Mangalayaan
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The Mars Orbiter Mission (MOM), also called ''Mangalyaan'', was a
space probe A space probe is an artificial satellite that travels through space to collect scientific data. A space probe may orbit Earth; approach the Moon; travel through interplanetary space; flyby, orbit, or land or fly on other planetary bodies; or ...
orbiting
Mars Mars is the fourth planet from the Sun and the second-smallest planet in the Solar System, only being larger than Mercury. In the English language, Mars is named for the Roman god of war. Mars is a terrestrial planet with a thin at ...
since 24 September 2014. It was launched on 5 November 2013 by the Indian Space Research Organisation (ISRO). It was India's first interplanetary mission and it made ISRO the fourth
space agency This is a list of government agencies engaged in activities related to outer space and space exploration. As of 2022, 77 different government space agencies are in existence, 16 of which have launch capabilities. Six government space agencie ...
to achieve Mars orbit, after
Roscosmos The State Space Corporation "Roscosmos" (russian: Государственная корпорация по космической деятельности «Роскосмос»), commonly known simply as Roscosmos (russian: Роскосмос) ...
,
NASA The National Aeronautics and Space Administration (NASA ) is an independent agencies of the United States government, independent agency of the US federal government responsible for the civil List of government space agencies, space program ...
, and the European Space Agency. It made India the first Asian nation to reach Martian orbit and the first nation in the world to do so on its maiden attempt. The Mars Orbiter Mission probe lifted-off from the First Launch Pad at
Satish Dhawan Space Centre Satish Dhawan Space Centre - SDSC (formerly Sriharikota Range - SHAR) is a rocket launch centre ( spaceport) operated by Indian Space Research Organisation (ISRO). It is located in Sriharikota, Tirupati district of Andhra Pradesh. Sriharikota ...
( Sriharikota Range SHAR),
Andhra Pradesh Andhra Pradesh (, abbr. AP) is a state in the south-eastern coastal region of India. It is the seventh-largest state by area covering an area of and tenth-most populous state with 49,386,799 inhabitants. It is bordered by Telangana to the ...
, using a
Polar Satellite Launch Vehicle The Polar Satellite Launch Vehicle (PSLV) is an expendable medium-lift launch vehicle designed and operated by the Indian Space Research Organisation (ISRO). It was developed to allow India to launch its Indian Remote Sensing (IRS) satellites ...
(PSLV) rocket C25 at 09:08 UTC on 5 November 2013. The
launch window In the context of spaceflight, launch period is the collection of days and launch window is the time period on a given day during which a particular rocket must be launched in order to reach its intended target. If the rocket is not launched wit ...
was approximately 20 days long and started on 28 October 2013. The MOM probe spent about a month in
Earth orbit Earth orbits the Sun at an average distance of 149.60 million km (92.96 million mi) in a counterclockwise direction as viewed from above the Northern Hemisphere. One complete orbit takes  days (1 sidereal year), during which time Eart ...
, where it made a series of seven
apogee An apsis (; ) is the farthest or nearest point in the orbit of a planetary body about its primary body. For example, the apsides of the Earth are called the aphelion and perihelion. General description There are two apsides in any ell ...
-raising orbital manoeuvres before
trans-Mars injection A heliocentric orbit (also called circumsolar orbit) is an orbit around the barycenter of the Solar System, which is usually located within or very near the surface of the Sun. All planets, comets, and asteroids in the Solar System, and the Sun i ...
on 30 November 2013 ( UTC). After a 298-day transit to Mars, it was put into Mars orbit on 24 September 2014. The mission was a "
technology demonstrator A technology demonstration (or tech demo), also known as demonstrator model, is a prototype, rough example or an otherwise incomplete version of a conceivable product or future system, put together as proof of concept with the primary purpose of ...
" project to develop the technologies for designing, planning, management, and operations of an interplanetary mission. It carried five scientific instruments. The spacecraft was monitored from the Spacecraft Control Centre at ISRO Telemetry, Tracking and Command Network (ISTRAC) in Bengaluru with support from the Indian Deep Space Network (IDSN) antennae at Bengaluru, Karnataka. On 2 October 2022, it was reported that the orbiter had irrecoverably lost communications with Earth after entering a seven-hour eclipse period in April 2022 that it was not designed to survive. The following day, ISRO released a statement that all attempts to revive Mangalyaan had failed and officially declared it dead, citing the loss of fuel and battery power to the probe's instruments.


History

On 23 November 2008, the first public acknowledgement of an uncrewed mission to Mars was announced by then-ISRO chairman
G. Madhavan Nair G. Madhavan Nair (born 31 October 1943) is an Indian space scientist and a former Chairman of the Indian Space Research Organisation, and Secretary to the Department of Space, Government of India. He has also been the Chairman of the Space ...
. The MOM mission concept began with a feasibility study in 2010 by the
Indian Institute of Space Science and Technology Indian Institute of Space Science and Technology (IIST) is a government-aided institute and deemed university for the study and research of space science, located at Valiamala, Nedumangad, Thiruvananthapuram, Kerala. It is the first universit ...
after the launch of lunar satellite
Chandrayaan-1 Chandrayaan-1 (, ) was the first Indian lunar probe under the Chandrayaan program. It was launched by the Indian Space Research Organisation in October 2008, and operated until August 2009. The mission included a lunar orbiter and an impact ...
in 2008. Prime Minister Manmohan Singh approved the project on 3 August 2012, after the Indian Space Research Organisation completed of required studies for the orbiter. The total project cost may be up to . The satellite costs and the rest of the budget has been attributed to ground stations and relay upgrades that will be used for other ISRO projects. The space agency had planned the launch on 28 October 2013 but was postponed to 5 November following the delay in ISRO's spacecraft tracking ships to take up pre-determined positions due to poor weather in the Pacific Ocean. Launch opportunities for a fuel-saving
Hohmann transfer orbit In astronautics, the Hohmann transfer orbit () is an orbital maneuver used to transfer a spacecraft between two orbits of different altitudes around a central body. Examples would be used for travel between low Earth orbit and the Moon, or ...
occur every 26 months, in this case the next two would be in 2016 and 2018. Assembly of the PSLV-XL launch vehicle, designated C25, started on 5 August 2013. The mounting of the five scientific instruments was completed at
Indian Space Research Organisation Satellite Centre The U R Rao Satellite Centre (URSC), formerly ISRO Satellite Centre (ISAC) ( hi, इसरो उपग्रह केंद्र) is an Indian Space Research Organisation centre for the design, development, and construction of Indian satell ...
, Bengaluru, and the finished spacecraft was shipped to Sriharikota on 2 October 2013 for integration to the PSLV-XL launch vehicle. The satellite's development was fast-tracked and completed in a record 15 months, partly due to using reconfigured
Chandrayaan-2 Chandrayaan-2 (, ; ) is the second lunar exploration mission developed by the Indian Space Research Organisation (ISRO), after Chandrayaan-1. It consists of a lunar orbiter, and also included the ''Vikram'' lander, and the ''Pragyan'' lunar ...
orbiter bus. Despite the US federal government shutdown, NASA reaffirmed on 5 October 2013 it would provide communications and navigation support to the mission "with their
Deep Space Network The NASA Deep Space Network (DSN) is a worldwide network of American spacecraft communication ground segment facilities, located in the United States (California), Spain (Madrid), and Australia (Canberra), that supports NASA's interplanetary ...
facilities.". During a meeting on 30 September 2014, NASA and ISRO officials signed an agreement to establish a pathway for future joint missions to explore Mars. One of the working group's objectives will be to explore potential coordinated observations and science analysis between the
MAVEN MAVEN is an American spacecraft orbiting Mars to study the loss of its atmospheric gases to space, providing insight into the history of the planet's climate and water. The spacecraft name is an acronym for "Mars Atmosphere and Volatile Evolu ...
orbiter and MOM, as well as other current and future Mars missions. On 2 October 2022, it was reported that the orbiter had irrecoverably lost communications with Earth after entering long eclipse period in April 2022 that it was not designed to survive. At the time of communications loss it was unknown whether the probe had lost power or inadvertently realigned its Earth-facing antenna during automatic maneuvers.


Team

Some of the scientists and engineers involved in the mission include: *
K. Radhakrishnan Koppillil Radhakrishnan (born 29 August 1949) is an Indian space scientist who headed the Indian Space Research Organisation (ISRO) between November 2009 and December 2014 as Chairman of Space Commission, Secretary of the Department of Spac ...
led as Chairman ISRO. * Mylswamy Annadurai was the Programme Director and in charge of budget management as well as direction for spacecraft configuration, schedule and resources. *S Ramakrishnan was a Director who helped in developing the liquid propulsion system of the PSLV launcher. * P. Kunhikrishnan was a Project Director in the PSLV programme. He was also a Mission director of PSLV-C25/Mars Orbiter Mission. * Moumita Dutta was the Project manager of the Mars Orbiter Mission. * Nandini Harinath was the Deputy Operations Director of Navigation. * Ritu Karidhal was the Deputy Operations Director of Navigation. *BS Kiran was the Associate Project Director of Flight Dynamics. *V Kesava Raju was the Mars Orbiter Mission Director. *V Koteswara Rao was ISRO scientific secretary. *Chandradathan was the Director of the Liquid Propulsion System. *
A. S. Kiran Kumar Aluru Seelin Kiran Kumar (born 22 Oct 1952) is an Indian space scientist and former chairman of the Indian Space Research Organisation, having assumed office on 14 January 2015. He is credited with the development of key scientific instruments ...
was the Director of the Satellite Application Centre. * M. Y. S. Prasad is the Director at Satish Dhawan Space Centre. He was also the chairman at Launch Authorisation Board. * S. K. Shivakumar was a Director at the ISRO Satellite Centre. He was also a Project Director for the Deep Space Network. * Subbiah Arunan was a Project Director at Mars Orbiter Mission. *B Jayakumar was an Associate Project Director at the PSLV programme who was responsible for testing the rocket systems. *MS Pannirselvam was the Chief General Manager at the Sriharikota Rocket port and was tasked to maintain launch schedules.


Cost

The total cost of the mission was approximately 450 Crore (), making it the least-expensive Mars mission to date. The low cost of the mission was ascribed by
K. Radhakrishnan Koppillil Radhakrishnan (born 29 August 1949) is an Indian space scientist who headed the Indian Space Research Organisation (ISRO) between November 2009 and December 2014 as Chairman of Space Commission, Secretary of the Department of Spac ...
, the chairman of ISRO, to various factors, including a "modular approach", few ground tests and long working days for scientists, ( 18 – 20 hours ).
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's Jonathan Amos specified lower worker costs, home-grown technologies, simpler design, and a significantly less complicated payload than NASA's
MAVEN MAVEN is an American spacecraft orbiting Mars to study the loss of its atmospheric gases to space, providing insight into the history of the planet's climate and water. The spacecraft name is an acronym for "Mars Atmosphere and Volatile Evolu ...
.


Mission objectives

The primary objective of the mission is to develop the technologies required for designing, planning, management and operations of an
interplanetary mission Interplanetary spaceflight or interplanetary travel is the crewed or uncrewed travel between stars and planets, usually within a single planetary system. In practice, spaceflights of this type are confined to travel between the planets of the S ...
. The secondary objective is to explore Mars' surface features,
morphology Morphology, from the Greek and meaning "study of shape", may refer to: Disciplines * Morphology (archaeology), study of the shapes or forms of artifacts * Morphology (astronomy), study of the shape of astronomical objects such as nebulae, galaxies ...
, mineralogy and
Martian atmosphere The atmosphere of Mars is the layer of gases surrounding Mars. It is primarily composed of carbon dioxide (95%), molecular nitrogen (2.8%), and argon (2%). It also contains trace levels of water vapor, oxygen, carbon monoxide, hydrogen, and no ...
using indigenous scientific instruments. The main objectives are to develop the technologies required for designing, planning, management and operations of an interplanetary mission comprising the following major tasks: * Orbit manoeuvres to transfer the spacecraft from Earth-centred orbit to heliocentric trajectory and finally, capture into Martian orbit * Development of force models and algorithms for orbit and attitude (orientation) computations and analysis * Navigation in all phases * Maintain the spacecraft in all phases of the mission * Meeting power, communications, thermal and payload operation requirements * Incorporate autonomous features to handle contingency situations


Scientific objectives

The scientific objectives deal with the following major aspects: *
Exploration of Mars The planet Mars has been explored remotely by spacecraft. Probes sent from Earth, beginning in the late 20th century, have yielded a large increase in knowledge about the Martian system, focused primarily on understanding its geology and habi ...
surface features by studying the morphology, topography and mineralogy * Study the constituents of Martian atmosphere including
methane Methane ( , ) is a chemical compound with the chemical formula (one carbon atom bonded to four hydrogen atoms). It is a group-14 hydride, the simplest alkane, and the main constituent of natural gas. The relative abundance of methane on Ea ...
and using remote sensing techniques * Study the dynamics of the upper atmosphere of Mars, effects of
solar wind The solar wind is a stream of charged particles released from the upper atmosphere of the Sun, called the corona. This plasma mostly consists of electrons, protons and alpha particles with kinetic energy between . The composition of the sol ...
and radiation and the escape of volatiles to outer space The mission would also provide multiple opportunities to observe the Martian moon Phobos and also offer an opportunity to identify and re-estimate the orbits of asteroids seen during the Martian Transfer Trajectory.


Studies

In May–June 2015 Indian scientists got an opportunity to study the Solar Corona during the Mars conjunction when earth and Mars are on the opposite sides of the sun. During this period the S band waves emitted by Mangalyaan were transmitted through the Solar Corona that extends millions of kms into space. This event helped scientists study the Solar surface and regions where temperature changed abruptly.


Spacecraft design

*Mass: The lift-off mass was , including of propellant. *Bus: The spacecraft's
bus A bus (contracted from omnibus, with variants multibus, motorbus, autobus, etc.) is a road vehicle that carries significantly more passengers than an average car or van. It is most commonly used in public transport, but is also in use for cha ...
is a modified I-1 K structure and propulsion hardware configuration, similar to
Chandrayaan-1 Chandrayaan-1 (, ) was the first Indian lunar probe under the Chandrayaan program. It was launched by the Indian Space Research Organisation in October 2008, and operated until August 2009. The mission included a lunar orbiter and an impact ...
, India's lunar orbiter that operated from 2008 to 2009, with specific improvements and upgrades needed for a Mars mission. The satellite structure is constructed of an aluminium and composite fibre reinforced plastic (
CFRP CFRP may refer to: * Carbon fiber reinforced polymer Carbon fiber-reinforced polymers (American English), carbon-fibre-reinforced polymers (Commonwealth English), carbon-fiber-reinforced plastics, carbon-fiber reinforced-thermoplastic (CFRP, ...
) sandwich construction. *Power: Electric power is generated by three
solar array A photovoltaic system, also PV system or solar power system, is an electric power system designed to supply usable solar power by means of photovoltaics. It consists of an arrangement of several components, including solar panels to absorb and ...
panels of each ( total), for a maximum of 840 watts of power generation in Mars orbit. Electricity is stored in a 36 Ah
Lithium-ion battery A lithium-ion or Li-ion battery is a type of rechargeable battery which uses the reversible reduction of lithium ions to store energy. It is the predominant battery type used in portable consumer electronics and electric vehicles. It also s ...
. *Propulsion: A liquid fuel engine with a thrust of is used for orbit raising and insertion into Mars orbit. The orbiter also has eight thrusters for
attitude control Attitude control is the process of controlling the orientation of an aerospace vehicle with respect to an inertial frame of reference or another entity such as the celestial sphere, certain fields, and nearby objects, etc. Controlling vehicle ...
(orientation). Its propellant mass at launch was . *Attitude and Orbit Control System: Maneuvering system that includes electronics with a MAR31750 processor, two star sensors, a solar panel Sun sensor, a coarse analog Sun sensor, four reaction wheels, and the primary propulsion system. *Antennae: Low gain antenna, mid gain antenna, and high gain antenna


Scientific instruments

The scientific payload consists of five instruments: *Atmospheric studies: ** Lyman-Alpha Photometer (LAP) – a
photometer A photometer is an instrument that measures the strength of electromagnetic radiation in the range from ultraviolet to infrared and including the visible spectrum. Most photometers convert light into an electric current using a photoresistor, ...
that measures the relative abundance of
deuterium Deuterium (or hydrogen-2, symbol or deuterium, also known as heavy hydrogen) is one of two stable isotopes of hydrogen (the other being protium, or hydrogen-1). The nucleus of a deuterium atom, called a deuteron, contains one proton and one ...
and
hydrogen Hydrogen is the chemical element with the symbol H and atomic number 1. Hydrogen is the lightest element. At standard conditions hydrogen is a gas of diatomic molecules having the formula . It is colorless, odorless, tasteless, non-toxic ...
from Lyman-alpha emissions in the upper atmosphere. Measuring the deuterium/hydrogen ratio will allow an estimation of the amount of water loss to
outer space Outer space, commonly shortened to space, is the expanse that exists beyond Earth and its atmosphere and between celestial bodies. Outer space is not completely empty—it is a near-perfect vacuum containing a low density of particles, pred ...
. The nominal plan to operate LAP is between the ranges of approximately before and after Mars periapsis. Minimum observation duration for achieving LAP's science goals is 60 minutes per orbit during normal range of operation. The objectives of this instrument are as follows: ***Estimation of D/H ratio ***Estimation of escape flux of H2 corona ***Generation of
hydrogen Hydrogen is the chemical element with the symbol H and atomic number 1. Hydrogen is the lightest element. At standard conditions hydrogen is a gas of diatomic molecules having the formula . It is colorless, odorless, tasteless, non-toxic ...
and
deuterium Deuterium (or hydrogen-2, symbol or deuterium, also known as heavy hydrogen) is one of two stable isotopes of hydrogen (the other being protium, or hydrogen-1). The nucleus of a deuterium atom, called a deuteron, contains one proton and one ...
coronal profiles. ** Methane Sensor for Mars (MSM) – was meant to measure methane in the atmosphere of Mars, if any, and map its sources with an accuracy of few 10s parts-per-billion (ppb). After entering Mars orbit it was determined that the instrument, although in good working condition, had a design flaw and it was incapable of distinguishing methane on Mars. The instrument can accurately map Mars albedo at 1.65um. *** MSM Design Flaw. The MSM sensor was expected to measure methane in the Mars atmosphere; methane on Earth is often associated with life. However, after it entered orbit, it was reported that there was an issue with how it collected and processed data. The spectrometer could measure intensity of different spectral bands, uch as methanebut instead of sending back the spectra, it sent back the sum of the sampled spectra and also the gaps between the sampled lines. The difference was supposed to be the methane signal, but since other spectra such as carbon dioxide could have varying intensities, it was not possible to determine the actual methane intensity. The device was repurposed as an albedo mapper. *Particle environment studies: ** Mars Exospheric Neutral Composition Analyser (MENCA) – is a
quadrupole mass analyser The quadrupole mass analyzer, originally conceived by Nobel Laureate Wolfgang Paul and his student Helmut Steinwedel, also known as quadrupole mass filter, is one type of mass analyzer used in mass spectrometry. As the name implies, it consists ...
capable of analysing the neutral composition of particles in the range of 1–300 amu (atomic mass unit) with unit mass resolution. The heritage of this payload is from Chandra's Altitudinal Composition Explorer (CHACE) payload aboard the Moon Impact Probe (MIP) in
Chandrayaan-1 Chandrayaan-1 (, ) was the first Indian lunar probe under the Chandrayaan program. It was launched by the Indian Space Research Organisation in October 2008, and operated until August 2009. The mission included a lunar orbiter and an impact ...
mission. MENCA is planned to perform five observations per orbit with one hour per observation. *Surface imaging studies: ** Thermal Infrared Imaging Spectrometer (TIS) – TIS measures the thermal emission and can be operated during both day and night. It would map surface composition and mineralogy of Mars and also monitor atmospheric and turbidity (required for the correction of MSM data). Temperature and emissivity are the two basic physical parameters estimated from thermal emission measurement. Many minerals and soil types have characteristic spectra in TIR region. TIS can map surface composition and mineralogy of Mars. ** Mars Colour Camera (MCC) – This tricolour camera gives images and information about the surface features and composition of Martian surface. It is useful to monitor the dynamic events and weather of Mars like dust storms/atmospheric turbidity. MCC will also be used for probing the two satellites of Mars, Phobos and Deimos. MCC would provide context information for other science payloads. MCC images are to be acquired whenever MSM and TIS data is acquired. Seven Apoareion Imaging of the entire disc and multiple Periareion images of are planned in every orbit.


Telemetry and command

The ISRO Telemetry, Tracking and Command Network performed navigation and tracking operations for the launch with ground stations at Sriharikota,
Port Blair Port Blair () is the capital city of the Andaman and Nicobar Islands, a union territory of India in the Bay of Bengal. It is also the local administrative sub-division (''tehsil'') of the islands, the headquarters for the district of South An ...
,
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and
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in
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, and after the spacecraft's
apogee An apsis (; ) is the farthest or nearest point in the orbit of a planetary body about its primary body. For example, the apsides of the Earth are called the aphelion and perihelion. General description There are two apsides in any ell ...
became more than 100,000 km, an and a diameter antenna of the Indian Deep Space Network were utilised. The dish antenna was used for communication with the craft until April 2014, after which the larger antenna was used. NASA's Deep Space Network is providing position data through its three stations located in Canberra,
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and Goldstone on the US West Coast during the non-visible period of ISRO's network. The
South African National Space Agency The South African National Space Agency (SANSA) is South Africa's government agency responsible for the promotion and development of aeronautics and aerospace space research. It fosters cooperation in space-related activities and research in sp ...
's (SANSA) Hartebeesthoek (HBK) ground station is also providing satellite tracking, telemetry and command services.


Communications

Communications are handled by two 230-watt
TWTA A traveling-wave tube (TWT, pronounced "twit") or traveling-wave tube amplifier (TWTA, pronounced "tweeta") is a specialized vacuum tube that is used in electronics to amplify radio frequency (RF) signals in the microwave range. The TWT belongs t ...
s and two coherent transponders. The antenna array consists of a low-gain antenna, a medium-gain antenna and a
high-gain antenna A directional antenna or beam antenna is an antenna which radiates or receives greater power in specific directions allowing increased performance and reduced interference from unwanted sources. Directional antennas provide increased performanc ...
. The high-gain antenna system is based on a single 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.


Mission profile


Launch

ISRO originally intended to launch MOM with its Geosynchronous Satellite Launch Vehicle (GSLV), but the GSLV failed twice in 2010 and still had issues with its
cryogenic engine A cryogenic rocket engine is a rocket engine that uses a cryogenic fuel and oxidizer; that is, both its fuel and oxidizer are gases which have been liquefied and are stored at very low temperatures. These highly efficient engines were first flo ...
. Waiting for the new batch of rockets would have delayed the MOM for at least three years, so ISRO opted to switch to the less-powerful
Polar Satellite Launch Vehicle The Polar Satellite Launch Vehicle (PSLV) is an expendable medium-lift launch vehicle designed and operated by the Indian Space Research Organisation (ISRO). It was developed to allow India to launch its Indian Remote Sensing (IRS) satellites ...
(PSLV). Since it was not powerful enough to place MOM on a direct-to-Mars trajectory, the spacecraft was launched into a highly elliptical Earth orbit and used its own thrusters over multiple perigee burns (to take advantage of the
Oberth effect In astronautics, a powered flyby, or Oberth maneuver, is a maneuver in which a spacecraft falls into a gravitational well and then uses its engines to further accelerate as it is falling, thereby achieving additional speed. The resulting maneuver ...
) to place itself on a trans-Mars trajectory. On 19 October 2013, ISRO chairman
K. Radhakrishnan Koppillil Radhakrishnan (born 29 August 1949) is an Indian space scientist who headed the Indian Space Research Organisation (ISRO) between November 2009 and December 2014 as Chairman of Space Commission, Secretary of the Department of Spac ...
announced that the launch had to be postponed by a week for 5 November 2013 due to a delay of a crucial telemetry ship reaching Fiji. The launch was rescheduled ISRO's PSLV-XL placed the satellite into Earth orbit at 09:50 UTC on 5 November 2013, with a perigee of , an apogee of , and inclination of 19.20 degrees, with both the antenna and all three sections of the solar panel arrays deployed. During the first three orbit raising operations, ISRO progressively tested the spacecraft systems. The orbiter's dry mass is and it carried of fuel at launch. Its main engine, a derivative of the system used on India's communications satellites, uses the bipropellant combination
monomethylhydrazine Monomethylhydrazine (mono-methyl hydrazine, MMH) is a highly toxic, volatile hydrazine derivative with the chemical formula . It is used as a rocket propellant in bipropellant rocket engines because it is hypergolic with various oxidizers such as ...
and dinitrogen tetroxide to achieve the thrust necessary for
escape velocity In celestial mechanics, escape velocity or escape speed is the minimum speed needed for a free, non- propelled object to escape from the gravitational influence of a primary body, thus reaching an infinite distance from it. It is typically ...
from Earth. It was also used to slow down the probe for Mars orbit insertion and, subsequently, for orbit corrections. Models used for MOM:


Orbit raising manoeuvres

Several orbit raising operations were conducted from the Spacecraft Control Centre (SCC) at the ISRO Telemetry, Tracking and Command Network (ISTRAC) at Peenya, Bengaluru on 6, 7, 8, 10, 12 and 16 November by using the spacecraft's on-board propulsion system and a series of perigee burns. The first three of the five planned orbit raising manoeuvres were completed with nominal results, while the fourth was only partially successful. However, a subsequent supplementary manoeuvre raised the orbit to the intended altitude aimed for in the original fourth manoeuvre. A total of six burns were completed while the spacecraft remained in Earth orbit, with a seventh burn conducted on 30 November to insert MOM into a heliocentric
orbit In celestial mechanics, an orbit is the curved trajectory of an object such as the trajectory of a planet around a star, or of a natural satellite around a planet, or of an artificial satellite around an object or position in space such as ...
for its transit to Mars. The first orbit-raising manoeuvre was performed on 6 November 2013 at 19:47 UTC when the spacecraft's liquid engine was fired for 416 seconds. With this engine firing, the spacecraft's
apogee An apsis (; ) is the farthest or nearest point in the orbit of a planetary body about its primary body. For example, the apsides of the Earth are called the aphelion and perihelion. General description There are two apsides in any ell ...
was raised to , with a
perigee An apsis (; ) is the farthest or nearest point in the orbit of a planetary body about its primary body. For example, the apsides of the Earth are called the aphelion and perihelion. General description There are two apsides in any ell ...
of . The second orbit raising manoeuvre was performed on 7 November 2013 at 20:48 UTC, with a burn time of 570.6 seconds resulting in an apogee of . The third orbit raising manoeuvre was performed on 8 November 2013 at 20:40 UTC, with a burn time of 707 seconds, resulting in an apogee of . The fourth orbit raising manoeuvre, starting at 20:36 UTC on 10 November 2013, imparted a
delta-v Delta-''v'' (more known as " change in velocity"), symbolized as ∆''v'' and pronounced ''delta-vee'', as used in spacecraft flight dynamics, is a measure of the impulse per unit of spacecraft mass that is needed to perform a maneuver such a ...
of to the spacecraft instead of the planned as a result of underburn by the motor. Because of this, the apogee was boosted to instead of the planned . When testing the redundancies built-in for the propulsion system, the flow to the liquid engine stopped, with consequent reduction in incremental velocity. During the fourth orbit burn, the primary and redundant coils of the solenoid flow control valve of 440 newton liquid engine and logic for thrust augmentation by the attitude control thrusters were being tested. When both primary and redundant coils were energised together during the planned modes, the flow to the liquid engine stopped. Operating both the coils simultaneously is not possible for future operations, however they could be operated independently of each other, in sequence. As a result of the fourth planned burn coming up short, an additional unscheduled burn was performed on 12 November 2013 that increased the apogee to , a slightly higher altitude than originally intended in the fourth manoeuvre. The apogee was raised to on 15 November 2013, 19:57 UTC in the final orbit raising manoeuvre.


Trans-Mars injection

On 30 November 2013 at 19:19 UTC, a 23-minute engine firing initiated the
transfer Transfer may refer to: Arts and media * ''Transfer'' (2010 film), a German science-fiction movie directed by Damir Lukacevic and starring Zana Marjanović * ''Transfer'' (1966 film), a short film * ''Transfer'' (journal), in management studies ...
of MOM away from Earth orbit and on heliocentric orbit toward Mars. The probe travelled a distance of to reach Mars.


Trajectory correction maneuvers

Four trajectory corrections were originally planned, but only three were carried out. The first trajectory correction manoeuvre (TCM) was carried out on 11 December 2013 at 01:00 UTC by firing the thrusters for a duration of 40.5 seconds. After this event, MOM was following the designed trajectory so closely that the trajectory correction manoeuvre planned in April 2014 was not required. The second trajectory correction manoeuvre was performed on 11 June 2014 at 11:00 UTC by firing the spacecraft's 22 newton thrusters for 16 seconds. The third planned trajectory correction manoeuvre was postponed, due to the orbiter's trajectory closely matching the planned trajectory. The third trajectory correction was also a deceleration test 3.9 seconds long on 22 September 2014.


Mars orbit insertion

The plan was for an insertion into Mars orbit on 24 September 2014, approximately 2 days after the arrival of NASA's
MAVEN MAVEN is an American spacecraft orbiting Mars to study the loss of its atmospheric gases to space, providing insight into the history of the planet's climate and water. The spacecraft name is an acronym for "Mars Atmosphere and Volatile Evolu ...
orbiter. The 440-newton liquid apogee motor was test fired on 22 September at 09:00 UTC for 3.968 seconds, about 41 hours before actual orbit insertion. After these events, the spacecraft performed a reverse manoeuvre to reorient from its deceleration burn and entered Martian orbit.


Status

The orbit insertion put MOM in a highly elliptical orbit around Mars, as planned, with a period of 72 hours 51 minutes 51 seconds, a
periapsis An apsis (; ) is the farthest or nearest point in the orbit of a planetary body about its primary body. For example, the apsides of the Earth are called the aphelion and perihelion. General description There are two apsides in any elli ...
of and
apoapsis An apsis (; ) is the farthest or nearest point in the orbit of a planetary body about its primary body. For example, the apsides of the Earth are called the aphelion and perihelion. General description There are two apsides in any elli ...
of . At the end of the orbit insertion, MOM was left with of fuel on board, more than the necessary for a six-month mission. On 28 September 2014, MOM controllers published the spacecraft's first global view of Mars. The image was captured by the Mars Colour Camera (MCC). On 7 October 2014, the ISRO altered MOM's orbit so as to move it behind Mars for Comet Siding Spring's flyby of the planet on 19 October 2014. The spacecraft consumed of fuel for the manoeuvre. As a result, MOM's apoapsis was reduced to . After the comet passed by Mars, ISRO reported that MOM remained healthy. On 4 March 2015, the ISRO reported that the MSM instrument was functioning normally and are studying Mars'
albedo Albedo (; ) is the measure of the diffuse reflection of solar radiation out of the total solar radiation and measured on a scale from 0, corresponding to a black body that absorbs all incident radiation, to 1, corresponding to a body that refl ...
, the reflectivity of the planet's surface. The Mars Colour Camera was also returning new images of the Martian surface. On 24 March 2015, MOM completed its initial six-month mission in orbit around Mars. ISRO extended the mission by an additional six months; the spacecraft has of propellant remaining and all five of its scientific instruments are working properly. The orbiter can reportedly continue orbiting Mars for several years with its remaining propellant. A 17-day communications blackout occurred from 6 to 22 June 2015 while Mars' orbit took it behind the Sun from Earth's view. On 24 September 2015, ISRO released its "Mars Atlas", a 120-page scientific
atlas An atlas is a collection of maps; it is typically a bundle of maps of Earth or of a region of Earth. Atlases have traditionally been bound into book form, but today many atlases are in multimedia formats. In addition to presenting geograp ...
containing images and data from the Mars Orbiter Mission's first year in orbit. In March 2016, the first science results of the mission were published in ''
Geophysical Research Letters ''Geophysical Research Letters'' is a biweekly peer-reviewed scientific journal of geoscience published by the American Geophysical Union that was established in 1974. The editor-in-chief is Harihar Rajaram. Aims and scope The journal aims for rap ...
'', presenting measurements obtained by the spacecraft's MENCA instrument of the Martian exosphere. During 18 to 30 May 2016, a communication whiteout occurred with Earth coming directly between Sun and Mars. Due to high solar radiation, sending commands to spacecraft was avoided and payload operations were suspended. On 17 January 2017, MOM's orbit was altered to avoid the impending eclipse season. With a burn of eight 22 N thrusters for 431 seconds, resulting in a velocity difference of using of propellant (leaving 13 kg remaining), eclipses were avoided until September 2017. The battery is able to handle eclipses of up to 100 minutes. On 19 May 2017, MOM reached 1,000 days (973 sols) in orbit around Mars. In that time, the spacecraft completed 388 orbits of the planet and relayed more than 715 images back to Earth. ISRO officials stated that it remains in good health. On 24 September 2018, MOM completed 4 years in its orbit around Mars, although the designed mission life was only six months. Over these years, MOM's Mars Colour Camera has captured over 980 images that were released to the public. The probe is still in good health and continues to work nominally. On 24 September 2019, MOM completed 5 years in orbit around Mars, sending 2 terabytes of imaging data, and had enough propellant to complete another year in orbit. On 1 July 2020, Mangalyaan was able to capture a photo of the Mars satellite Phobos from 4200 km away. On 18 July 2021 Mars Colour Camera (MCC) captured full disc image of Mars from an altitude of about 75,000 km with spatial resolution about 3.7 km. In October 2022, ISRO admitted that it has lost the communication with MOM in April 2022, when it faced increasingly longer duration eclipses, including a seven-hour long eclipse that it was not designed to withstand. ISRO said the spacecraft was likely out of propellant and not recoverable. File:One of the first images of the surface of Mars taken by the Mangalyaan on September 25, 2014.jpg, One of the first images of the surface of Mars taken by MOM on 25 September 2014 File:Arsia Mons - Mars Orbiter Mission (30108068296).png, Mangalyaan's image of
Arsia Mons Arsia Mons is the southernmost of three volcanoes (collectively known as Tharsis Montes) on the Tharsis bulge near the equator of the planet Mars. To its north is Pavonis Mons, and north of that is Ascraeus Mons. The tallest volcano in the So ...
File:Tharsis and Valles Marineris - Mars Orbiter Mission (30055660701).png, Image of
Tharsis Tharsis () is a vast volcanic plateau centered near the equator in the western hemisphere of Mars. The region is home to the largest volcanoes in the Solar System, including the three enormous shield volcanoes Arsia Mons, Pavonis Mons, and Asc ...
and
Valles Marineris Valles Marineris (; Latin for '' Mariner Valleys'', named after the ''Mariner 9'' Mars orbiter of 1971–72 which discovered it) is a system of canyons that runs along the Martian surface east of the Tharsis region. At more than long, wide and ...
by Mangalyaan File:Mars as seen from Mangalyaan (MOM).png, Mars as seen from Mangalyaan File:Syrtis Major - Mars Orbiter Mission (29512601624).png, Three frame Mars Orbiter Mission Mars Color Camera mosaic of the Syrtis Major region on 24 September 2015. File:NorthMars.jpg, North Pole


Recognition

In 2014, China referred to India's successful Mars Orbiter Mission as the "Pride of Asia". The Mars Orbiter Mission team won US-based
National Space Society The National Space Society (NSS) is an American international nonprofit 501(c)(3) educational and scientific organization specializing in space advocacy. It is a member of the Independent Charities of America and an annual participant in the Comb ...
's 2015 Space Pioneer Award in the science and engineering category. NSS said the award was given as the Indian agency successfully executed a Mars mission in its first attempt; and the spacecraft is in an elliptical orbit with a high apoapsis where, with its high resolution camera, it is taking full-disk colour imagery of Mars. Very few full disk images have ever been taken in the past, mostly on approach to the planet, as most imaging is done looking straight down in mapping mode. These images will aid planetary scientists. An illustration of the Mars Orbiter Mission spacecraft is featured on the reverse of the currency note of India. An image taken by the Mars Orbiter Mission spacecraft was the cover photo of the November 2016 issue of '' National Geographic'' magazine, for their story "Mars: Race to the Red Planet".


Follow-up mission

ISRO plans to develop and launch a follow-up mission called
Mars Orbiter Mission 2 Mars Orbiter Mission 2 (MOM 2), also called ''Mangalyaan-2'' ("Mars-craft", from sa, मंगल ''mangal'', "Mars" and यान ''yān'', "craft, vehicle"), is India's second interplanetary mission planned by the Indian Space Research Organi ...
(MOM-2 or ''Mangalyaan-2'') with a greater scientific payload to Mars in 2024 or 2026. The orbiter will use
aerobraking Aerobraking is a spaceflight maneuver that reduces the high point of an elliptical orbit ( apoapsis) by flying the vehicle through the atmosphere at the low point of the orbit ( periapsis). The resulting drag slows the spacecraft. Aerobraking ...
to reduce
apoapsis An apsis (; ) is the farthest or nearest point in the orbit of a planetary body about its primary body. For example, the apsides of the Earth are called the aphelion and perihelion. General description There are two apsides in any elli ...
of its initial orbit and reach an altitude more suitable for scientific observation.


In popular culture

* The 2019 Hindi film ''
Mission Mangal ''Mission Mangal'' (English: "Mission Mars") is a 2019 Indian Hindi-language drama film directed by Jagan Shakti and produced by Cape of Good Films, Hope Productions, Fox Star Studios, Aruna Bhatia and Anil Naidu. Loosely based on the life of s ...
'' is loosely based on India's mission to Mars. *A web series called ''
Mission Over Mars ''M.O.M. - Mission Over Mars'' is a 2019 Indian Hindi drama web series created by Ekta Kapoor. The series is developed and produced by Endemol Shine India for online streaming platforms ALTBalaji and ZEE5. The series stars Sakshi Tanwar, Mona ...
'' is loosely based on India's Mars mission. * ''Space MOMs'' released online in 2019 is based India's Mars Mission. * ''Mission Mars'' released in 2018 is a short Film based on India's Mars Mission.


See also

* * * List of ISRO missions *
List of Mars orbiters The following table is a list of Mars orbiters, consisting of space probes which were launched from Earth and are currently orbiting Mars. As of February 2021, there have been 18 spacecraft missions operating in Mars' orbit, 8 of which are curre ...
*
List of missions to Mars This is a list of the 50 spacecraft missions (including unsuccessful ones) relating to the planet Mars, such as orbiters and rovers. Missions ;Mission Type Legend: Mars landing locations There are a number of derelict orbiters around ...
*


References


External links


Mars Orbiter Mission website

Mars Orbiter Mission brochure

Current Science Vol.109, Issue 6: Special Section on Mars Orbiter Mission with featured papers
(25 September 2015) {{Portal bar, Astronomy, Stars, Spaceflight, Outer space, Solar System, India ISRO space probes Missions to Mars Space probes launched in 2013 2013 in India Satellites orbiting Mars Geography of Mars Spacecraft launched by PSLV rockets