ppt on mission Mangalyaan
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Mangalyaan presentation
1. Research Done by: Praveena.K Devanathan Balarageetha Krishna Suriya.K Priyadharshini.M
2. MANGALYAAN-like a breath of fresh air Stepping in an ocean A successful completion.
3. CONCEPT ANALYSIS TO ANALYSE THE PLANET MARS.
4. Need of Mangalyaan ISRO is already using the technology to help other countries put their equipment in space. If we continue to innovate in cost and speed, we could become a big hub for space projects. That would mean employment for 1000s of engineers and lot of foreign money. If we could launch a Mars mission at the cost of setting up ERP in an enterprise, we could build anything.
5. Objective1. Mission Objective: Develop the Technologies Required for Design, Planning, Management and operations of an Interplanetary missions. 2. Technical Objectives : Design and realization of Mars orbiter • Orbit around the Mars • Deep space communication, Navigation, Mission planning and management 3. 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. What Mangalyaan actually going to do??? 1. To find methane. 2. To find the availability of water in MARS. 3. To find temperature and climatic condition in mars. 4. To find the chemical components present.
7. SHORT DESCRIPTION ABOUT MANGALAAN Name meaning : Mars-Craft (from sanskrit mangala) Duration:15 months. Budget:450 crores. Purpose: To analyse MARS.
8. Conti.. Operator: ISRO Launched Place:Satish Dawan Space Centre (Sriharikota) Launch Date: 5 November 2013. Orbital Insertion:24th September 2014
9. Brain’s Behind the mission K. Radhakrishnan M.Annadurai S.Ramakrishnan S.K.Shivakumar
10. Detailed Description K.Radhakrishnan- Chairman ISRO responsible for leading the mission and overall activities of ISRO M.Annadurai- Programme Director, MOM responsible for budget management, direction for spacecraft configuration, schedule and resources
11. S. Ramakrishnan-Director of Vikram Sarabhai Space Centre . responsible for development of liquid propulsion stages and their interfacing with vehicle and launch operations. S.K.Shivakumar-Orbiting payload Director, ISAC responsible for developing satellite technology and implementing satellite systems for scientific, technological and application missions
12. Specification MASS The lift-off mass was 1,350 kg , including 852 kg of propellant mass. DIMENSIONS Cuboid in shape of approximately 1.5 m . POWER Electric power is generated by three solar array panels of 1.8 × 1.4 m each. Electricity is stored in a 36 Ah Li-ion battery.
13. Conti… PROPULSION Liquid fuel engine of 440 N thrust is used for orbit raising and insertion in Martian orbit, and 8 numbers of 22 N thrusters are used for attitude control . COMMUNICATIONS Two 230 W TWTAs and two coherent transponders. The antenna array consists of a low-gain antenna, a medium-gain antenna and a high-gain antenna.
14. Image of Mangalyaan
15. Trajectory path