
PSLV puts Mars orbiter precisely into earth-orbit; trip to the Red Planet will take more than 300 days
The nation’s prestigious interplanetary mission to Mars, 40 crore km
away, got off to a flying start on Tuesday when the Indian Space
Research Organisation’s trusty Polar Satellite Launch Vehicle (PSLV-C25)
roared off the first launch pad of the spaceport at Sriharikota at 2.38
p.m. and put the Mars orbiter precisely into its earth-orbit about 44
minutes later.
This was the first crucial and difficult step in the ISRO’s Mars Orbiter
Mission. However, the XL version of the PSLV achieved it with aplomb.
The elliptical orbit achieved was so accurate that against the predicted
perigee of 250 km and an apogee of 23,500 km, it went into an orbit of
246.9 km x 23,566 km.
The spacecraft first going into orbit around the earth signalled the
start of its 300-day voyage to the Red Planet. If everything goes well
during this complex and challenging journey through deep space, it will
be put into the Mars orbit on September 24, 2014.
Mission highlights
Two mission highlights are: it was the longest PSLV mission at 44
minutes — the previous missions lasted about 18 minutes, and this was
the silver jubilee lift-off of the PSLV. Out of the 25 launches, 24 had
been successful in a row.
Suspense filled the newly-built Mission Control Centre (MCC) when there
was a long coasting phase of 25 minutes between the PSLV’s third stage
burnout and the fourth stage ignition.
Tension gripped the MCC again for about half-a-minute for it was only 37
seconds after the fourth stage burnout that the spacecraft was put into
orbit. But all this was as planned.
The ISRO scientists’ cup of joy overflowed when M.S. Pannirselvam, Range
Operations Director, PSLV-C25, announced tersely from the MCC,
“Spacecraft separation achieved. It has been successfully put into
orbit.”
Asked later how he felt when he made the announcement, he said, “We had no feeling. We were doing our job.”
Applause erupted when ISRO Chairman K. Radhakrishnan, who did not hide
his joy, turned towards his colleagues in the MCC and acknowledged their
cheers with folded hands. He called the flight a copybook and textbook
mission. It was a new and complex mission in design and execution, he
said.
Project Director of Mars Orbiter S. Arunan called it an “excellent
mission.” The primary and secondary panels and the high gain antenna of
the spacecraft had been deployed. “The spacecraft is in good heath,” he
said.
Yash Pal, former Member of the Space Commission, called the successful mission ISRO’s “very very special gift to the nation.”
Long way to go
All former and present brass of ISRO tried to temper the delight by
cautioning that “there was a long way to go in time and distance” before
the orbiter was put into the Martian orbit in September 2014. They
included present top engineers S. Ramakrishnan, M.Y.S. Prasad, A.S.
Kiran Kumar, S.K. Shivakumar, M.C. Dathan, P. Kunhikrishnan and the
former ISRO chairmen, U.R. Rao and K. Kasturirangan. They emphasised
that “while the first job has been successfully done, a long journey
lies ahead.”
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.
Spacecraft
The spacecraft structure and propulsion hardware configurations are similar to Chandrayaan 1, India's first successful robotic lunar orbiter that operated from 2008 to 2009, with specific improvements and upgrades needed for a Mars specific mission.
Mass
The lift-off mass was 1350 kg, including 852 kg of propellant mass.
Dimensions
Cuboid in shape of approximately 1.5 m
Bus
The spacecraft's bus is a modified I-1 K structure and propulsion hardware configurations similar to Chandrayaan 1, India's successful lunar orbiter that operated from 2008 to 2009, with specific improvements and upgrades needed for a Mars mission. The satellite structure is of aluminum and composite fiber reinforced plastic (CFRP) sandwich construction.
Power
Electric power is generated by three solar array panels of 1.8 m X 1.4 m each (7.56 m2 total), for a maximum of 840 W generation in Martian orbit. Electricity is stored in a 36 Ah Li-ion battery.
Propulsion
Liquid fuel engine of 440 N thrust is used for orbit raising and insertion in Martian orbit.
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. The High-gain antenna system is based on a single 2.2 meter 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.
Payload
The 15 kg (33 lb) scientific payload consists of five instruments:
Atmospheric studies
Lyman-Alpha Photometer (LAP) — a photometer that measures the relative abundance of deuterium and hydrogen from Lyman-alpha emissions in the upper atmosphere. Measuring the deuterium/hydrogen ratio will allow the amount of water loss to outer space to be estimated.
Methane Sensor For Mars (MSM) — will measure methane in the atmosphere of Mars, if any, and map its sources.
Particle environment studies
Mars Exospheric Neutral Composition Analyzer (MENCA) — is a quadrupole mass analyzer capable of analyzing the neutral composition of particles in the exosphere.
Surface imaging studies
Thermal Infrared Imaging Spectrometer (TIS) — will measure the temperature and emissivity of the Martian surface, allowing for the mapping of surface composition and mineralogy of Mars.
Mars Color Camera (MCC) — will provide images in the visual spectrum, providing context for the other instruments