mangalayaan

1. -INDIAN SPACE
RESEARCH ORGANISATION

2. MARS ORBITAL
MISSION
(MOM)
SESSION - 2014-15
SUBMITTED BY:
PRADIPTA MUKHERJEE RAKESH BHASKAR NAGALAKSHMI

3. Shri Koteswara Rao holds post graduate degree in
Instrumentation and Control Systems from JNTU College of
Engineering, Kakinada.
He has made significant contribution in the design and
development of satellite sensor systems of .
Shri Rao is a Member of
and the Executive Secretary of the of India.
Shri V Koteswara Rao
• Scientist and Director of Laboratory for Electro Optic
Systems (LEOS), a unit of ISRO.
• Scientific Secretary of ISRO.

5. DISCRIPTION OF MOM

6. Design and realization of a Mars orbiter with a capability to
survive and perform Earth bound manoeuveres, cruise phase of
300 days, Mars orbit insertion / capture, and on-orbit phase
around Mars.
Deep space communication, navigation, mission planning and
management.
Incorporate autonomous features to handle contingency
situations.
Exploration of Mars surface features, morphology, mineralogy
and Martian atmosphere by indigenous scientific instruments.

7. OBJECTIVES—CONTINUED…..
•DESIGN AND REALISATION OF A MARS ORBITER WITH A CAPABILITY TO PERFORM
EARTH BOUND MANEUVERS, CRUISE PHASE OF 300 DAYS, MARS ORBIT INSERTION
/ CAPTURE, AND ON-ORBIT PHASE AROUND MARS.
•DEEP SPACE COMMUNICATION, NAVIGATION, MISSION PLANNING AND
MANAGEMENT.
• THE SECONDARY OBJECTIVES ARE SCIENTIFIC, AND INCLUDE THE STUDY OF
MARS SURFACE FEATURES, MORPHOLOGY, MINERALOGY AND THE MARTIAN
ATMOSPHERE.

8. COST FACTOR
• Total cost for the mission is around 450 Crores
• The amount is less than the production cost of the movie
“GRAVITY”
• The cost spent by India is just 1/10th of the amount spent
by NASA, US for MAVEN (Mars Spacecraft)

9. MOM’s Disassembled View

11. Payload Primary Objective Weight (Kg)
Mars Colour Camera (MCC) Optical imaging 1.27
Thermal Infrared Imaging
Spectrometer(TIS)
Map surface
composition and
mineralogy
3.2
Methane Sensor for Mars
(MSM)
Detection of Methane
presence
2.94
Mars Enospheric Neutral
Composition Analyser (MENCA)
Study of the neutral
composition of
Martian upper
atmosphere
3.56
Lyman Alpha Photometer (LAP)
Study of Escape
processes of Martian
upper atmosphere
through
Deuterium/Hydrogen
1.97

12. CONSTRUCTION

15. PSLV-C25 launched the MARS
ORBITER into an orbit of
250 km X 23,550 km ,
around EARTH on
5TH NOVEMBER,2013

18. PSLV(POLAR SATELLITE LAUNCH VEHICLE)
• The Polar Satellite Launch Vehicle
commonly known by its abbreviation
PSLV, is an expendable launch system
developed and operated by the Indian
Space Research Organization (ISRO). It
was developed to allow India to launch
its Indian Remote Sensing (IRS) satellites
into sun synchronous orbits

21. GROUND STATION SUPPORT DURING MOM

26. MOMENT OF PROUDNESS

27. REFERENCES
• http://www.isro.org/pslv-c25/c25-status.aspx
• http://www.isro.org/mars/home.aspx
• http://www.isro.org/mars/challenges.aspx