The Mars Orbiter Mission (MOM) had technological objectives to design and realize a Mars orbiter capable of surviving Earth maneuvers, a 300-day cruise phase, Mars orbit insertion, and on-orbit operations around Mars. It also had scientific objectives to explore Mars' surface features, morphology, mineralogy, and atmosphere using scientific payloads. The payloads included a Methane Sensor, Mars Color Camera, Thermal Infrared Imaging Spectrometer, Mars Exospheric Neutral Composition Analyzer, and Lyman Alpha Photometer. The mission involved launch, orbital, and ground segments to support the objectives.

1. Mars Orbiter
Mission(MOM)
By
TEJA (13F01A0447)
BRAHMAM (13F01A0433)

2. Contents
•Mission Objectives
•Space Craft
•Payloads
•Ground Segment
•Conclusion

3. Mission Objectives
A. Technological Objectives:
• Design and realization of a Mars orbiter with a capability to survive and
perform Earth bound manoeuvres, cruise phase of 300 days, Mars orbit
insertion / capture, and on-orbit phase around Mars.
• Deep space communication, navigation, mission planning and management.
B. Scientific Objectives:
• Exploration of Mars surface features, morphology, mineralogy and Martian
atmosphere by indigenous scientific instruments.

4. Space Craft

5. Payloads
• Methane Sensor
• Mars Color Camera
• Thermal Infrared Imaging Spectrometer
• Mars Exospheric Neutral Composition Analyzer
• Lyman Alpha Photometer(LAP)

6. Methane Sensor

7. Mars Color Camera

8. Mars Exospheric Neutral
Composition Analyzer

9. Lyman Alpha Photometer

10. Thermal Infrared Imaging
Spectrometer

11. Ground Segment

12. Launch Phase

13. Orbital Phase

14. Pictures From Mars Color Camera

15. Conclusion
A specific search for methane in the Martian atmosphere
will provide information about the possibility of existence
of life on the planet.