dc.description.abstract |
The Earth WOl1l(l be lifeless without the atmosphere which not only protects the
Earth from harmful ra(hation from the Sun but also supports life system by maintaining
suitable temperature and warming the surface through heat retention. The
Sun-Earth system provides insight to the structure and dynamics of the Earth's atmosphere.
The basis of all physical and chemical processes occurring in the Earth's
atmosphere is the Sun-Earth interaction. The study of Sun-Earth interaction reqiures
acci.irate knowledge of variations in solar radiation and solar wind which is a
very challenging task clue to active interaction of solar energy with the atmosphere
of the Earth. Different layers of Earth's atmosphere interact with the energy of the
Sun in a (hiferent nianner. The atmosphere of the Earth comprises of four layers
(lependmg on the vertical structure of the temperature profile [1-3]. These layers
are troposphere (0-12 km). stratosphere (12-50 kin), rnesosphere (50-90 kni) and
thermosphere (above 90 km). The ionosphere (above 60 krn) is a region of Earth's
atmosphere containing large amount of charged atoms and molecules [4-14]. It is
not a separate layer but is embeckled in the layers of atmosphere. The Earth's
atmosphere can also be broadly classified into three regions. These are lower atmosphere
(0-20 km), middle atmosphere (20-100 kin), and upper atmosphere (above
I'
100 km). The upper atmosphere is one of the most important part of the Earth's
atmosphere since it is the region where solar radiation makes its first contact with
the planet Earth. Most of the ionosphere and atmosphere interactions occur in
this region. The photoclissociation of N2 and 02 produces 0 and N atoms in
abundance. The atomic species are dominated at higher altitudes and the molectilar
species are mostly accumulated in the lower (lomnain of the upper atmosphere.
The temperature in this region first rises dramatically with the altitude dine to
the absorption of solar EUV radiation by oxygen and nitrogen molecules and then
becomes constant above 50() km [15].
The solar radiation interacts with different species of the Earth's atmosphere
at different wavelengths at all altitudes, energizing these species in terms of ionization.
(liSSOCiatiOn and excitation. Almost all of the ultraviolet radiation is absorl)ed
in the Earth's atmosphere and is therefore a good proxy to predict the dynamics,
temperature distribution and the chemical processes occurring in the upper atmnosphere.
There are various measurements and modeling studies reported in the
literature on solar UV radiation [16-19]. The interaction of solar UV radiation
with the atmospheric species causes specific transitions of some species from lower
to higher excitation states. In the upper atmosphere, which has a low density and
is optically thin for the radiations above 350 urn, these species may dc-excite to
lower energy states by elmtting radiations. These emitted radiations constitute a
very wide range of emission spectrum known as 'airgiow' . Airglow emissions are
(lassifiedl into three types based on the time of observation. These are dayglow.
nightglow and twilight glow. When the observations are taken during the day
time it is dayglow. The dayglow emissions are difficult to observe due to high
solar background. The nightglow is observed during the night time. The twilight
glow is observed during early morning or early evening when the Sun is below the
horizon but is seen from altitudes above 50 km.
The airgiow emission line structure and intensity provide wealth of information
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about the composition and temperature of the atmosphere and the doppler shifts
give information about the wind motions. The structure and (lynaimcs of gravity,
planetary and tidal waves can be studied using airglow emissions [20-22]. The
airglow features are used to retrieve ozone concentration in the upper mesosphere
and lower thermosphere [23]. The rotational temperatures could be easily traced
out from airglow emission features [24,25]. The effects of geomagnetic storms on
airglow emissions have been studied by various researchers [26-28]. Thus for a
complete overview and understanding of the Earth's atmosphere airglow emission
studies play a vital role. The airglow emission arising due to molecular species
occurs in the altitude range of 80-270 km since dissociation is (lormnant above
100 kin while the density of the species decreases with altitude. The airglow
emissions arising due to atomic species occur in the altitude range 80-1000 kin.
Thus airglow is generated by different species at different altitudes [29-32]. The
most important ones are those generated by atomic and molecular oxygen and
nitrogen, OH molecule, and Na atoms [33-36]. The atomic oxygen generated 557.7
urn, 630.0 run, 732.0 mn and 844.6 nm airglow emissions are of much interest to the
researchers due to the valuable information provided by these emissions [30,37-45].
The 557.7 mu (green line) airglow emission occurs in rarefied gaseous media
al)ove 90 kin altitude involving transition between metastable states O('S-'D). The
green line airglow emission involves a lot of complex chemistry and tracing out accurate
atomic oxygen number density from this emission is difficult. However, this
emission is a good indicator of wind dynamics and horizontal diffusion [46-48].
The 630.0 nm airglow emission arises at the F2 ionospheric layer altitudes and
is a good tracer of neutral wind fields and vertical temperatures in the upper
atmosphere [49, 501. This emission results from a metastable state 0(1 D) which
involves various photocliernical production processes and loss mechanisms. Hence,
tracing of the atomic oxygen number density is a complicated procedure .Above
200 kin altitude the reliable knowledge of atomic oxygen number density becomes
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essential to track the satellite drag and to predict the space weather conditions.
The satellite passing through the Earth's upper atmosphere experiences drag force
which depends upon density at the satellite altitude. The 732.0 urn airgiow emission
dominates above 200 km which arises from the transition from metastable
state 0(2 P-2D). The 0(2P) is produced through photoionisation excitation of
ground-state atomic oxygen and photoelectron impact ionisation of ground-state
atomic oxygen [44,51,52]. Consequently, the production rate of 732.0 nm emission
would strongly depend upon the atomic oxygen number density. A number of
researchers have found that the O+(2P) 732.0 nm airglow emission proves to be
a potent tool to predict thermnospheric density above 200 km altitude [52,53]. A
limited number of studies have been reported in the literature to infer solar UV
fluxes and the exospheric temperatures from 732.0 urn airgiow emission [54-561.
Another important emission effective in investigating the atomic oxygen number
density in the altitude range 130-260 km is the 844.6 nm airgiow emission since
it arises from allowed transition and hence no loss mechanism processes involve in
the modeling tecimiques. Therefore, 844.6 nm airglow emission serves as a direct
measure of atomic oxygen concentration [57. 58].
A very limited number of measurement studies have been reported on 732.0 nm
and 844.6 urn airgiow emissions in the literature [39,44,52-55,57,59-61]. Although
few modeling studies have been clone on 732.0 nrn and 844.6 urn airgiow emissions,
but these could not be validated due to lack of experimental data on parameters
such as reaction rate coefficients, transition probabilities, collisional cross sections
etc. However, the data on these parameters is still limited. Therefore, the existing
models of 732.0 urn and 844.6 urn day-glow emissions need to be modified in
the light of recently revised reaction rate coefficients, transition probabilities and
collision cross sections. In the present thesis an attempt is made to study 732.0
urn and 844.6 urn (layglow emissions by means of mnocleling by incorporating latest
transition probabilities, reaction rate coefficients and cross sections. The solar
extreme ultraviolet (EUV) fluxes calculated using the Solar Irradiance Platform
(SIP) are incorporated into the model [62.63]. The neutral atmospheric parameters
are adopted from the Naval Research Laboratory Mass Spectrometer and
Incoherent Scatter Radar Exosphere (NRLMSISE-00) model. The ionospheric parameters
are adopted from the International Reference Ionosphere (IRI-07) model.
The photochemical models of 732.0 nm and 844.6 nm dayglow emissions are further
used to study these emissions under various solar and geomagnetic activity
conditions. The research work presented in this thesis is summarized in the form
of five chapters.
The first chapter gives the general introduction to the Sun-Earth interaction,
solar radiation, airglow emissions, and topics related. It outlines the need and
importance of studying airglow emissions. A brief literature survey of the earlier
studies in this field in context to the present study is presented. The importance
of the present problem and the reason for choosing the same are also presented in
this chapter.
In the second chapter, the development of a photochemical model of 732.0 nm
dayglow emission is discussed using latest updated transition probabilities, reaction
rate coefficients and cross sectionis. The measurements as provided by instruments
oriboard Atmosphere Explorer-C satellite, Dynamics Explorer-2 spacecraft and
Upper Atmosphere Research Satellite are used to validate the model results. It
has been found that the emission rates conhl)l.itedl using the present model are in
good agreement with the measurements. It is also found that the present model
results are in better agreement with the measurements in comparison with the
earlier models. The model results show that the updated rate coefficients and
transition probabilities are quite consistent with each other and may be used in
the aeronomical studies.
In the third chapter, the effect of atomic oxygen abundance on the voli.uiie emission
rate of 732.0 urn dayglow emission at the equator for edluinox and solstice cases
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is discussed. To study the effect of atomic oxygen abundance on 732.0 rim (layglow
emission, the atomic oxygen number densities obtained from the NRLMSISE-00
model are increased (or decreased) in an increment (or decrement) of 20% and
are incorporated into the photochemical model to compute volume emission rate
profiles. The present study shows that the peak emission rate (PER) varies linearly
below the reference level of atomic oxygen number density and does not
vary linearly above the reference level of atomic oxygen number density. The
atomic oxygen number density at reference level corresponds to that value which
is obtained from the NRLMSISE-0() model. It is found that the altitude of peak
emission rate moves upward as the F10.7 solar index increases. On an average
the upward movement of altitude of PER is about 9 kni for both the equinox and
solstice cases. The upward movement of the altitude of peak emission rate is clue
to the enihamicemnienit in atomic oxygen number density with increase in F10.7 solar
index.
In the fourth chapter, the effect of geomagnetic storms on 0+(2p.2D) 732.0 nrn
dayglow emission is studied. Three geomagnetic storms which occurred on 23-27
August 2005, 13-17 April 2006 and 1-5 February 2008 are chosen in the present
study. A negative correlation is found between the volume emission rate (VER)
and the Dst index for all the three geomagnetic storms. The present study shows
that the relative variation of VER with respect to the initial value of VER (before
the onset of a geomagnetic storm) during the main phase increases above 260 km.
It is also found that the altitude of the peak emission rate does not show any appreciable
variation with the activity of geomagnetic storm. A positive correlation
is found between the zenith intensity and the atomic oxygen number density. The
atomic oxygen number density obtained from NRL1SISE-0() model is compared
with the measurements of Earle et al. [26] during a geomagnetic storm. This cornparison
shows that the atomic oxygen number density is provided by NRLMSISE-
00 model is significantly lower than the measured value. Consequently, the atomic
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oxygen number density is treated as a variable parameter in the photochemical
model and its effect on the VER of 732.0 run dayglow emission is further studied.
The zenith intensity is found to increase about 70% even in the case of weakest
storm when the atomic oxygen number density is doubled.
In the fifth chapter, a photochemical model is developed to study 844.6 nm
dayglow emission. The Solar2000 EUV (Extreme UltraViolet) flux model, neutral
atmosphere model (NRLMSISE-00) and latest available cross-sections are incorporated
in this model. The present model is used to study the effects of geomagnetic
storm on the 844.6 urn dayglow emission at a low latitude station Tirunelveli
(8.7°N, 77.8°E). Three geomagnetic storms which occurred during 23-27 August
2005, 13-17 April 2006 and 1-5 February 2008 are chosen in the present study. It is
found that the volume emission rate (VER) shows a negative correlation with the
Dst index for all the three geomagnetic storms. The present study also shows that
the altitude of the peak emission rate does not vary with the activity of geomagnetic
storm. The model predicts a positive correlation between the zenith intensity
of 844.6 nm dayglow emission and atomic oxygen number density. It is reported by
Dharwan et al. [60] that the atomic oxygen number density given by NRLMSISE-
00 model is significantly lower than the measured values. Consequently, the effect
of atomic oxygen number density abundance on 844.6 nrn dayglow emission is further
studied by treating the atomic oxygen number density as a varial)le parameter
in the present model. An increase of more than 50% in the zenith intensity above
the normal level (before the onset of the storm) is found when the atomic oxygen
number density which is obtained from NRLMSISE-00 model is doubled (under
the limits of measurements). A comparative study of 732.0 nm and 844.6 urn dayglow
emission under geomagnetic storm conditions is also carried out for the above
mentioned geomagnetic storms. The study shows that there is an increase of 10%
- in the ratio of VERs of the two emissions (VER514(i/VER7320) for the intense storm
and around 7% for the weakest storm during the main phase at 260 km. The ratio
of zenith intensity of the two emissions (I846/I7:320) is more or less constant during
all the phases of the storm in all the three cases. |
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