There are many satellites which are orbiting around our
planet earth. There are around 4900 different types of satellites out of which
around 1900 active satellites are orbiting in different orbits. Obvious
questions which arise in our mind are why satellites are orbiting in different
orbits, how does a satellite perform its work and what are components inside
the satellite which makes satellite functioning?
It is true that a satellite due balance between
gravitational pull and centrifugal force remains in orbit. The angular velocity
of the satellite is governed by balancing the centrifugal and gravitational
force, which balance the centrifugal and gravitational force. When a satellite
is deployed in space, sufficient speed is given to the satellite to balance
these two forces. To oppose the gravitational pull outside the earth’s sphere
of influence, increased speed in necessitated. Due to negligible resistance
(due to friction) a satellite never loses its speed. It means without any energy
source, the satellite will continue to follow a circular path (more precisely elliptical) around the earth.
Satellites are deployed in LEO (low earth orbit), MEO (medium earth orbit) or Geosynchronous orbits.
View of satellite with unfolded Solar Panels |
There is an interesting region in space called Van Allen
belt; this region is completely occupied by high energy and charged particles
which may seriously damage the electronic section the satellite. It is advised
not to deploy satellite in Van Allen belt region, but the deployment altitude
from earth depends on application and purpose of the satellite. If the
satellite is used for the purpose of weather forecasting, earth observation,
geographic area surveying, satellite phone calls etc., then the low earth orbit satellites
are preferred.
Low Earth Orbit covers the altitude range of 160 km to 2000 km and the
orbital period is around 1.5 hours. These satellites covers small area of
earth, large number of satellites are required for global coverage that’s why
for the purpose of broadcasting geosynchronous satellites are used.
Geosynchronous satellites have the altitude about 35786 km and these satellites
orbits around the earth with same angular velocity of earth, means these
satellites takes 23 hours and 56 minutes and 4 seconds to complete orbital period.
At a particular altitude special belt in Geosynchronous orbit called Geo-stationery belt is present which is concentric with earth’s equator. These
satellites are in constant position with relative to earth, that’s why Geo-stationery satellites are ideal choice for television broadcasting, these
satellites are the reason that you do not have to change your dish antenna angle
continuously, due this reason Geo-stationery belt is full of satellites. And
this belt is controlled and managed by an international organization called
ITU. Among these satellites some navigation satellites are also orbiting in this
belt which is generally used in GPS.
Medium Earth Orbit is a wise option for GPS satellites
even if LEO is closer to earth. In LEO satellites angular speed of satellites is more due
to which navigational calculations cannot be performed accurately by receivers
on earth, also to cover whole earth a large number of LEO satellites will be
required. GPS satellite are deployed at altitude of 20,200 km. In a typical GPS
system 24 satellites can cover whole earth and the orbital period for these
satellites is 12 hours.
Let take a look at main components of a satellite.
At center of the satellite a transponder is incorporated,
the main functions of transponder are to change the frequency of received
signals, to remove noise and to amplify the magnitude of signal. In Ku band
satellites transponder converts from 14 GHz to 12 GHz and the numbers of
transponders may vary from one to twenty in a typical satellite. It is clear
that to perform all these functions by transponder, power will required, to
provide power supply a satellite is incorporated with batteries and solar
panels.
Solar panels are used to power electronic components of
satellites and at time of eclipses batteries are used. A sun sensor can be
easily seen on satellite, this sun sensor helps satellite to give correct angle
toward sun so that more power can be generated.
How transponder receives signals from antennae?
Common
antenna used in a satellite are reflector antennas. A satellite should follow
its intended smooth orbit. Gravitational field around the earth is not uniform
due to unequal distribution of mass and presence of moon due to which
satellites get deviated from their intended orbit, this is a serious and undesirable
issue because it results in signal loss, to overcome these problems firing
thrusters are used to keep the satellites in position orbit. A sufficient
amount of fuel is place in fuel tank of satellite. Mono Methyl Hydrazine
Nitrogen Tetra Oxide is used as fuel. Thrusters and position control systems
are continuously monitored from earth stations. Beside thrusters and position
controls earth station also monitors satellite’s health. It is done by
telemetry, control system and tracking systems. These systems continuously send
signals to earth stations and keep a continuous relation between earth and
satellite. These signals are exchanged at different frequencies to
differentiate communication signals.
What happens to the satellites which completed their life span or becomes non-functional?
These satellites may damage other operational
satellites or spacecrafts, to counter these situations these inactive
satellites are shifted to graveyard orbit by firing thrusters. By firing
thrusters of satellites velocity of satellite gets increased and radius of
orbit also increased. Graveyard orbit is situated about few hundred km above from
geostationary orbit.
Communication Tower |
We have discussed only communication satellites whose
important components are atomic clock and a antenna. Generally L-Band antenna
is used in these satellites. Whenever you saw a satellite you have noticed that
about whole satellite components are covered by gold foil type layer what is
it? Actually if you see its cross sectional area you will find a multi layer
film made of polyimide or polyester coated with aluminum. There is a large
temperature variation in space which is encountered by satellites. These
temperature variations vary from -150 degree Celsius to 200 degree Celsius also
satellites are faced by heavy radiations from sun. This film protects
satellites from these stuffs.
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