at 7:58 UT (SGD 1996). This adds uncertainty to the
estimation. With data in hand we can rule out injection of first
protons before 9:08 UT - 500 s and after 9:28 UT - 500 s
(with a view to comparison with results of radio observations, we
artificially add to and then explicitly subtract from the particle
injection time the 500 s value required for radio waves to travel
from near-Sun to Earth). Thus based on velocity dispersion, we can
estimate the first proton injection time as
(9:18 UT - 500 s)
10 min.
![[FIGURE]](img27.gif) |
Fig. 2. Proton arrival time vs. scatter plot visualized in a gray scale proportional to the product of the times intensity, V being proton velocity (upper panel); also the intensity-time profiles of 12-20 MeV protons (middle panel) and 0.7-3 MeV electrons (lower panel). The tilted line A illustrates expected arrival times of first protons if injected from the Sun at 9:12 UT - 500 s.
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Fig. 2 also illustrates an abrupt decrease of proton flux,
simultaneously seen in all energy channels at 12:50 UT. This fall of
intensity indicates entering a new magnetic flux tube with very
different proton transport conditions (Kocharov et al. 1997). The tube
named a slow transport channel (STC) had been traversed at 16:00 UT on
July 9, 1996. In our present study, we do not consider observations
after entering STC. The employed period is limited by vertical lines
and
in Fig. 2.
On the middle panel of Fig. 2 we present the 5-minute averaged
proton intensity in the energy channel of 12-20 MeV employed for the
anisotropy measurement. In order to gain better statistics, the
channel is wider than in the anisotropy study by Torsti et al. (1997),
but otherwise the method is similar. A high anisotropy observed during
the entire event (excluding STC) implies a prolonged injection of
protons at the Sun. There were two peaks in the injection. The first
peak of the 12-20 MeV proton flux was about 90 min long, while only a
portion of the second peak was observed before entering a new flux
tube at 12:50 UT.
Relativistic electron flux was recorded with the COSTEP instrument
(Bothmer et al. 1997). The electron event start corresponds to the
injection of first electrons several minutes after the soft X-ray
emission maximum, 9:12 UT - 500 s (cf. vertical line A in
Fig. 3). Two sub-peaks can be seen at the top of the 0.25-0.7 MeV
electron profile (Fig. 3), but dip between them is rather
shallow. Entering a new transport channel (STC), observed with protons
at 12:50 UT, is only marginally observable in the electron profile
(marked with line B in Fig. 3). The STC effect in
electrons is much weaker than in protons.
![[FIGURE]](img31.gif) |
Fig. 3. The 0.25-0.7 MeV electron intensity as observed by the COSTEP/SoHO instrument (fluctuating curve) and the theoretical intensity (unlabeled heavy solid curve) comprising the main impulsive injection E2 and two minor injections E1 and E3 (correspondingly labeled light solid curves). Expected arrival of first electrons injected from the Sun at 9:12 UT - 500 s is shown with vertical line A. Start of the new magnetic flux tube (STC) is shown with line B. A spike at 9:10 UT is caused by the flare hard X-ray pulse.
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2.3. Scenario of electron injection
The electron intensity maximum (Fig. 3) is too flat and decays
too fast to be fitted with an exactly impulsive injection, but the
introduction of minor additions before and after the main injection
pulse produces a satisfactory fit. We have fitted the SoHO-observed
electron event with three impulsive injections, using the injection
time and injection strength as free parameters. The transport model
parameters have been adopted as explained in Appendix. The best-fit
curve in the case of the three-pulse injection is shown in
Fig. 3. It fits well the observed intensity-time profile. The
deduced injection times at the Sun are
9:17 UT - 500 s (the first
minor pulse of injection),
9:26 UT - 500 s (the major
injection peak) and 9:58 UT -
500 s (the last minor peak). Contribution of the injections to
the total 0.25-0.70 MeV fluence is 9%, 76% and 15% for the E1, E2 and
E3 pulses, respectively. Note that the decay of the first minor
injection, E1, and also the rise of the last minor injection, E3, were
essentially overlaid by the major peak, E2. For this reason, time
profiles of the minor injections could not be precisely deduced, but
should be regarded as the first
electron injection time, while gives
a min estimate of the last injection
time. Uncertainties in the determination of
and
do not exceed
min. Thus, the major electron
injection is impulsive and occurs not earlier than 15 min after the
flare start.
An analysis of the pulse-height data for the period 9:18-10:18 UT
within the 0.25-1.5 MeV energy range indicates nearly power law
differential energy spectrum: (H.
Sierks, pers. comm. 1999). The total number of
MeV electrons injected at the Sun is
per sr of the heliocentric solid
angle (i.e. per the area of solar
surface at the root of the Earth-connected interplanetary magnetic
field line).
The mildly relativistic electrons seen by COSTEP are associated
with an electron event observable also at lower energies, from about
1 keV to hundreds of keV, as detected by the 3-D Plasma and
Energetic Particle experiment on the Wind spacecraft (Lin et al.
1995). Determining the solar release time from the energy dispersion
of the electrons at the spacecraft (Krucker et al. 1999),
S. Krucker (pers. comm. 1999) finds that the first electrons are
released at the Sun at (9:21 UT - 500 s)
3 min. We have deduced with the
COSTEP data the first injection time
(9:17 UT - 500 s)
2 min. Given the different
techniques of analysis, the onset times of the electrons at Wind and
of the mildly relativistic electrons at SoHO are consistent. A mean
estimate for the first electron injection time finally is
(9:18-9:19) UT - 500 s. That implies that the electron
injection into interplanetary space occurs nearly ten minutes after
the onset of the radiative signatures of the flare.
2.4. Scenario of proton injection
Proton injection functions are deduced by a careful fitting of the
observed anisotropy and intensity-time profiles. A choice of proton
transport model is described in the Appendix. Several injection
scenarios have been studied. In particular, we attempted to fit the
proton intensity-time profile with an injection scenario deduced for
relativistic electrons, but it became evident that the proton
injection is prolonged and the impulsive injection scenario is not
applicable. Several other scenarios were also tested before we decided
to use a double-exponential injection profile (the alternative
scenarios are described more thoroughly in Sect. 4.2.3). The
injection rate is finally approximated in the following form
![[EQUATION]](img46.gif)
where
![[EQUATION]](img47.gif)
The fitting parameters, ,
and
, dominate the injection rise, decay
and the maximum injection time, respectively (Fig. 4). Those
parameters were allowed to be energy dependent and adjusted to get a
best fit for each energy channel. The normalization factors
determine injection energy spectra
for the first and second injection components,
. Similar to the 1990 May 24 event
study (Torsti et al. 1996), we call the 1st and 2nd injections
p-component and d-component injections,
respectively.
![[FIGURE]](img55.gif) |
Fig. 4. Solar injection rate profiles for protons. The injection rate is shown in units protons / (min MeV) per solar hemisphere; time as it was at the Sun. A d-component contribution to the 1.6-3 MeV channel has not been calculated.
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SoHO is a three-axis stabilized spacecraft and thus ERNE's particle
detectors do not cover the whole
solid angle, and the magnetic field direction is not stable. In order
to take this into account we calculate the differential acceptance of
the detector as a function of time and pitch angle and convolve it
with the interplanetary transport function to get a value of the
proton intensity averaged over the instrument acceptance cone. The
resulting intensity curve is directly comparable with the experimental
intensities (Fig. 5).
![[FIGURE]](img58.gif) |
Fig. 5. Theoretical (curves) and observed (asterisks) proton intensities in six energy channels. The double-exponential injection model has been used (see Eqs. 1-4 and Fig. 4). Light solid and dashed curves are for p- and d- components of injection, respectively. Heavy solid curves are for sums of the components.
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Highest uncertainties are expected in the low energy channels,
1.6-3 MeV and 3-6 MeV. In the lowest energy channel the instrument
consists of two detectors with a narrow,
, field of view. This results in a
high sensitivity to the magnetic field direction, if proton anisotropy
is large. In addition, low energy protons arrived too close to the
slow transport channel. Also the influence of the earlier flare
contaminates the 3-6 MeV channel (Fig. 2). In this view, we had
decided for the two lowest energy channels not to vary the maximum
injection time, , but to set it equal
to the time obtained from the four higher energy channels. Furthermore
in the lowest, 1.6-3 MeV, channel, we do not attempt to fit the
d-component portion of the intensity profile, i.e. the last 3-4 points
in the upper left frame of Fig. 5. Those data points certainly
indicate a new rise, but uncertainties of fitting few points would be
very large.
The deduced injection functions are presented in Fig. 4. In
this figure, we do not show initial portions of injection profiles
before the maximum cumulative effect of the injection exceeds the
level above background. The portion
of injection curves from which the particles would not reach SoHO
before entering the new magnetic tube (STC) is also left out. It is
seen from Fig. 4 that the maximum injection of the p-component
protons occurred around 9:50 UT (the corresponding near Earth
light-arrival time is 9:58 UT).
No energy dependent trend in the maximum injection time,
, is seen. The variance of
illustrates statistical
uncertainties, min. It is noteworthy
that the maximum time of the p-component proton injection,
, is close to the deduced time of the
last electron injection, . On the
other hand, the earliest observable injection of protons occurred
close to the time of the first electron injection
(see the 12-15 MeV proton injection
profile in Fig. 4). The first and the last electron injection
times, and
, bracket the rise phase of the
p-component proton production. Those minor electron injections might
be related to protons, and a kind of continual minor production of
electrons between and
cannot be ruled out.
Amplitudes and
(Eqs. 1, 2) give the proton
injection spectra at the peak injection time for the p-component and
the d-component, respectively. Best power law fits to the deduced
differential energy spectra are obtained for the spectral indexes
and
. Total numbers of the p- and d-
component protons injected at the Sun are respectively
and
per sr of the heliocentric solid
angle. Note that the d-component is dominant at low energies and
correspondingly in the total proton energetics.
© European Southern Observatory (ESO) 2000
Online publication: August 17, 2000
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