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• Satellite is any object
that orbits another
object:
• It has wide range of
mission
 Weather observation
 Military support
 Navigation
 Earth imaging
SATELLITE
TYPES OF SATELLITE
• Astronomical satellite: used for observing
distant planet and galaxies
• Communication satellite: used for
telecommunication using radio at microwave
frequencies
• Earth observation satellite: specially designed
for observing earth
• Weather satellite : monitor the weather and
climate of earth
TYPE OF ORBITS
• Geo stationary orbits: it
always positioned over
same spot on
earth(22,223 miles)
• Asynchonoly orbit : they
pass at overhead at
different time of day (644
km)
• Polar orbit : generally files
at low attitude and pass
over planet’s pole on each
revolution
THE ROCKET
• Rocket is a launching vehicle used to launch
satellite in to required orbit.
STRAP ON ROCKET
• 40 tones of hydraulic
propellants
• It burns before starting
the main engine.
TYPES OF ROCKET
• Expandable rocket : they destroyed while
completing their mission.
• Space shuttle: which is reusable
EXPANDABLE ROCKET
SPACE SHUTTLE
ROCKET ENGINE
• It is a self propellant engine.
• It carry fuel as well as oxidizer.
• Efficiency is measured as
specific impulse.
sp: impulse = thrust
produced /mass of propellant
burnt in a second.
SOLID ENGINE
LIQUID ENGINE
MECHANISM OF ROCKET ENGINE
Basic working principle is newton's 3rd low of
motion
Chemical reaction
Feed pump
Fuel tank
Oxidizer
Combustion chamber
Nozzle
TYPES OF PROPELLANTS
• Propellant is the chemical mixture burned to
produce thrust in rockets and consists of a fuel
and an oxidizer
• Solid propellant: gun powder
Zinc sulphur
High energy composite propellants
• Liquid propellant: LH2
LOH
LNH3
LAUNCHING STAGES
• Stage 1
• Stage 2
• Stage 3
STAGE 1
• Its travel 80 km
• The maximum thrust is 4700 kN
• Usually solid propellants are used
• Max thrust are produced this stage
• It split the 1st part of the rocket
• 125 tone of propellants are used, 3.2m dia &
25m length in the stage
STAGE 2
• It travel 168 km
• Maximum thrust produced is 720 kN
• Usually liquid propellants are used N2O2
• 110 ton of fuels are used
STAGE 3
In this stage satellites are get in to transfer orbit
73.5kN thrust are produced
Cryogenic engines are used
Fuels are LOH & LH2
25 tones fuels are used and 8.2m in length
When the rocket reaches T orbit, it must have
been attain the orbital velocity of earth other
vise it will return back to earth
APOGEE KICK MOTOR
Satellite are safely suited in this motor
Its also called the pay load firing
During the end of third stage the motor will
start firing and goes to required pallet
PROPULSION SUB SYSTEM
• The challenges are faced by rocket launching
• Thrust to weight ratio: it must be greater than
1 to take of the ground.
• Nozzle design: nozzle face varying expansion
condition from ground to space
THRUST TO WEIGHT RATIO
• To get a rocket off the ground, the total thrust
must be greater than the vehicles weight.
• The launch vehicle’s prolusion system must
produce a thrust to weight ratio greater than
1.0
COMMUNICATION & DATA HANDLING
Through out launch the vehicle must stay in
contact with a launch control center.
The flight controller continuously monitor
telemetry from the launch vehicle sub system to
ensure they’re working properly
The computer process sensor information and
compute commands for actuators, as well as
monitor other on board processes
Electric power
Launch vehicle need only enough power to run the
communication & data handling subsystem as well
as sensor & actuators.
In space uses fuel cell powered by hydrogen and
oxygen.
In expandable launch vehicle simple batteries are
used for primary power.
In satellite also have a battery for their working and
its recharged by a solar power through solar panel.
Conclusion
With the help of satellite any information
sending instantly at any place. Various tasks
such as mapping, locating, environmental
situation, locating mineral deposits, finding crop
problems etc. are performed by a satellite easily
they are used in field of communication in
the are of TV, the internet, the phones,
observations, are of geology and navigation, in
the area of transportation etc..
REFERENCE
http://en.wikipedia.org/wiki/Rocket_engine
http://science.howstuffworks.com/rocket.htm
http://youtube.com/launchingstages/rocket
http://videomide.com
Satellite sajith

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Satellite sajith

  • 1.
  • 2. • Satellite is any object that orbits another object: • It has wide range of mission  Weather observation  Military support  Navigation  Earth imaging SATELLITE
  • 3. TYPES OF SATELLITE • Astronomical satellite: used for observing distant planet and galaxies • Communication satellite: used for telecommunication using radio at microwave frequencies • Earth observation satellite: specially designed for observing earth • Weather satellite : monitor the weather and climate of earth
  • 4. TYPE OF ORBITS • Geo stationary orbits: it always positioned over same spot on earth(22,223 miles) • Asynchonoly orbit : they pass at overhead at different time of day (644 km) • Polar orbit : generally files at low attitude and pass over planet’s pole on each revolution
  • 5. THE ROCKET • Rocket is a launching vehicle used to launch satellite in to required orbit.
  • 6. STRAP ON ROCKET • 40 tones of hydraulic propellants • It burns before starting the main engine.
  • 7. TYPES OF ROCKET • Expandable rocket : they destroyed while completing their mission. • Space shuttle: which is reusable
  • 10.
  • 11. ROCKET ENGINE • It is a self propellant engine. • It carry fuel as well as oxidizer. • Efficiency is measured as specific impulse. sp: impulse = thrust produced /mass of propellant burnt in a second.
  • 14. MECHANISM OF ROCKET ENGINE Basic working principle is newton's 3rd low of motion Chemical reaction Feed pump Fuel tank Oxidizer Combustion chamber Nozzle
  • 15. TYPES OF PROPELLANTS • Propellant is the chemical mixture burned to produce thrust in rockets and consists of a fuel and an oxidizer • Solid propellant: gun powder Zinc sulphur High energy composite propellants • Liquid propellant: LH2 LOH LNH3
  • 16. LAUNCHING STAGES • Stage 1 • Stage 2 • Stage 3
  • 17. STAGE 1 • Its travel 80 km • The maximum thrust is 4700 kN • Usually solid propellants are used • Max thrust are produced this stage • It split the 1st part of the rocket • 125 tone of propellants are used, 3.2m dia & 25m length in the stage
  • 18. STAGE 2 • It travel 168 km • Maximum thrust produced is 720 kN • Usually liquid propellants are used N2O2 • 110 ton of fuels are used
  • 19. STAGE 3 In this stage satellites are get in to transfer orbit 73.5kN thrust are produced Cryogenic engines are used Fuels are LOH & LH2 25 tones fuels are used and 8.2m in length When the rocket reaches T orbit, it must have been attain the orbital velocity of earth other vise it will return back to earth
  • 20. APOGEE KICK MOTOR Satellite are safely suited in this motor Its also called the pay load firing During the end of third stage the motor will start firing and goes to required pallet
  • 21. PROPULSION SUB SYSTEM • The challenges are faced by rocket launching • Thrust to weight ratio: it must be greater than 1 to take of the ground. • Nozzle design: nozzle face varying expansion condition from ground to space
  • 22. THRUST TO WEIGHT RATIO • To get a rocket off the ground, the total thrust must be greater than the vehicles weight. • The launch vehicle’s prolusion system must produce a thrust to weight ratio greater than 1.0
  • 23. COMMUNICATION & DATA HANDLING Through out launch the vehicle must stay in contact with a launch control center. The flight controller continuously monitor telemetry from the launch vehicle sub system to ensure they’re working properly The computer process sensor information and compute commands for actuators, as well as monitor other on board processes
  • 24. Electric power Launch vehicle need only enough power to run the communication & data handling subsystem as well as sensor & actuators. In space uses fuel cell powered by hydrogen and oxygen. In expandable launch vehicle simple batteries are used for primary power. In satellite also have a battery for their working and its recharged by a solar power through solar panel.
  • 25.
  • 26. Conclusion With the help of satellite any information sending instantly at any place. Various tasks such as mapping, locating, environmental situation, locating mineral deposits, finding crop problems etc. are performed by a satellite easily they are used in field of communication in the are of TV, the internet, the phones, observations, are of geology and navigation, in the area of transportation etc..