Slide about Indias first mission to planet Mars. Include basic information about the mission.

1. Mars Mission of India
MOM( MA RS O RB ITE R MISSI ON)/
L A UNCHED : 5 T H N O V 2 0 1 3
.

2. Contents
• Features
• Why Mars?
• Mission Objectives
• Main Frame Elements of Mission
• Pay Loads
• Mission Plan
• Actual Mission
• Peoples Perspective

3. Features
• India’s First Mission to Red Planet
• 300 Days Cruise to Mars
• Cost $73 million (450 Crore)
• Weight 1.35 tones
• India is 5th in world travel towards
the Red Planet.
• All whether Rocket
• Self Diagnostic system that keeps
Space craft healthy.

4. Why Mars?
• 24 hours 37 minutes day
• 687 Days Year
• Gravity=1/3 of Earth
• Inspires vision of a approachable
word
• Planet Similar to Earth
• Human Speculation

5. Mission Objectives
Develop the Technologies Required for Design, Planning, Management and operations of an Interplanetary
missions.
Technical Objectives
• Design and realization of Mars orbiter
• Orbit around the Mars
• Deep space communication, Navigation, Mission planning and management
Scientific Objectives
• Exploration of Mars surface features.
• Study of Morphology, Topography, Mineralogy and Martian atmosphere by Indigenous scientific instruments.
• To see mars had the environment in which life evolved.

6. Main Frame Elements of
Mission
1. Polar Satellite Launch
Vehicle(PSLV)
2. Mars Orbiter

7. Polar Satellite Launch Vehicle (PSLV)
1. All Whether Rocket
2. Good Liability
3. 23 Successful mission
4. Responsible to put
Mangalyan into an elliptical
orbit.

8. Mars Orbiter [Payloads]
1. Lymph Alpha Photo Meter
2. Methane Sensor for Mars
(MSM)
3. Mars Exospheric Neutral
Composition Analyzer
(MENCA)
4. Mars Color Camera (MCC)
5. Thermal Infrared Imaging
Spectrometer (TIS).

9. Mission Plan
Develop the Technologies Required for Design, Planning, Management and operations of an Interplanetary missions.
Geocentric Phase
•
The spacecraft is injected into Elliptical parking orbit by the launcher
•
ISRO use s a method of travel called Hohmann Transfer Orbit or minimum Energy Transfer Orbit to send spacecraft from Earth to Mars
•
Six main engines burns in this phase for six midnight maneuvers .
•
At the end of this phase the spacecraft is escaped from Earth Sphere Of Influence(SOI). Earth SOI is 918347.
Heliocentric Phase
•
Spacecraft enters into Mars tangential orbit
•
This phase depends on relative position of Earth, Mars and Sun
•
Such relative arrangement recur periodically at interval of about 780 days.
Martian Phase
•
The spacecraft is arrives at the Mars Sphere Of Influence(SOI) [573473 KM from surface of Mars]
•
At the time of spacecraft reaches the closest approach to Mars, It is captured into planed orbit around Mars

10. Actual Mission
1. Geocentric Phase
2. Heliocentric Phase
3. Martian Phase

11. Peoples Perspective
+VE
•First Asian and fourth in word to
reach Red Planet.
•Put India out from the Space
faring nations.
•international standing
-VE
•Unwarranted Expense
•Economy Slowdown
•Major problems in front of
country is Hunger, Poverty and
Illiteracy.

12. Thank You