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MANGALYAAN
 

MANGALYAAN

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INDIA'S FIRST MARS SPACE MISSION NAMED MARS ORBITER MISSION(MOM) SIMPLY KNOWN AS MANGALYAN. FOR MORE UPDATES AND SLIDES VISIT www.mechanizeinn.wordpress.com OR www.facebook.com/mechanizeinn

INDIA'S FIRST MARS SPACE MISSION NAMED MARS ORBITER MISSION(MOM) SIMPLY KNOWN AS MANGALYAN. FOR MORE UPDATES AND SLIDES VISIT www.mechanizeinn.wordpress.com OR www.facebook.com/mechanizeinn

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    MANGALYAAN MANGALYAAN Presentation Transcript

    • Presented by: Fazlur Rahman
    • Mars Orbiter Mission (MOM) is mars orbiter that was successfully launched into earth orbit on 5th November 2013 by Indian space research organisation (ISRO). The MOM probe lifted-off from the First Launch Pad at Sriharikota near Chennai, using a Polar Satellite Launch Vehicle (PSLV) rocket C25 at 09:08 UTC (2:38 PM IST) on 5 November 2013. The total project cost may be up to 454 crore (US$69 million). P. Kunhikrishnan was the PSLV-XL spacecraft launch Mission Director. Mylswamy Annadurai is the Program Director and S.Arunan is the Project Director. S. K. Shivkumar of ISAC was responsible for the orbiting payload and also oversaw design and development of the orbiter.
    •      ISRO is the primary space agency of the Indian government. Established in 15th august 1969, headquartered in Bengaluru, under the administrative control of the Department of Space, Government of India. Motto “Space Technology in the Service of Human Kind” Launch vehicles: Satellite Launch Vehicle (SLV) Augmented Satellite Launch Vehicle (ASLV) Polar Satellite Launch Vehicle (PSLV) Geosynchronous Satellite Launch Vehicle (GSLV) Geosynchronous Satellite Launch Vehicle Mark-III (GSLV III) Launch facilities: ISRO Satellite Centre, Bangalore Satish Dhawan Space Centre, Sriharikota Vikram Sarabhai Space Centre, Thiruvananthapuram Thumba Equatorial Rocket Launching Station,Thiruvananthapuram
    • Dr.VIKRAM SARABHAI Dr. K. RADHAKRISHNAN
    •       PSLV was designed and developed at Vikram Sarabhai Space Centre (VSSC), Thiruvananthapuram, Kerala. It was developed to allow India to launch its Indian Remote Sensing (IRS) satellites into sun synchronous orbits. Launch vehicle used is PSLV-XL PSLV-XL is the updated version of Polar Satellite Launch Vehicle. The PSLV has four stages using solid and liquid propulsion systems alternately. It has five successful launch in history
    • Payload Primary Objective Weight (Kg) Mars Colour Camera (MCC) Optical imaging 1.27 Thermal Infrared Imaging Map surface composition Spectrometer(TIS) 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 Study of Escape processes 1.97 (LAP) of Martian upper atmosphere through Deuterium/Hydrogen
    • Lyman Alpha Photometer (LAP) is an absorption cell photometer . It measures the relative abundance of deuterium and hydrogen from lyman-alpha emission in the Martian upper atmosphere (typically Exosphere and exobase). Measurement of D/H (Deuterium to Hydrogen abundance Ratio) allows us to understand especially the loss process of water from the planet.
    • MSM is designed to measure Methane (CH4) in the Martian atmosphere with PPB accuracy and map its sources. Data is acquired only over illuminated scene as the sensor measures reflected solar radiation. Methane concentration in the Martian atmosphere undergoes spatial and temporal variations.
    • MENCA is a quadruple mass spectrometer capable of analyzing the neutral composition in the range of 1 to 300 amu with unit mass resolution. The heritage of this payload is from Chandra’s Altitudinal Composition Explorer (CHACE) payload. MENCA is a quadrupole mass spectrometer based scientific payload, capable of measuring relative abundances of neutral constituents in the mass range of 1 to 300 amu, with a unit mass resolution.
    • This tri-color Mars color camera gives images & information about the surface features and composition of Martian surface. They are useful to monitor the dynamic events and weather of Mars. MCC will also be used for probing the two satellites of Mars-Phobos & Deimos. It also provides the context information for other science payloads.
    • TIS measure the thermal emission and can be operated during both day and night. Temperature and emissivity are the two basic physical parameters estimated from thermal emission measurement. Many minerals and soil types have characteristic spectra in TIR region. TIS can map surface composition and mineralogy of Mars.
    • We are wait for a grand success. Join us on : www.mechanizeinn.wordpress.com www.facebook.com/mechanizeinn