2. CONTENTS
About Vijnana Bharati & VSF
Mission Mars – Mangalyaan
About ISRO, launch vehicles
Why Mission Mars?, Objectives
Mangalyaan the spacecraft configuration
The MoI event
Payload on Mangalyaan.
3. About Vijnana Bharati
Established in Nagpur in 1991
Is a national organization of the scientific community
of India. A “swadeshi Vijnana Parishad”
Is working for the propagation of science, including
India’s traditional scientific knowledge
Has its 21 branches all over India and 5 in Middle
East countries including Saudi Arabia
Has distinguished scientists associated with it in
different capacities
4. Vijnana Bharati
National president - Dr. Vijay Bhatkar
Patron - Dr. G Madhavan Nair
Former space commission chairman
Patron - Dr. Anil Kakodkar
Former chairman of Atomic energy
commission
5. Vijnana Bharati
Vijnana Bharati has different wings working in different
specialized areas of Science
Vigyan Prasar Bharati (VPB)
National Ayurveda Students And Youth Association
(NASYA)
World Ayurveda Congress (WAC)
Vishwa Veda Vigyan Sammelan (VVVS)
The Women Empowerment Movement (SHAKTI)
Rashtriya Yuva Vaigyanik Manch (RYVM)
6. Benefits of VSF to institutions
Meet the Scientist sessions at your institution
either in person or
through Webinars.
Popular science talks at your institution
Visit of students to Science laboratories in the
region.
Science related competitions.
Do it yourself - simple experiments to understand
scientific concepts
11. Why Mission to Mars?
Similarities with Earth
Mars also has elliptical orbit like Earth and similar -
Surface conditions
Similar geology
Availability of water?
Atmosphere (thin)
Polar ice caps
Magnetic field
Natural conditions similar to arctic and Antarctic
12. Mars is like EARTH
Large river valleys
‘Super’ grand canyon
14. Mars is like EARTH
Climate range similar to Earth
Sky and clouds, dust storms
15. To develop the technologies required for an
interplanetary mission.
Design and realisation 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.
Scientific Objectives are - Exploration of Mars surface
features, morphology, mineralogy and Martian atmosphere by
indigenous scientific instruments.
16.
17. The satellite structure is of aluminium and composite fibre
reinforced plastic (CFRP) sandwich construction
18.
19. The lift-off mass was 1,350 kg, including 852 kg of propellant
mass.
Cuboid in shape of approximately 1.5 m (4 feet 11
inches).
20. Electric power is generated by three solar array panels of 1.8 m × 1.4 m
each 7.56 Sqm, for a maximum of 840 W generation in Martian orbit.
Electricity is stored in a 36 Ah Li-ion battery.
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.
The antenna array consists of a low-gain antenna, a medium-gain antenna
and a high-gain antenna. The High-gain antenna system is based on a
single 2.2-metre reflector illuminated by a feed at S-band. It is used to
transmit and receive the telemetry, tracking, commanding and data to and
from the Indian Deep Space Network.
21. The 15 kg scientific payload
consists of five instruments:
LAP Lyman-Alpha Photometer 1.97 kg
MSM Methane Sensor For Mars 2.94 kg
MENCA Mars Exospheric Neutral Composition Analyser 3.56 kg
TIS Thermal Infrared Imaging Spectrometer 3.20 kg
MCC Mars Colour Camera 1.27 kg