Sunday, December 7, 2008

MOON IMPACT PROBE INSERTION-CHANDRAYAAN

[edit] Injection of MIP on lunar surface

The Moon Impact Probe took this close-up picture of the moon's surface during its descent.

The Moon Impact Probe (MIP) crash-landed on the lunar surface on 14 November 2008, 15:01 UTC (20:31 Indian Standard Time (IST)) near Shackleton Crater at the south pole.The MIP was one of eleven scientific instruments (payloads) onboard Chandrayaan-1.

The MIP separated from Chandrayaan at 100 km from lunar surface and began its nosedive at 14:36 UTC (20:06 IST) going into a free fall for thirty minutes.As it fell, it kept sending information back to the mother satellite which, in turn, beamed the information back to earth. The altimeter then also began recording measurements to prepare for a rover to land on the lunar surface during a second moon mission planned for 2012. When the MIP was closer to the surface, rockets were fired to slow down its speed and to soften impact

Following the successful deployment of MIP, the other scientific instruments will be turned on one-by-one starting the next phase of the two-year mission.


LUNAR ORBIT INSERTION-CHANDRAYAAN MISSION PROFILE

Chandrayaan-1 successfully completed the lunar orbit insertion operation on 8th Nov 2008 at 16:51 IST. This manoeuvre involved firing of the liquid engine for 817 seconds (about thirteen and half minutes) when the spacecraft passed within 500 km from the moon. The satellite was placed in an elliptical orbit that passed over the polar regions of the moon, with 7502 km aposelene (point farthest away from the moon) and 504 km periselene (nearest to the moon). The orbital period was estimated to be around 11 hours. With the successful completion of this operation, India became the fifth nation to put a vehicle in lunar orbit.

First orbit reduction

First Lunar Orbit Reduction Manoeuvre of Chandrayaan-1 was carried out successfully on 9 November 2008 at 20:03 IST. During this, the engine of the spacecraft was fired for about 57 seconds. This reduced the periselene from 504 km to 200 km while aposelene remained unchanged at 7,502 km. In this elliptical orbit, Chandrayaan-1 took about ten and a half hours to circle the moon once.

Second orbit reduction

This manoeuvre, which resulted in steep decrease in Chandrayaan-1’s aposelene from 7,502 km to 255 km and its periselene from 200 km to 187 km, was carried out on 10 November 2008 at 21:58 IST. During this manoeuvre, the engine was fired for about 866 seconds (about fourteen and half minutes). Chandrayaan-1 took two hours and 16 minutes to go round the Moon once in this orbit.

Third orbit reduction

Third Lunar Orbit Reduction was carried out by firing the on board engine for 31 seconds on 11 November 2008 at 18:30 IST. This reduced the periselene from 187 km to 101 km, while the aposelene remained constant at 255 km. In this orbit Chandrayaan-1 took two hours and 9 minutes to go round the Moon once

Final orbit

Chandrayaan-1 spacecraft was successfully placed into a mission specific lunar polar orbit of 100 km above the lunar surface on 12 November 2008.In the final orbit reduction manoeuvre, Chandrayaan-1’s aposelene was reduced from 255 km to 100 km while the periselene was reduced from 101 km to 100 km.In this orbit, Chandrayaan-1 takes about two hours to go round the moon once. Two of the 11 payloads – the Terrain Mapping Camera (TMC) and the Radiation Dose Monitor (RADOM) – have already been successfully switched on. The TMC has successfully taken pictures of both the Earth and the moon.

CHANDRAYAAN-1-MISSION ISRO TEAM

The scientists considered instrumental to the success of the Chandrayaan-1 project are:

  • G. Madhavan Nair – Chairman, Indian Space Research Organisation
  • Dr.T. K. Alex – Director, ISAC (ISRO Satellite Centre)
  • Mylswamy Annadurai– Project Director, Chandrayan-1
  • S. K. Shivkumar – Director - Telemetry, Tracking and Command Network.
  • Mr.M.Pitchaimani – Operations Director, Chandrayan-1
  • Mr.Leo Jackson John – Spacecraft Operations Manager, Chandrayan-1
  • Dr.K.Radhakrishnan – Director, VSSC
  • George Koshi –Mission Director,PSLV-C11
  • Srinivasa Hegde – Mission Director,Chandrayaan-1
  • M C Dattan – Director of the Satish Dhawan Space Centre,Sriharikota
  • Prof.J N Goswami – Director of Physical Research Laboratory,Ahemadabad and Principal Scientific Investigator of Chandrayaan-1

CHANDRAYAAN-SPECIFICATION

Specifications
Mass
1380 kg at launch, 675 kg at lunar orbit,and 523 kg after releasing the impactor.
Dimensions
Cuboid in shape of approximately 1.5 m
Communications
X band, 0.7 m diameter parabolic antenna for payload data transmission. The Telemetry, Tracking & Command (TTC) communication operates in S band frequency.
Power
The spacecraft is mainly powered by its solar array, which includes one solar panel covering a total area of 2.15 x 1.8 m generating 700 W of power, which is stored in a 36 A·h lithium-ion battery.The spacecraft uses a bipropellant integrated propulsion system to reach lunar orbit as well as orbit and altitude maintenance while orbiting the Moon.

Thursday, November 13, 2008

PLACING INDIAN FLAG ON LUNAR SURFACE

The Indian moon mission is not just about science; it is also about India's coming out party on the world stage having sealed the nuclear deal with the United States.

In attempting to place the Indian flag on the moon's surface, if successful, it would make India just the fourth country in the world to have ever done so after Russia, America and Japan.

The flag will fly all the 4,00,000 kilometers to the moon on Chandrayaan-1 and on command from Indian space scientists, it will hurtle down to the moon's surface.

Called the Moon Impact Probe, this 35 kilogram computer monitor sized instrument was included on Chandryaan-1 at the behest of former President APJ Abdul Kalam.

Kalam felt that India's tricolor should be firmly placed on the moon sooner than later so that whenever the lunar resources are ever shared by the world community, India should get its rightful share and not be left out.

This will be the very first task that Chandrayaan-1 will perform when it reaches its designated 100 kilometer circular orbit around the moon.

And to execute it successfully, the space scientists have designed a proper course of action.

Once the space shuttle Chandrayaan-1 reaches the lunar orbit it will be reoriented for the special task.

Then, a small square carton sized instrument, which was carried piggyback on the Indian satellite, will be released on command.

With the mother craft (Chandrayaan-1) keeping a watchful eye, the small probe, powered with its own rockets, will hurtle down 100 kilometers to strike the lunar surface at a designated spot -- a challenging task indeed.

On its way down it will take images of the moon, analyze the moon's atmosphere and when it strikes the moon's surface at high speed it will also instantaneously analyze the moon's soil and transmit its data back to the mother craft that will be closely listening to its calls.

Most importantly, this probe would have placed India's tricolor on the moon surface for howsoever short-lived a moment may be before the instruments gets shattered on hard impact, heralding India's arrival on the moon!

The only other countries to have attempted such a feat are Russia, America and Japan.

The last time such a deliberate attempt to successfully hard land robots on the moon surface done was more than three decades ago when Russia placed instruments as part of its Luna 24 mission in 1976.

Since then no country has tried this at all and India attempts this challenging task on its maiden mission, making it a stride ahead of its regional rival China.

Commenting on the mission, Dr G Madhavan Nair, Chairman, ISRO, said, "We have the Indian flag built in it, we are going to drop the Indian flag on the moon surface when the mission is getting completed."

To take a look at this very unique experiment, NDTV went up close to the satellite; even climbed up very near the Chandrayaan-1 and checked out the small box that carries with it the dreams of a billion plus Indians.

CHANDRAYAAN REACHED 100 KM FORM LUNAR SURFACE

Matt_dk writes "Today, Chandrayaan-1 spacecraft has successfully reached its intended operational orbit at a height of about 100 km from the lunar surface. This followed a series of three orbit reduction manoeuvres conducted during the past three days by repeatedly firing the spacecraft's 440 Newton Liquid Engine. The next major event of Chandrayaan-1 mission planned in the coming days is the release of Moon Impact Probe (MIP) from the spacecraft and its eventual hitting of the moon's surface."

INDIAN FLAG ON MOON

NEW DELHI: Two days before the launch of India's first lunar orbiter, chairman of the Indian Space Research Organisation (ISRO) G. Madhavan Nair
said on Monday that India will plant its flag on the moon to help establish its presence on the earth's only natural satellite.

India will drop its flag on the moon to establish its presence, Nair said in an interview. This will make India the fourth country after the US, Russia, and Japan to have its flag on the moon.

Asked for the geopolitical reason behind the planting of the flag, Nair said: "Today, as per the international charter, the moon belongs to the global community. Nobody can make special claim on the surface. But in due course, we don't know how things will change. But our presence will be established through this mission."

Nair also reiterated in the interview that ISRO planned to put a man in space by 2015. "If certain finer observation are to be made, online decisions have to be made, the presence of man becomes important," he said.

"The man behind the instrument. And also the reaction time for any decision will be a fraction of a second, whereas you know it takes almost eight seconds for the data to come from the moon to the earth and then again sent back and so on, and here also somebody has to analyse....so ultimately if you want to do a perfect experiment, man behind the instrument is a must."

Nair said it would cost around Rs.100 billion to put a man in space. However, he added, "in the Indian context we are committed to taking the space technology for grass root applications. We have done that and we will continue to do so. So nearly 80 percent of the budget is going to be spent on programmes which are relevant to the common man."

The lunar orbiter mission Chandrayaan that will be launched Wednesday will look for water on the moon, Nair confirmed. "If you are thinking of establishing lunar colony, water is essential element for that and if from it you can generate oxygen, and also if you can decompose and generate into fuel which is required for interplanetary travel, so the presence of water is a very-very important element for further exploration."

Nair also confirmed that the mission would look for Helium-3, one of the fuels for nuclear fusion. "Even one tonne of that can sustain the entire country's energy for one year," he pointed out. Reiterating that there was Helium-3 on the moon, he added: "Is it in abundant quantity, whether we can exploit, these are question marks."

The ISRO chief said that after the moon, the organisation had its sights set on Mars. "The GSLV can take a nearly 500 kg spacecraft to Mars. So if there are good ideas about experimental exploration of that system we can have the Mars mission and in about 3-4 years."

"If we want to maintain our leadership naturally we have to have the scientific goals which is set ahead so that we can be really either at par or ahead of the others in some of the fields. So this is a really challenging task. We believe that India, such a big nation, huge resources, both natural and human resource... we should be in leadership position as far as our space technology is concerned."

Asked if the space programme was cost effective, Nair said that for every rupee spent, ISRO gave back Rs.1.50 to the Indian society. "That is the first part of it. The second part is, the human resource and the technology we create, that is not valued. That is tremendous."

Asked if India have a colony on the moon sometime, Nair said: "We cannot lag behind others in this race. We have to really catch up and we should have our own technology for the manned capsule.

"Of course initial thing would be around earth itself, then from there how to send a man to the moon etc has to be considered. And today with the economic growth what you are seeing in the country this is affordable.

"And a very small fraction of the national budget we spend on space technology. It is really worth it. In fact if you take the entire budget for the space programme it is like 0.2-0.3 (percent) of the national budget. So it is very small compared to...others are using even up to 2 or 3%."

Tuesday, October 28, 2008

GROUND SEGMENT FOR CHANDRAYAAN-1 MISSION

GROUND SEGMENT FOR CHANDRAYAAN-1 MISSION
The Ground Segment for Chandrayaan-1 comprises of three major elements : the Ground Station Network including the Indian Deep Space Network (IDSN), Mission Operations Complex (MOX)and Indian Space Science Data Centre (ISSDC). This trio of ground facility ensures the success of the mission by providing to and fro conduit of communication, securing good health of the spacecraft, maintaining the orbit and attitude to the requirements of the mission and conducting payload operations. The ground segment is also responsible for making the science data available for the Payload Scientists along with auxiliary information, in addition to archiving of payload and spacecraft data. Payload Operation Centres (POCs) also form a part of the Ground Segment.
Elements of Ground Segment

ABOUT PSLV-Polar Satellite Launch Vehicle

Polar Satellite Launch Vehicle
The Indian Space Research Organisation (ISRO) built its first Polar Satellite Launch Vehicle (PSLV) in the early 90s. The 45 m tall PSLV with a lift-off mass of 295 tonne, had its maiden success on October 15, 1994, when it launched India's IRS-P2 remote sensing satellite into a Polar Sun Synchronous Orbit (SSO) of 820 km altitude. Since its first successful launch in 1994, PSLV has launched nine Indian Remote Sensing satellites as well as two micro satellites HAMSAT and IMS-1 built by ISRO, a recoverable space capsule SRE-1, and fourteen small satellites for foreign customers into polar Sun Synchronous Orbits. Besides, it has launched one Indian meteorological satellite Kalpana-1 into Geosynchronous Transfer Orbit (GTO). PSLV has emerged as ISRO's workhorse launch vehicle and proved its reliability and versatility by scoring continuous successes in launching multiple payloads to both SSO as well as GTO.

Considering the maturity of Polar Satellite Launch Vehicle (PSLV) demonstrated through various performances, PSLV is chosen for the first lunar mission. The upgraded version of PSLV viz., PSLV-XL (PSLV-C11) will be used to inject the 1380 kg mass spacecraft into a 255 x 22860 km orbit.

PSLV has four stages, using solid and liquid propulsion systems alternately. Six strap-on motors augment the first stage thrust. PSLV-XL is the upgraded version of PSLV. In PSLV-XL, the six strap-on motors carry 4 tonne more propellant compared to PSLV; There is also an increase in the length of each strap-on.

PAYLOAD INFORMATION OF CHANDRAYAAN 1

Scientific Payloads
Chandrayaan-1 is an Indian Mission to the Moon. The indigenously developed payload/ experiments are:
TMC
TMC
Terrain Mapping stereo Camera (TMC) in the panchromatic band, having 5 m spatial resolution and 20 km swath
Read More..
HySi
HySI
Hyper Spectral Imaging camera (HySI) operating in 400-950 nm bands with a spectral resolution better than 15 nm and spatial resolution of 80 m with a swath of 20 km
Read More..
LLRI
LLRI
Lunar Laser Ranging Instrument (LLRI) with height resolution of less than 5 m
Read More..
HEX
HEX
High Energy X-ray spectrometer (HEX) using Cadmium-Zinc-Telluride (CdZnTe) detector in the 30-270 keV energy region with spatial resolution of 33 km
Read More..
MIP
MIP
Moon Impact Probe (MIP) as piggyback on the main orbiter of the Chandrayaan-1 spacecraft, which will impact on the surface of the moon.
Read More..
Apart from the above indigenous payloads/experiments, ISRO solicited proposals through an Announcement of Opportunity (AO) from International and Indian Scientific Community for participating in the mission by providing suitable scientific payloads, complementing the overall Chandrayaan-1 scientific objectives. Out of the proposals received, six experiments were selected for inclusion in Chandrayaan-1 mission; two of the AO payloads, C1XS and SARA are developed by ESA jointly with ISRO.
The AO payloads Onboard Chandrayaan-1 are:
C1XS
C1XS
Chandrayaan-1 X-ray Spectrometer (C1XS) through ESA - a collaboration between Rutherford Appleton Laboratory,UK and ISRO Satellite Centre, ISRO. Part of this payload is redesigned by ISRO to suit Chandrayaan-1 scientific objectives.
Read More..
SIR-2
SIR-2
Near Infra Red spectrometer (SIR-2) from Max Plank Institute for Solar System Science, through Max-Planck Society, Germany and ESA
Read More..
SARA
SARA
Sub keV Atom Reflecting Analyser (SARA) through ESA, from Swedish Institute of Space Physics, Sweden and Space Physics Laboratory, Vikram Sarabhai Space Centre, ISRO. The digital processing unit of this payload/ experiment is designed and developed by ISRO, while Swedish Institute of Space Physics develops the payload.
Read More..
RADOM
RADOM
Radiation Dose Monitor Experiment (RADOM) from Bulgarian Academy of Sciences.
Read More..
Mini SAR
Mini-SAR
Miniature Synthetic Aperture Radar (Mini-SAR) from Applied Physics Laboratory, Johns Hopkins University and Naval Air Warfare Centre, USA through NASA
Read More..
M3
M3
Moon Mineralogy Mapper (M3) from Brown University and Jet Propulsion Laboratory, USA through NASA
Read More..
Summary of Chandrayaan-1 Prime Science Objectives and Wavelength range coverage
Prime Objectives Payload
  • Search for water-ice
  • MiniSAR, HEX, SARA
  • Chemical Mapping
  • C1XS, HEX
  • Mineralogical Mapping
  • HySI, SIR-2, M3
  • Topography Mapping
  • LLRI,TMC
  • Radiation Environment
  • RADOM, HEX, C1XS
  • Magnetic Field Mapping
  • SARA
  • Volatile Transport
  • HEX
  • Lunar Atmospheric constituent
  • MIP

    CHANDRAYAAN 1 SPACE CRAFT DESCRIPTION

    Description
    Spacecraft for lunar mission is :
  • Cuboid in shape of approximately 1.5 m side.
  • Weighing 1380 kg at launch and 675 kg at lunar orbit.
  • Accommodates eleven science payloads.
  • 3-axis stabilized spacecraft using two star sensors, gyros and four reaction wheels.
  • The power generation would be through a canted single-sided solar array to provide required power during all phases of the mission. This deployable solar array consisting of a single panel generates 750W of peak power. Solar array along with yoke would be stowed on the south deck of the spacecraft in the launch phase. During eclipse, spacecraft will be powered by Lithium ion (Li-Ion) batteries.
  • After deployment, the solar panel plane is canted by 30ยบ to the spacecraft pitch axis.
  • The spacecraft employs a X-band, 0.7m diameter parabolic antenna for payload data transmission. The antenna employs a dual gimbal mechanism to track the earth station when the spacecraft is in lunar orbit.
  • The spacecraft uses a bipropellant integrated propulsion system to reach lunar orbit as well as orbit and attitude maintenance while orbiting the Moon.
  • The propulsion system carries required propellant for a mission life of 2 years, with adequate margin.
  • The Telemetry, Tracking & Command (TTC) communication is in S-band frequency.
  • The scientific payload data transmission is in X-band frequency.
  • The spacecraft has three Solid State Recorders (SSRs) Onboard to record data from various payloads.
  • SSR-1 will store science payload data and has capability of storing 32Gb data.
  • SSR-2 will store science payload data along with spacecraft attitude information (gyro and star sensor), satellite house keeping and other auxiliary data. The storing capacity of SSR-2 is 8Gb.
  • M3 (Moon Mineralogy Mapper) payload has an independent SSR with 10Gb capacity.

    CHANDRAYAAN 1 MISSION PROFILE

    Mission Sequence
  • Chandrayaan-1 spacecraft would be launched from the Satish Dhawan Space Centre, SHAR, Sriharikota by PSLV-XL (PSLV-C11) in an highly elliptical initial orbit (IO) with perigee (nearest point to the Earth) of about 257 km and an apogee (farthest point from the Earth) of about 22,858 km.
  • After a few revolutions in the initial orbit, the spacecraft's Liquid Apogee Motor (LAM) firing would be done, when the spacecraft is near perigee, to raise the apogees to 37,421 km and 73,925 km respectively.
  • Subsequently, the LAM is fired to take the Chandrayaan-1 spacecraft to extremely high elliptical orbit with apogees 199,277 km and 269,201 km. Later the spacecraft would be raised to an orbit with 1,019 km perigee and 386,194 km apogee.
  • Once the Chandrayaan-1 spacecraft reaches the vicinity of the Moon, the spacecraft is slowed down sufficiently so as to enable the gravity of the moon capture it into an elliptical orbit (LC). After a careful and detailed observation the height of the spacecraft's orbit will be finally lowered to its intended 100 km circular polar orbit. Following this, the Moon Impact Probe (MIP) would be ejected from Chandrayaan-1 to impact on the lunar surface. Afterwards, all the scientific instruments/payloads are commissioned sequentially and Chandrayaan-1 spacecraft explores the Moon with its array of instruments for two years.
    Chandrayaan-1 Mission Phase

    CHANDRAYAAN 1 -SCIENTIFIC OBJECTIVES AND MISSION OBJECTIVES

    Scientific Objectives
    The Chandrayaan-1 mission is aimed at high-resolution remote sensing of the moon in visible, near infrared (NIR), low energy X-rays and high-energy X-ray regions. Specifically the objectives are
  • To prepare a three-dimensional atlas (with high spatial and altitude resolution of 5-10 m) of both near and far side of the moon.
  • To conduct chemical and mineralogical mapping of the entire lunar surface for distribution of mineral and chemical elements such as Magnesium, Aluminum, Silicon, Calcium, Iron and Titanium as well as high atomic number elements such as Radon, Uranium & Thorium with high spatial resolution.
    The Simultaneous photo geological, mineralogical and chemical mapping through Chandrayaan-1 mission will enable identification of different geological units to infer the early evolutionary history of the Moon. The chemical mapping will enable to determine the stratigraphy and nature of the Moon's crust and thereby test certain aspects of magma ocean hypothesis. This may allow to determine the compositions of impactors that bombarded the Moon during its early evolution which is also relevant to the formation of the Earth.
    Radiation Environment
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    Radiation Environment of the Moon
    Radiation environment of the Moon produced by solar radiation and solar and galactic cosmic rays: The reflectance spectrum is useful for mineral identification, the fluorescent X-ray spectrum and solar and galactic cosmic-ray produced gamma radiation for chemical mapping, and radiogenic gamma and alpha particle spectrum for mapping of radioactive nuclides (U, Th, K, etc.) and in understanding the leakage of radon from the lunar interior and its transport on the lunar surface. The uranium decay chain, which produces 222Rn and its daughters, forming a thin 'paint' on the lunar surface, are shown on the right. The temperature regimes on the sunlit and night side of the Moon and the permanently shadowed cold Polar Regions are shown schematically. (Ref: Current Science, Bhandari 2004)
    Mission Objectives
  • To realise the mission goal of harnessing the science payloads, lunar craft and the launch vehicle with suitable ground support systems including Deep Space Network (DSN) station.
  • To realise the integration and testing, launching and achieving lunar polar orbit of about 100 km, in-orbit operation of experiments, communication/ telecommand, telemetry data reception, quick look data and archival for scientific utilisation by scientists.

    CHANDRAYAAN PAY LOD PHOTO GALLERY-

    HySI
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    LLRI

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    HEX
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    MIP

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    C1XS
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    SIR-2
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    CHANDRAYAAN PHOTO GALLERY-PAY LOADS-TMC

    INDIAN MOON TRIP LAUNCHING SITE BEFORE LAUNCHING



    The fully assembled PSLV-C11, which will launch Chandrayaan-1 on October 22, stands encased in the Vehicle Assembly Building of the second launch pad at Sriharikota on Saturday. In the foreground is the launch pad to which the PSLV -C11 will be wheeled on rail tracks on October 18.

    SRIHARIKOTA: If all goes well, Chandrayaan-1 spacecraft, to be launched by the Polar Satellite Vehicle (PSLV-C11) on October 22 at 6.20 a.m. from the Sriharikota space port, will reach the lunar orbit on November 8, according to M.Y.S. Prasad, Associate Director, Satish Dhawan Space Centre, Sriharikota.

    About 1,000 engineers and technicians of the Indian Space Research Organisation (ISRO) have rolled up their sleeves and are working hard for the past two months to ensure a flawless launch. The 52-hour countdown will begin on October 20 at 4 a.m.

    On Saturday, the PSLV-C11, which is 44.4 metres tall and weighs 316 tonnes, looked majestic in the huge Vehicle Assembly Building (VAB) of the state-of-the-art second launch pad on the Sriharikota island. As it gleamed in white and brown colours, the VAB’s massive doors, in contrast, shone in speckled grey.

    “All checks on the vehicle are completed. The vehicle is now ready to receive the satellite,” declared T. Subba Reddy, Manager, Second Launch Pad, when journalists visited the complex.

    A few kilometres away, Chandrayaan-1 spacecraft, which weighs 1,380 kg, is undergoing a battery of tests to test its flight-worthiness.

    The spacecraft will be moved to the VAB on October 14 and married up with the PSLV-11. The “marriage ceremonies” such as filling Chandrayaan-1 with propellants and gas, and cobbling of the heat-shield which protects the spacecraft through searing heat when the rocket climbs through the atmosphere, will be performed over the next four days. On October 18 will begin the extremely slow journey of the rocket with the spacecraft, as if it were a temple chariot with the deity, from the VAB to the launch pad.

    The PSLV, which stands on a mobile platform, will be wheeled on rail tracks to the launch pad, also called the umbilical tower, which is one km away. A powerful hydraulic bogey system will slowly pull the vehicle. The one-km journey will take two hours!

    “The movement of the vehicle to the launch pad will take place on October 18. There will be minimum four days of work on the launch pad. The launch will take place on October 22 at 6.20 a.m., provided the weather supports us,” said M.C. Dathan, Director, Satish Dhawan Space Centre, Sriharikota.

    However, V. Krishnamurthy, the Range Safety Officer for the mission, is a confident man. “Rains do not matter. The launch vehicle is rain-proof. It can get drenched and we can still launch,” he asserted.

    The PSLV had lifted off earlier when it was pouring over the island. Only a cyclone would pose a problem to the launch on time. Since this was the time when the north-east monsoon set in, Mr. Krishnamurthy said ISRO had formed a team of weather specialists who would be in Sriharikota six days before the launch.

    Depending on their inputs, ISRO would take a decision on when to ignite the rocket.

    Mission-life

    Chandrayaan-1 will carry 730 kg of propellants. About 600 kg of these propellants will be used to put the spacecraft into lunar orbit at an altitude of 100 km. The spacecraft will have a mission-life of two years and use up 70 kg of propellants during this period, Mr. Prasad said.

    Chandrayaan-1 has 11 scientific payloads — five from India and six from abroad. The payloads from abroad includes those from NASA, the European Space Agency and Bulgaria. The payloads will map the chemicals and minerals on the moon, and also prepare a 3-diemensional map of the entire lunar surface. The mission will also give clues on the early origin of the moon.

    Mr. Prasad said, “We will be able to confirm whether there is water on the surface of the moon near the Poles with the help of the Chandrayaan mission.” Water on the moon was first identified by a NASA mission called Clementine. Based on that, NASA concluded that there could be a possibility of water in the moon’s South Pole, he added.

    Moon Impact Probe

    S. Satish, Director, Publications and Public Relations, ISRO, said an important Indian payload on the Chandrayaan-1 was the Moon Impact Probe (MIP). When the spacecraft reached the lunar orbit at an altitude of 100 km, the MIP would eject from Chandrayaan. As the MIP sped towards the moon’s surface, its video-camera would take pictures of the lunar surface. Its altimeter would measure the instantaneous altitude from the moon. A third instrument, a mass spectrometer, would sniff the tenuous atmosphere above the moon.

    V. Seshagiri Rao, Deputy Director, Range Operations, Sriharikota, said each payload on the Chandrayaan, was subjected to different tests at Sriharikota. Experts sat in front of consoles and watched the differences in parameters when the payloads were tested. The tests related to solar panel deployment as well.