Mangalyaan mars orbiter mission
Download as PPTX, PDF4 likes4,011 views
The Mars Orbiter Mission was launched by ISRO on November 5, 2013 from Sriharikota, India. Its primary objective was to demonstrate India's ability to design, plan and manage an interplanetary mission. The spacecraft weighed 1350 kg at launch and successfully performed orbit raising maneuvers before the Trans-Mars Injection on November 30th, 2013 that placed it on a heliocentric orbit en route to Mars. The orbiter is scheduled to perform Mars Orbit Insertion on September 24, 2014 to study the Martian surface, atmosphere and further demonstrate India's deep space capabilities.
![SPACECRAFT
Mass -The lift-off mass was 1,350 kg
(2,980 lb), including 852 kg (1,878 lb) of
propellant mass.
Dimensions -Cuboid in shape of approximately
1.5 m (4 ft 11 in)
Bus-The spacecraft's bus is a modified I-1
K structure and propulsion hardware
configurations similar to Chandrayaan 1, India's
lunar orbiter that operated from 2008 to
2009, with specific improvements and upgrades
needed for a Mars mission.[28] The satellite
structure is of aluminum and composite fiber
](https://image.slidesharecdn.com/mangalyaan-marsorbitermission-131211220745-phpapp01/85/Mangalyaan-mars-orbiter-mission-5-320.jpg)
![TELEMETRY AND COMMAND
The Indian Space Research Organisation Telemetry, Tracking and
Command Network performed navigation and tracking operations for
the launch with ground stations at Sriharikota, Port
Blair, Brunei and Biak in Indonesia,[32] and after the spacecraft's
apogee became more than 100,000 km, two large 18-metre and 32metre diameter antennas of the Indian Deep Space Network started
to be utilised.[33] NASA's Deep Space Network is providing position
data through its three stations located in Canberra, Madrid and
Goldstone on the U.S. West Coast during the non-visible period of
ISRO's network.[34] The South African National Space Agency's
(SANSA) Hartebeesthoek (HBK) ground station is also providing
satellite tracking, telemetry and command services.[35] Additional
monitoring is provided by technicians on board two leased ships from
the Shipping Corporation of India, SCI Nalanda and SCI
Yamuna which are currently in position in the South Pacific near Fij](https://image.slidesharecdn.com/mangalyaan-marsorbitermission-131211220745-phpapp01/85/Mangalyaan-mars-orbiter-mission-8-320.jpg)
More Related Content
Similar to Mangalyaan mars orbiter mission (20)
![Mars orbitar misson [mom]](https://cdn.slidesharecdn.com/ss_thumbnails/marsorbitarmissonmom-150109091928-conversion-gate01-thumbnail.jpg?width=560&fit=bounds)
Mangalyaan mars orbiter mission
- 1. Is life possible on Mars ?
- 2. INTRODUCTION The mars orbiter mission informally called as Mangalyaan is a mars orbiter launched into earth orbit on 5th november 2013 by ISRO. The mission is a "technology demonstrator" project aiming to develop the technologies required for design, planning, management and operations of an interplanetary mission.
- 3. The Mars Orbiter Mission probe lifted-off from the First launch pad at Sriharikota Andhra Pradesh near Chennai, using a Polar Satellite Launch Vehicle (PSLV) rocket C25 at 2:38 pm on 5 November 2013. The launch window was approx 20 days long and started on 28 October 2013. The MOM probe spent about a month in Earth orbit, where it made a series of seven altitude-raising orbital manoeuvres before trans-Mars injection on 30 November 2013
- 4. OBJECTIVES The primary objective of the Mars Orbiter Mission is to showcase India's rocket launch systems, spacecraft-building and operations capabilities. Specifically, the primary objective is to develop the technologies required for design, planning, management and operations of an interplanetary mission, comprising the following major tasks: design and realisation of a Mars orbiter with a capability to 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; incorporate autonomous features to handle contingency situations. The secondary objective is to explore Mars' surface features, morphology, mineralogy and Martian atmosphere using indigenous scientific instruments
- 5. SPACECRAFT Mass -The lift-off mass was 1,350 kg (2,980 lb), including 852 kg (1,878 lb) of propellant mass. Dimensions -Cuboid in shape of approximately 1.5 m (4 ft 11 in) Bus-The spacecraft's bus is a modified I-1 K structure and propulsion hardware configurations similar to Chandrayaan 1, India's lunar orbiter that operated from 2008 to 2009, with specific improvements and upgrades needed for a Mars mission.[28] The satellite structure is of aluminum and composite fiber
- 6. Propulsion-Liquid fuel engine of 440 N thrust is used for orbit raising and insertion in Martian orbit. The orbiter also has eight 22 N thrusters for attitude control or orientation Power -Electric power is generated by three solar array panels of 1.8 × 1.4 m (5 ft 10 in × 4 ft 7 in) each (7.56 m2 (81.4 sq ft) total), for a maximum of 840 W generation in Martian orbit. Electricity is stored in a 36 Ah Liion battery.[
- 7. PSLV-C25 carrying the Mars Orbiter Mission spacecraft was launched from Sriharikota on 05 November 2013
- 8. TELEMETRY AND COMMAND The Indian Space Research Organisation Telemetry, Tracking and Command Network performed navigation and tracking operations for the launch with ground stations at Sriharikota, Port Blair, Brunei and Biak in Indonesia,[32] and after the spacecraft's apogee became more than 100,000 km, two large 18-metre and 32metre diameter antennas of the Indian Deep Space Network started to be utilised.[33] NASA's Deep Space Network is providing position data through its three stations located in Canberra, Madrid and Goldstone on the U.S. West Coast during the non-visible period of ISRO's network.[34] The South African National Space Agency's (SANSA) Hartebeesthoek (HBK) ground station is also providing satellite tracking, telemetry and command services.[35] Additional monitoring is provided by technicians on board two leased ships from the Shipping Corporation of India, SCI Nalanda and SCI Yamuna which are currently in position in the South Pacific near Fij
- 9. Timeline of operations Phase Date Event Detail Result 5 November 2013 09:08 UTC Launch Burn time: 15:35 min in 5 stages Apogee: 23,550 km 6 November 2013 19:47 UTC Orbit raising manoeuvre Burn time: 416 sec Apogee: 23,550 km to 28,825 km 7 November 2013 20:48 UTC Orbit raising manoeuvre Burn time: 570.6 sec Apogee: 28,825 km to 40,186 km 8 November 2013 20:40 UTC Orbit raising manoeuvre Burn time: 707 sec Apogee: 40,186 km to 71,636 km 10 November 2013 UTC Orbit raising manoeuvre Incomplete burn Apogee: 71,636 km to 78,276 km 11 November 2013 23:33 UTC Orbit raising manoeuvre (supplementary) Burn time: 303.8 sec Apogee: 78,276 km to 118,642 km 15 November 2013 19:57 UTC Orbit raising manoeuvre Burn time: 243.5 sec Apogee: 118,642 km to 192,874 km 30 November 2013, 19:19 UTC Trans-Mars Injection (TMI) Burn time: 1328.89 sec Successful heliocentric insertion Heliocentric phase December 2013 - September 2014 En route to Mars - The probe is currently travelling a distance of 780 million kilometres (484 million miles) to reach Mars. The plan includes four trajectory correction manoeuvres-the first is on December 11, 2013, the second will be in April 2014, the third in August 2014, and the last in September 2014. Martian phase 24 September 2014 (planned) Mars Orbit Insertion (MOI) manoeuvre Geocentric phase
- 11. ANSHA KOHLI RADHA PAREKH GAURAV RAI DEVANSH CHOUDAHA