Mars Orbiter Mission

Mission type Mars orbiter
Operator ISRO
COSPAR ID 2013-060A
SATCAT № 39370
Website www.isro.org/mars/home.aspx
Mission duration 6 months (planned)[1]
Spacecraft properties
Bus I-1K[2]
Manufacturer ISAC
Launch mass 1,337 kg (2,948 lb)[3]
Dry mass 500 kg (1,100 lb)
Payload mass 15 kg (33 lb)[4]
Dimensions 1.5-metre (4 ft 11 in) cube
Power 840 watts[2]
Start of mission
Launch date 5 November 2013, 09:08 UTC[5]
Rocket PSLV-XL C25[6]
Launch site Satish Dhawan FLP
Contractor ISRO
Orbital parameters
Reference system Areocentric
Periareon 421.7 km (262.0 mi)[7]
Apoareon 76,993.6 km (47,841.6 mi)[7]
Inclination 150.0° [7]
Period 72 hours 51 minutes 51 seconds[7]
Epoch Planned
Mars orbiter
Orbital insertion 24 September 2014, 02:00 UTC
MSD 50027 06:27 AMT[8]
  • Project Director – M Annadurai
  • ISRO Chairman – K.Radhakrishnan
  • 4th agency to reach Mars after Soviet Space Program, NASA and ESA


Challenges Faced

  1. Distance – Target was moving at a rapid pace around the sun and adding to that was unknown of venturing into the space.
  2. Communication – Owing to huge distance (upto 400 million kms), a communication system with low, medium and high gain antenna and other ground antennae was put in place to handle communication which took between 6 to 43 minutes for 2-way communication.
  3. Power – Demand of strong solar panels by the spacecraft. A solar panel was put in place to generate 840W of power in Martian orbit with 36 AH lithium ion attached onboard for power storage.
  4. Protection – Designing the spacecraft to avoid all the the thermal and radiation environments on en route to Mars.


Payloads onboard Spacecraft

  1. Mars Color Camera (MCC) – To capture images and composition of Mars, monitoring dynamic events and weather etc.
  2. Methane Sensors – To map the sources of methane in Martian environment.
  3. Lyman Alpha Photometer (LAP) – To study the escape process of upper atmosphere as well as water from Mars.
  4. Thermal Infrared Imaging Spectrometer – To map surface composition and mineralogy of Mars based on thermal emissions.
  5. Mars Exospheric Neutral Composition Analyzer (MENCA) – To analyze the neutral composition.



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