India’s Mission
to the Red Planet
Mars has always been a world
shrouded in mystery . Mars was thought to be a bright red star shining in the night sky. Sophisticated
technology and modern space missions have provided scientists with a wealth of
knowledge and information. Numerous questions remain unanswered. Although Mars
shared certain characteristics with the other planets, sky watchers observed
that it was unique in several ways. Because of its peculiar behavior, along
with its fiery red color, Mars was associated with war, violence, danger, and
death. As a result, some ancient peoples named the planet after their gods of
war. The Greeks called it Ares, and the Romans called it Mars.
Even though it
is doubtful that life exists on Mars today, was there a time when it did? If
so, what happened to it? The absence of living things is likely related to the
lack of water on the planet, which is another unsolved mystery. Scientists have
concrete proof that water once ran freely on Mars, but there appears to be no
trace of surface water now. What caused it to disappear? Recent missions
to Mars have provided direct evidence for the presence of hydrated minerals on
the exposed surface and of water at sub-surface regions. Possible presence of
methane has been proposed based on limited observations. Understanding the loss
of martian atmosphere, and in particular, carbon dioxide and water, is also
essential for understanding the evoution
of martian atmosphere. The Indian Mars mission includes payloads to obtain data
covering all the above important aspects that will advance our current
understanding of the planet Mars.
Mars orbiter mission(MOM)
Mars orbiter mission is ISRO’s first interplanetary mission
to planet Mars. The orbiter is designed to orbit Mars in an elliptical orbit to
collect scientific data. The mission is primarily a technology demponstration
mission with some important scientific objectives also. The orbiter will study
the physical features of Mars and the Martian atmosphere.
Mars Orbiter Spacecraft
The spacecraft configuration is a balanced mix of design
from flight proven IRS/INSAT/Chandrayaan-1 . Modifications required for Mars
mission are in the areas of Communication, Power, Propulsion systems (mainly
related to Liquid Engine restart after nearly 10 months) and on-board autonomy.
Mission Objectives:
Develop the technologies required for design, planning, management and operations
of an interplanetary mission ,orbit maneuvers to transfer the spacecraft from
an elliptical Earth orbit to a heliocentric trajectory and finally insert it
into Mars orbit ,development of force models and algorithms for orbit and
attitude computations and analyses,navigation in all mission phases ,maintain
the spacecraft in all phases of the Mission meeting Power,Communications,
Thermal and Payload requirements, incorporate autonomous features to handle
contingency situations .The scientific objectives set for the Mars Orbiter
Mission are : Study climate, geology, origin and evolution of Mars and to study
sustainability of life on the planet.
Payloads
aimed at un-derstanding the evolution of Mars are:
(i)
Lyman Alpha Photometer (LAP) for estimation of Deuterium /Hydrogen ratio based on absorption spectra of Deuterium and Hydrogen. Itconsists of an UV detector equipped with gas filled
pure molecular hydrogen and deuterium cells with tungsten filaments that are
located between an objective lens and a detector. Deuterium, also known as heavy hydrogen, is one of two stable isotopes
of hydrogen, and contains one proton and one neutron in its nucleus while the
common hydrogen isotope (Protium) has no neutron in the nucleus. Determining
the D/H ratio in the atmosphere allows scientists to learn more about the
atmospheric environments on Mars with a special focus on atmospheric loss.
(ii) Methane Sensor for Mars
(MSM): Methane on Mars can have a number of origins. When methane was first
discovered on Mars, many saw the presence of it as a clear indication of life
or microbial activity, but aside from biological processes, methane can have a
number of origins. Geological processes such as volcanism or reactions
involving iron oxide, water and carbon dioxide can produce large amounts of the
gas. In addition to these two traditionally known origins on atmospheric
methane, both, on Earth and on Mars, scientists have a number of other
theories. In recent years, exogenous sources have been studied. Methane being
produced by micro-meteorites and interplanetary dust particles that enter the
thin Martian atmosphere and settle on the surface. The instrument has a sensor to measure methane at several ppb
level.
(iii) Thermal Infrared
imaging Spectrometer (TIS): TIS will provide map of composition and
mineralogy of the martian surface. It uses a 120×160 element bo-lometer array
as detector and consist of fore optics, slit, collimating optics, grating and
reimaging optics. The knowledge on
type of minerals present in any planetary system provides the information on
the conditions under which minerals are formed and process by which they are
weathered. Much of what we know about the elemental composition of Mars comes
from orbiting spacecraft and landers. Most of these spacecraft carry
spectrometers(A spectrometer is an instrument used to measure properties
of light over a specific portion of the electromagnetic spectrum, typically
used in spectroscopic analysis to identify materials) and other instruments to
measure the surface composition of Mars.
(iv) Mars Exospheric Neutral
Composition Analyzer (MENCA): The objective of MENCA is to study the
exospheric neutral density and composition above the Martian surface.The instrument
examines radial,diurnal,and seasonal variations in the Martian exosphere.with
Mangalyaan in its operational orbit, MENCA is to estimate the upper limits of
the neutral density distribution and composition around mars.Studying Martian exosphere
will provide valuable data on the present conditions A quadrapole mass
spectrometer be employed to study the neutral composition of the martian upper
atmosphere.
(v) Mars Colour Camera
(MCC): Imaging of topogra-phy of the martian surface.. It provides images in the visual spectrum. Acquires color images of planet Mars. MCC
covers a spectral range of 400 to 700 nanometers – the visible spectrum..At
periapsis( near Mars) MCC provides images with a 50 by 50-Kilometer frame size
and a resolution of 25 meters per pixel. At apoapsis( distant from Mars) the
camera provides a wide field of view of 8,000 by 8,000 Kilometers. Imagery
provided by MCC are used to study Martian surface topography.
Mission
The mission consisted of three phases. During the geocentric phase, the
spacecraft was launched to the ellipltic parking orbit by the PSLV C25, rocket. Thjen it was gradually manouvered
to a hyperbolic trajectory and it escaped the Earth sphere of influence which
is upto 918347 Kms. The Mars orbiter entered the heliocentric orbit. To reach
Mars with minimum energy consuption Hohmann transfer orbit was used. This is
the orbit used to send a spacecraft to Mars with least amount of fuel. During
the journey to Mars two trajectory corrections were carried out. The spacecraft
arrived at the Martian sphere of influence at 573473 Kms in a hyperbolic
trajectory. At the time the spacecraft reached the closest point to Mars it was
captured into the planned orbit around Mars through a Mars orbit insertion
manouvere. On November
5th 2013:
PSLV-C25, , successfully launched Mars Orbiter Mission from Sriharikota .
Subsequently five orbit raising manouvers were carriedout.
Spacecraft has traversed beyond the Sphere of Influence (SOI) of Earth extending about on Dec 4, 2013.
In between two trajectory corrections were carriedout.
.On September 2nd the test Firing of Main Liquid Engine of Mars Orbiter Spacecraft was successful.On 24th September Mars orbiter entered the Martian orbit. The orbit of the spacecraft around Mars is 423 X 80000 Kms elliptical . It takes approximately three Earth days for one complete orbit. Mars Orbiter statrted sending pictures within hours of its orbital insertion. The total cost of the mission is Rs 450 crores.
Spacecraft has traversed beyond the Sphere of Influence (SOI) of Earth extending about on Dec 4, 2013.
In between two trajectory corrections were carriedout.
.On September 2nd the test Firing of Main Liquid Engine of Mars Orbiter Spacecraft was successful.On 24th September Mars orbiter entered the Martian orbit. The orbit of the spacecraft around Mars is 423 X 80000 Kms elliptical . It takes approximately three Earth days for one complete orbit. Mars Orbiter statrted sending pictures within hours of its orbital insertion. The total cost of the mission is Rs 450 crores.
On October 19th Comet A1 2013 Siding Spring will pass near
Mars at a distance of 132000Kms. The atmospheres of the Comet and Mars will
have an encounter and this is a n important event to observe. The comet may
harbour methane and water which will be studied by the Mars orbiter. Nasa’s
Maven orbiter reached Mars on 22nd September. The objective of that
spacecraft is to study the Martian atmosphere and the effects of solar wind in
the loss of atmosphere. It will also observe the comet closely.
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