N. P. Danilkin
Institute of Applied Geophysics, Moscow, Russia
Received May 16, 2000
Danilkin and Vaysman [1997]
suggested earlier that to
determine the principal ionospheric parameters used in
radiocommunication (the critical frequency of ionosphere
foF2,
height of maximum of the electron density in the ionosphere
hmF2,
and parameter
qF characterizing the half-thickness of the
F layer
in some approximation), the radiosounding may be conducted
practically from any height. If the ionosonde is located above the
maximum of the
F layer, usual ionograms which are well known and
described in literature
[Pulinets and Benson, 1999]
and for
which determination of the above-mentioned parameters causes no
problems, are obtained. The only difference is a considerably
shorter length of the vertical part of the
h'(f) curve (the
dependence of the virtual depth of the radio wave reflection on the
frequency). For the illustration sake Figure 1 shows such ionogram
obtained in Rostov-Don in the regime of the analog reception on a
portable antenna
[Danilkin and Ivanov, 1999].
Registration
of the amplitude of the signal reflected from the ionosphere and
Earth is a visible difference of the ionograms obtained in the
analog reception regime. The color corresponds to various
amplitudes and changes from red to violet while the amplitudes
change from higher to lower.
Location of the ionosonde at heights below or within the electron density maximum in the F region presents evidently the most difficult case which had no experimental verification before the Mir experiment. Conducting the experiments on the ionosphere radiosounding on board the orbital complex (OC) Mir provided a good chance to check this statement in the real conditions. During the experiments (August 1998-June 1999) OC Mir was at heights of about 340-360 km. Moving in the region of middle latitudes, it was, as a rule, above the ionosphere maximum and moving in the region approximately from 30o S to 30o N, OC Mir rather often moved below the F -region maximum. This paper describes the ionograms obtained in these conditions and their preliminary analysis.
The principal features typical for the radiosounding from a satellite flying below the F -layer maximum only slightly differ from the cases when the ionosonde flies at a height of about 1000 km. It should be only remembered that the deviations of rays from the vertical under the upward motion of a wave packet (the satellite is below hmF2, that is in the bottomside sounding) occurs in the same way as under the downward motion (topside sounding) in the magnetic meridian plane but in the opposite direction. In these cases the ordinary and extraordinary rays will be deviated northward and southward, respectively. In the situation under consideration, the satellite is in the plasma with higher electron concentration. Therefore the frequency ranges in which the conditions for propagation of three main magneto-ion components are fulfilled will be shorter. The initial frequencies (frequency cutoffs) are determined from the same conditions as for the topside sounding [Pulinets and Benson, 1999; Scannapieco and Ossakov, 1976]:
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where fZ is the slow extraordinary mode, fN is the fast ordinary mode, the cutoff frequency being equal to the local electron plasma frequency,
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where fX is the fast extraordinary mode.
The group velocity of the waves near the cutoff frequencies is small and therefore there appear effective conditions (the group velocity is close to the thermal velocities of the electrons) for occurrence of plasma resonances at the plasma frequencies of the region where the satellite is located. The group velocities increase sharply with an increase of the working frequency and, reaching the critical frequencies, they differ only slightly from the speed of light in the vacuum.
The noncoincidence of the lowest frequency of the sounding radio
wave reflection from the Earth with the critical frequency
foF2 of
the
F region is the main principal difference of the low-orbital
ionograms (that is, ionograms obtained when the satellite was below
the
F layer maximum). The coincidence of the parameters indicated
is the most prominent feature of the topside sounding (that is,
radio sounding by the ionosonde located above (as a rule,
considerably) the electron density maximum in the ionosphere) and
vertical propagation of the sounding radio waves. In the case when
the satellite is located below the electron density maximum of the
F region, the lowest frequency of the reflection from the Earth
determines the plasma frequency of the ionosphere at the OC Mir
location. Figure 2
shows the calculated expected ionogram and the
rays forming some of its components in the case when only one
reflection from the Earth is registered. In this case the term
virtual depths (the word "depths" is used as an analogy to the
topside sounding) is correct only for a part of the figure) has a
conventional meaning. Actually, they are rather virtual heights for
the rays of 1, 5, and 9. The correct term should have been "the
virtual distance under a vertical propagation", however it is too
long.
The calculated expected ionograms have very typical form and, processing the satellite ionograms, the above-mentioned difference (lower value of the lowest frequency reflected from the Earth as compared with the critical frequency of the ionosphere) may serve as a reliable criteria of the ionosonde location above or below the F region maximum. This difference is seen in all ionograms shown below and obtained during the sounding from the Mir station. The effect is visually seen in Figure 2. It should be noted also that the critical frequencies determined from the ionosphere reflection (rays 1, 5, and 9), from the ionosphere-Earth reflection (rays 3 and 7), and from the ionosphere-Earth-ionosphere reflection (rays 4 and 8) coincide.
Analyzing the ionograms one should bear in mind that the disposition of rays 3, 4, 7, and 8 is strictly determined by the disposition of rays 2 and 6 and 1, 5, and 9. Actually, any virtual depth, for example, for the ordinary component in the range from fn to foF2 reflected only from the ionosphere (ray 1) is defined by the relation
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where m' is the group refraction index, hs is the height of the satellite, r is the reflection height of a wave of the given frequency, f, fn, and fh are the working, plasma, and gyro frequencies, respectively, at the this height. Under reflection from the Earth the virtual depth from the satellite to the Earth ( hE ) at the given frequency is determined (ray 2) as
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Now the disposition of ray 3 is determined by the sum of rays 1 and 2 at each frequency. Similar consideration is correct for the extraordinary component and rays with a double reflection from the ionosphere.
Although the first ionograms obtained during the ionosonde
operation from heights below the
F region maximum confirmed the
main relations presented above,
they showed however that the
situation is much more complicated. Figure 3 (the left-hand panel)
shows an example of the ionogram which confirms the numerical
simulation shown in Figure 2 (color arrows show the
o,
x, and
z components reflected from the ionosphere, green and red points
show the reflection from the Earth and from the Earth and
ionosphere, respectively). One can distinctly see that the virtual
depth of the lower track is actually the sum of the virtual depths
of two upper tracks for both components within the accuracy the
measurements. Plasma resonances are almost always observed at the
cutoff frequencies for all three magneto-ionic components.
Besides the ionograms which confirm the model ionograms predicted, there is a considerable number of ionograms in which the lower track behaves principally different from the predicted one. It is not a sum of two upper tracks and, which is especially important, it is continued considerably further than the critical frequency and often reaches the end of the frequency range used. The right-hand panel of Figure 3 illustrates this case. Here the ionosonde is situated slightly below the layer maximum, the fact being confirmed by very narrow tracks of the reflection from the ionosphere of all three components of the magneto-split signal. The track of the reflection from Earth is also distinctly seen (the same colors are used as in the left-hand panel). Situated below is the second well-seen track which stretches in frequency much further than foF2, the latter being easily determined from the reflection from the ionosphere. We shall conventionally call tracks of the considered type as a "lower track".
The number of ionograms with the lower track exceeds the quantity of "correct" ionograms and the former were obtained under different geophysical conditions and in various parts of the Earth. Table 1 presents information on the ionograms with the lower track obtained on board OC Mir.
For a proper description of the phenomenon considered, Table 1 shows three groups (3 various days) in which ionograms of the considered type were observed. A daily series of observations was carried out on March 31, 1999 since 0949 UT till 0930 UT of the next day. This group is shown to illustrate the quantitative side of the phenomenon. During this time 6 groups of ionograms of the type described were observed, the corresponding data being shown in the top part of Table 1 (lines 1-6). They were observed mainly in the latitudinal belt from 20o S to 20o N. However at high latitudes the satellite also sometimes was below the F -layer maximum. Line 7 shows information about such case. Lines 8 and 9 illustrate particularly long periods of observation of the ionograms considered. The latter fact demonstrates that the region forming the extra track is very vast spatially and is a structure of the global scale.
To understand the physical nature of the phenomenon in question
we
consider a sequence of ionograms which arises when the satellite
moves from his position above the
F -region maximum to the position
below the maximum. The observations on April 21, 1999 were chosen
for the consideration. During 12 minutes of the station flight, an
increase of
foF2 from 8 to 15 MHz occurs smoothly enough
before the
first frame of Figure 4. Figure 4 shows four successive ionograms
(registered through unequal time intervals) along the OC Mir
trajectory and southward from the Taiwan Island (frames 567-582).
The reflections of various components of the magneto-split signal
and resonances at the plasma frequencies in the vicinity of the Mir
station for the ordinary and extraordinary rays are seen in all
ionograms.
The receiving station of ionograms from OC Mir in the analog regime and the station of the vertical sounding of the ionosphere operated in the Taiwan Island at this time. The comparison of the data of the ground-based and satellite sounding showed their full conformity in determination of the critical frequency and height of the ionosphere maximum [Pulinets et al., [1999]. At this orbit while the station moved equatorward there occurred an increase of the ionosphere maximum height and the station found itself below this height. Figure 4 presents successive phases of this process. Frame 567 shows that the station is still above the maximum. Frame 578 shows that the station passes the maximum. That is manifested very clearly by practically vertical reflection tracks of both components of the signal.
Frame 580 shows the first ionogram in which one can distinctly see that the station is already below the maximum of the layer. The track of reflection from the Earth and ionosphere is already well seen here in full conformity with the model-predicted ionogram in Figure 2. To let the reader see the real signals the artificial color points emphasizing the author's idea are not shown in this fragment of the ionogram. In the next frame 582, where the reflections from the Earth (yellow points) and from the Earth and ionosphere (red points) are already fully developed, the real signals are underlined by the above-mentioned colors.
The track of the reflection only from the Earth, from the Earth and ionosphere, plasma resonances at both components, coincidence of the sums of the virtual heights which was mentioned above, and so on are seen in this fragment. Until this ionogram all occurs in absolute conformity with the model predictions.
However further on occurs something unexpected. Already in
the
ionogram in Figure 5
(frame 583) one can clearly see that the track
of the reflection from the Earth and ionosphere is continued in the
frequency further than
foF2 ,
and the principle of the sum of the
virtual depths is not fulfilled. Frames 588, 603, and 608 show
further development of this process. A fast decrease of the
critical frequency occurs and at this background the lower track is
seen well for several megahertz (about 3 MHz in frame 588, that is,
about 60 soundings at fixed frequencies and about 2 MHz in frame
603, that is, about 40 soundings). Figures 3-5 and Table 1
provide
information about this phenomenon.
Ionograms presented in this section have been obtained in the conditions when the ionograms themselves do not indicate the disposition of the satellite, that is, it is not clear whether the satellite is below or above the maximum of the ionosphere. However this can be found from the events preceding and following the phenomenon in question. The corresponding analysis shows that this phenomenon arises both below and above the F -region maximum.
Figure 6 (frame 862) shows the ionogram typical for the case
considered. The horizontal track in a wide range of the plasma
frequencies of the ionosphere, by virtual depth beginning almost at
once after "opening" of the ionosonde receiver, is seen in the
ionogram. The reflections from the plasma frequencies between 6 and
15 MHz with the density of reflections irregular over the range are
seen here. Conventionally we call this type of reflection in
ionograms as an "upper track".
The most typical features of the
upper track are the absolute absence of group delays and minimum
possible virtual depth of the reflection.
The ionograms where the upper track is present are observed almost at all latitudes of the Mir station orbit, however, the predominant range of their appearance lies from 20o S to 20o N. Almost in a half of all cases the event described covers one or at the most two ionograms. In these cases the upper track in the succession of ionograms appears suddenly and also suddenly disappears.
In the second half of the cases of the upper track occurrence
it
arises in a chain of successive phenomenon. Figure 7 shows a
typical situation. One can see that the upper track appears (frame
480) in the conditions when the station is below the
F layer
maximum height. It is evident from the lower track which is also
distinctly seen in this ionogram. Further on it "develops"
(frame
482) and covers a vast region of the sounding frequencies (from 5
to 16 MHz), the reflection density being lower than in the previous
figure. In the frame 486 one can see again a group delay and
therefore the end of the phenomenon.
Sometimes the upper track is observed long enough. For example, on March 10, 1999 it was observed during 584 seconds or 73 frames. The station flew more 2500 km during this time. The upper and lower frequencies and also the track "density" were changing considerably, the upper frequency sometimes crossing the upper limit of the ionosonde measurement range (15.95 MHz).
Figure 8 shows one more typical (that is, repeated more than
once)
example of a "developing" upper track. Before its appearance the
group delay of the extraordinary component is sharply increased. It
is worth noting that the first ionogram of this cycle (frame 364)
was registered when the OC Mir was above the
hmF2 height. The last
ionogram (frame 374) corresponds to the station position almost
within the
F layer maximum. In this case the upper track was
observed during approximately one minute, that is, the dimension of
the corresponding region was about 300 km.
Analyzing possible explanations of the appearance of the
lower
track in the ionograms the author supposed that the lower track is
the result of an oblique reflection of radio waves from the Earth
and "lateral"
reflection of radio waves from the ionosphere, when
the wave "returns"
to the satellite due to a strong gradient of
the electron concentration situated aside the gravitational
vertical. Figure 9
shows this case conventionally. Possible
explanation of the appearance of this track as a result of only the
lateral reflection from steep gradients of the electron
concentration present in the equatorial "trough" seems less
probable. The matter is that the lower track arises always as a
continuation of the reflection from the Earth at its low-frequency
end. This reflection can not arise without reflection from the
Earth.
The author thinks that, discussing physical causes of the appearance of the upper track, two hypothesis should be considered. The first one deals with the well known at equatorial latitudes "bubbles" [Kelley et al., 1976; Scannapieco and Ossakov, 1976], that is, the formations where considerable decreases of the electron concentration are observed within some region. In this case the range of the plasma frequencies observed indicates the gradient of the electron concentration increase at the boundary of the bubble.
The second possible cause is a scatter of radio waves at some extremely thin and steeply-gradient layer of the electron concentration. Sometimes such layers occur and give reflections of the type of a sporadic E layer at heights of 100-150 km [Piggot and Rawer, 1977].
Danilkin, N., and A. Ivanov, Ionosonde "catches" space weather, Novosti Kosmonavtiki, 8, 56, 1999 (in Russian).
Danilkin, N. P., and G. M. Vaysman, Disposition of satellite ionosondes for the global ionospheric monitoring, Geomagn. Aeron., 33 (1), 190, 1997 (in Russian).
Kelley, M. C., et al., Evidence for a Rayleigh-Taylor type instability and upwelling of depleted density regions during equatorial spread F, Geophys. Res. Lett., 3 (8), 448, 1976.
Piggot, W. R., and K. Rawer, (Eds.), URSI Handbook of Ionogram Interpretation and Reduction, URSI, 1972.
Pulinets, S. A., and R. F. Benson, Radio-frequency sounders in space, in Review of Radio Science 1996-1999, pp. 711-734, Oxford Univ. Press., 1999.
Pulinets, S. A., Jann-Yeng Liu, Y. J. Chuo, N. P. Danilkin, and V. Kh. Depuev, Mir space station topside sounder: Possibilities for equatorial anomaly study, Terr. Atmos. Ocean. Sci. J.,
Scannapieco, A. J., and S. L. Ossakov, Nonlinear equatorial spread F, Geophys. Res. Lett., 3 (8), 451, 1976.