Astronomy:Chandrayaan programme

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Short description: Indian Lunar exploration programme

Chandrayaan programme
LVM3 M4, Chandrayaan-3 - Launch vehicle lifting off from the Second Launch Pad (SLP) of SDSC-SHAR, Sriharikota 03.webp
LVM3 M4 lifting off with Chandrayaan-3 on 14 July 2023
CountryIndia
OrganizationISRO
PurposeExploration of the Moon
StatusActive
Programme history
Cost₹1,364 crore (US$190 million)[1][2]
Duration2003–present[3]
First flightChandrayaan-1, 22 October 2008; 15 years ago (2008-10-22)
Last flightChandrayaan-3, 14 July 2023; 12 months ago (2023-07-14)
Successes2
Partial failures1 (Chandrayaan-2)
Launch site(s)Satish Dhawan Space Centre
Vehicle information
Launch vehicle(s)

The Chandrayaan programme (/ˌtʃʌndrəˈjɑːn/ CHUN-drə-YAHN) (from Sanskrit: Chandra, "Moon" and yāna, "craft, vehicle", About this soundpronunciation)[4][5] also known as the Indian Lunar Exploration Programme is an ongoing series of outer space missions by the Indian Space Research Organization (ISRO) for the exploration of the Moon. The program incorporates a lunar orbiter, an impactor, a soft lander and a rover spacecraft.

There have been three missions so far with a total of two orbiters, landers and rovers each. While the two orbiters were successful, the first lander and rover which were part of the Chandrayaan-2 mission, crashed on the surface. The second lander and rover mission Chandrayaan-3 successfully landed on the Moon on 23 August 2023, making India the first nation to successfully land a spacecraft in the lunar south pole region, and the fourth country to soft land on the Moon after the Soviet Union, the United States and China.

Background

The Indian space programme had begun with no intentions of undertaking sophisticated initiatives like human spaceflight and extraterrestrial missions during the initial days. It was only after ISRO developed the capabilities of creating satellites and orbital launch vehicles like PSLV, that the possibilities of India's first extraterrestrial exploration mission to the Moon were being explored in the early 2000s. The idea of a lunar scientific mission was first raised in 1999 during a meeting of the Indian Academy of Sciences (IAS) which was then carried forward by the Astronautical Society of India (ASI) in 2000.[6]

History

First mission

Soon after the proposals by the Indian Academy of Sciences in 1999 and by the Astronautical Society of India in 2000, a National Lunar Mission Task Force (NLMTF) was set up which constituted ISRO and leading Indian scientists and technologists across the nation to conduct the feasibility study. The study report was then reviewed by a peer group of 100 scientists from various fields.[6] The recommendations put forward were as follows:

  • The Indian Moon Mission assumes significance in the context of the international scientific community considering several exciting missions in planetary exploration, in the new millennium.
  • ISRO has the necessary expertise to develop and launch the Moon Mission with imaginative features and it would be different from the past missions. Hence ISRO should go ahead with the project approval and implementation.
  • Apart from technological and scientific gains, it would provide the needed thrust to basic science and engineering research in the country. The project would help return young talents to the arena of fundamental research.
  • The Academia, in particular, the university scientists would find participation in such a project intellectually rewarding. In this context, the scientific objectives would need further refinement to include other innovative ideas from a broader scientific community through Announcement of Opportunity, etc.
It is not whether we can afford it. It is whether we can afford to ignore it.

On 15 August 2003, then prime minister Atal Bihari Vajpayee announced the project which was estimated to cost ₹350 crore (US$49 million).[7][8] In November of the same year, the government approved the Chandrayaan project which would consist of an orbiter that would conduct mineralogical and chemical mapping of the surface.[9] During the assembly of the orbiter only mission, then president A.P.J. Abdul Kalam visited the ISRO office and advised that orbiter alone would not suffice and proposed of another instrument that could be dropped on the surface. Following the advice, the scientists made design changes to the project and included an impact probe named Moon Impact Probe (MIP).[10] The MIP was planned to be dropped from 100 km (62 mi) altitude and would acquire close-range images of the surface, collect telemetry data for future soft landing missions and measure the constituents of the lunar atmosphere.[11]

Moon Impact Probe being integrated with Chandrayaan-1.

The project required India set up its deep space network and the entire project cost ₹360 crore (US$50 million).[12] On 22 October 2008, Chandrayaan-1 was successfully launched aboard the PSLV rocket.[13] After earth bound maneuvers and trans lunar injection, Chandrayaan-1 entered the lunar orbit on 10 November, making India the fifth nation to orbit Moon.[14] Four days later, on 14 November, the Moon Impact Probe (MIP) impacted near the Shackleton crater, in the lunar south pole, this made India the fifth country to reach the lunar surface and the first to reach lunar south pole.[15] The MIP made the most significant discovery by confirming the existence of water on Moon. This discovery was not made public until NASA's Moon Mineralogy Mapper payload onboard Chandrayaan-1 orbiter confirmed the same on 24 September 2009.[16] The mission was intended to last two years, but the contact with the orbiter was lost on 28 August 2009, which officially ended the mission.[17]

Second mission and its problems

After the success of the Chandrayaan-1 mission, a follow-up mission worth ₹425 crore (US$60 million) was already being planned and was targeted for a launch in 2012.[18][19] Abdul Kalam suggested for collaboration between India and the United States for the Chandrayaan-2 mission, which would soft land near the lunar south pole and perform robotic penetrations into the surface to study more about the lunar water.[20] However, an agreement had already been signed in the year 2007 by ISRO and Roscosmos, the Russian federal space agency, for the second lunar mission under the Chandrayaan-2 project.[21]

Russian collaboration and back out

According to the agreement, ISRO had the responsibility of launching, orbiting, and deployment of the rover while Russia's Roscosmos would provide the lander.[22] The design of the spacecraft by ISRO was completed in 2009,[23] the payloads were also finalized and the launch was targeted for 2013.[24] The project then hit a roadblock when Russia delayed its development of the lander due to failure of its Fobos-Grunt mission which revealed technical issues in the similar parts that would be used in the lunar lander.[25] Russia then proposed a few changes which required ISRO to decrease mass of its rover due to increase in the mass of the lander. A delayed timeline and the Russian request to accept the risk meant that India had to undertake the entire project independently.[26] With Mars transfer window arriving in the 2013, ISRO repurposed the unused Chandrayaan-2 orbiter hardware for the Mars Orbiter Mission.[27]

Indigenous development of the lander

With the Russian agreement falling apart, India was left alone and now had complete responsibility for the project including the development of lander technology. For which, ISRO created a mimic of Chandrayaan-2's lunar landing site in Challakere with craters that measured 10 m (33 ft) in diameter and were 3 m (9.8 ft) deep. This site was used for testing the electronics of the lander and rover. The project was now estimated to cost ₹600 crore (US$84 million) and was expected to launch in the first quarter of 2018 on GSLV MK-II.[28][29]

Artificial craters created by ISRO in Doddallurathi, Challakere, Karnataka to mimic lunar surface.

In 2018, the mission faced its second delay after ISRO made design changes for the spacecraft as well as changes in its maneuver where the lander would orbit the Moon to assess the performance of various systems before performing landing. This was contrary to the previous plan where the lander would directly descend after arriving in the designated orbit. A fifth engine was added to the lander, the diameter of the landing legs was increased, two additional propellant tanks were added and additional support systems for power, structure, and thermal control were also provided. This significantly increased the mass of the composite and required ISRO to upgrade the GSLV Mk-II vehicle, but the scientists felt it would be risky to fly the test flight of the uprated Mk-II with Chandrayaan-2 payload, hence a more capable and already flown LVM3 vehicle was chosen.[30][31]

Vikram lander of Chandrayaan-2 being hoisted

During a landing test in February 2019, the lander suffered minor injuries in two of its legs due to a faulty orientation for the test, and the launch was then targeted for the second quarter of the year.[32] On 22 July 2019, Chandrayaan-2 worth around ₹800 crore (US$110 million) was finally launched on LVM3 putting an end to several roadblocks that hit the mission during the decade.[33] After orbit-raising maneuvers and finally the trans lunar injection, Chandrayaan-2 attained the lunar Orbit on 20 August. On 6 September 2019, during the descent to the surface, the contact with the lander was lost after it crash-landed. According to the chairman K. Sivan, the lander was operating as expected until it was just 2.1 km (1.3 mi) above the surface when it started deviating from the intended trajectory.[34] Four years later, ISRO chairman S. Somanath revealed three major reasons for the failure, the presence of five engines that generated a higher thrust which made the errors accumulate over time, the lander being unable to turn very fast because it was not expected to perform at such a high pace turning and the final reason was the small 500x500 m landing site chosen that left the lander with less room for error.[35]

Before and after images of the impact site of the Chandrayaan-2

Successful soft landing

Two months after the failure of Chandrayaan-2, the third mission was proposed with the lander and rover being the primary components of the mission, unlike previously where the orbiter carried a greater scientific payload. ISRO sought ₹75 crore (US$11 million) from the government as initial funding for the Chandrayaan-3 project that included a propulsion module, a lander, and a rover. It was expected to launch a year later in November 2020.[36][37] On 19 December 2019, P Veeramuthuvel was appointed as the director of the mission.[38] The work on the project was underway come January 2020 and K. Sivan revealed that the launch may happen in early 2021 with the total cost of the project being ₹615 crore (US$86 million).[39] Later in March, the government confirmed that the launch could take place in the first half of 2021.[40] The earlier addition of the fifth engine in the Chandrayaan-2's lander that caused the additional thrust was now removed from the design of Chandrayaan-3.[41] Like Chandrayaan-2, the testing for the lander was to be conducted in Challakere where ISRO's previously built Moon like site with craters had deteriorated. A total of ₹24.2 lakh (US$34,000) was spent on recreating the site with craters of similar dimensions (10 m (33 ft) wide and 3 m (9.8 ft) deep).[42]

The launch which was planned for early 2021, was then delayed to 2022 due to COVID-19 pandemic in India.[43] The propulsion module which was ready before the pandemic had begun its testing, following which the lander and rover tests were to be conducted but the pandemic delayed the project and pushed its tentative launch date to the third quarter of 2022.[44] Few more changes with strengthening the landing legs, improvisation in instruments, a failure-proof configuration and additional testing meant that the new schedule for the launch was moved to second quarter of 2023.[45]

In May 2023, the spacecraft was in its final stage of the assembly of payloads at the U R Rao Satellite Centre with the launch targeted for the first or second week of July.[46] On 14 July 2023, Chandrayaan-3 was successfully launched on LVM3 and was inserted in the lunar sphere of gravitational influence on 5 August 2023.[47] On 23 August 2023, the lander Vikram successfully soft landed in the lunar south pole region, achieving humanity's first soft landing in the region and making India the fourth country to soft land on the Moon after Soviet Union, United States and China.[48] Soon after the touchdown, the rover Pragyan got down of the ramp and drove 8 m (26 ft) making India only the third country to operate a robotic rover on the Moon after Soviet Union and China.[49]

Chandrayaan-3's lander Vikram on the Moon as seen by the Pragyan rover.
Pragyan rover roll out.

Structure

The Chandrayaan programme or Indian lunar exploration programme is divided into phases, with each mission built on the experience of previous ones. The first phase included the sole mission with an orbiter and an impactor and it was a technical demonstration mission to test India's capability of conducting extraterrestrial scientific missions. The second phase included missions for technical demonstration of soft landing and roving on the lunar surface. After a failed soft landing attempt in 2019, then ISRO vice chairman S. Somnath stated that it would not be the end of the programme and there would be forthcoming missions.[50] After a successful soft landing and roving mission, the programme has now moved into the third phase in which on-site samplings are to be conducted. A mission part of this phase is planned in collaboration with the Japanese national space agency, JAXA and it is planned to have a rover with greater scientific payload and electronics for conducting on-site sample analysis near the lunar south pole.[51]

Phase I: Orbiter and Impactor

The plans for India's first probe to the Moon were mooted during the turn of the millennium and the spacecraft was developed in the mid-2000s. The primary objectives of the mission were to demonstrate India's capability of creating a craft and launching it indigenously, to conduct scientific experiments such as mapping the surface at high resolution, mapping its chemical composition, and finally to collect telemetric data from the later addition of an impact probe that would help in programme's future soft landing missions.[52]

Chandrayaan-1

Further information: Astronomy:Chandrayaan-1
Diagram of the Chandrayaan-1 spacecraft

Chandrayaan-1 was launched on 22 October 2008 aboard PSLV-XL. The solar-powered cuboid orbiter along with the Moon Impact Probe (MIP) weighed 1,380 kg (3,042 lb). It was powered by a single-sided solar array during the day and was supported by lithium-ion batteries during night time. The attitude of the spacecraft was controlled by three-axis stabilization method using two star sensors, gyroscopes and four reaction wheels. The scientific data transmission was conducted in X band frequencies while telemetry tracking was done in S band frequencies. To store these data, two solid-state recorders (SSR) were used with SSR-1 carrying 32 GB dedicated capacity for scientific data while SSR-2 carrying 8 GB capacity for the rest of the scientific data and attitude information. Moon Mineralogy Mapper, an American scientific payload onboard carried its own SSR with 10 GB capacity.[53] The MIP weighed 35 kg (77 lb) with 25 minutes of expected operating duration. It carried a Radar altimeter to record the altitude data which would be used in qualifying technologies for future soft landing missions, a Video imaging system to acquire close-range pictures of the lunar surface, and a Mass spectrometer to study the tenuous atmosphere of the Moon.[54]

The orbiter-impactor composite entered the lunar sphere of gravitational influence on 8 November 2008 and after orbital reduction maneuvers, it attained an elliptical polar orbit of 100 km (62 mi), upon which, two of the eleven scientific payloads, the Terrain Mapping Camera (TMC) which had a spatial resolution of 5 m (16 ft)[55] and Radiation Dose Monitor (RADOM) were switched on for operations.[14][56] On 12 November 2008, the MIP separated from the orbiter and impacted near the lunar south pole's Shackleton crater.[15] While descending, the probe's Chandra's Altitudinal Composition Explorer (CHACE) instrument detected the presence of water.[16] Post deployment of MIP, rest of the nine scientific instruments began operations.[57]

On 25 November 2008, just a couple of weeks after entering lunar orbit, the orbiter's temperature rose to 50 °C (122 °F) after receiving equal amounts of heat from the sun as well as the moon (due to its Albedo). Efforts such as rotating the craft by 20 degrees, shutting down the mission computers, and increasing its orbit to 200 km (120 mi) were made to bring its temperature down and to avoid damaging the onboard instruments.[58] A year later, the overheating problem was responsible for ending the mission as it damaged the star sensors which maintained the orientation of craft. The orientation was then barely maintained with the help of gyroscopes as a temporary measure before losing contact on 28 August 2009, which ended the mission a year before its intended duration. However, the mission was analyzed to be 95% successful with its intended operations.[59][60]

Phase II: Soft landers and rovers

The second phase involved the technical demonstration of the lunar soft landing and operation of a rover. The preparations were already underway before the launch of the first mission. An agreement was signed in 2007 with Russia that included India's contribution in providing a launch vehicle, orbiter, and rover while Russia provided the lander.[21] However, it was later canceled in 2013 after the Russian lander was delayed and after its request to accept the risk.[26] Later in 2017, India signed a deal with Japan's JAXA to conduct a feasibility study for a joint lunar roving mission named Lunar Polar Exploration Mission (LUPEX). For which a technical demonstration of soft landing was required to be conducted.[61][62]

Chandrayaan-2

Further information: Astronomy:Chandrayaan-2
Orbiter and lander in a stacked configuration with the rover inside the lander

Chandrayaan-2 was the second mission under the programme and it included an orbiter, lander, and rover. After the failure of the Chandrayaan-1 orbiter, the Chandrayaan-2 orbiter enabled ISRO to conduct science with modern cameras and instruments. The primary objectives of this mission were to soft land on the surface and operate a rover, to study the lunar surface, its exosphere, minerals and water ice.[63][64]

The orbiter, lander, and rover composite weighed 3,850 kg (8,490 lb), with the orbiter alone weighing 2,379 kg (5,245 lb). The orbiter carried eight scientific instruments with two of the instruments; the Terrain Mapping Camera 2 and Chandrayaan-2 Atmospheric Compositional Explorer 2 (ChACE-2) being upgraded versions of Terrain Mapping camera (TMC) onboard Chandrayaan-1 orbiter and Chandra's Atmospheric Compositional Explorer (CHACE) onboard Moon Impact Probe respectively.[65] The lander named Vikram weighed 1,471 kg (3,243 lb) including the 27 kg (60 lb) rover named Pragyan that it housed inside.[66] Vikram had eight 58 N (13 lbf) thrusters for attitude control and five 800 N (180 lbf) liquid main engines that were derived from ISRO's 400 N (90 lbf) liquid apogee motors[67] and it was designed to safely land on slopes up to 12°.[68] It carried four payloads to study lunar seismic activity, measure the lunar sub-surface temperatures and to measure density and variation of lunar surface plasma (using a langmuir probe). Rover Pragyan carried two scientific payloads that were to be used in determining the elemental composition and its abundance near the landing site.[65] It was designed to travel at a speed of 1 cm/s (0.39 in/s) and could drive up to 500 m (1,600 ft) in its lifetime. Both the lander and rover were expected to operate for one lunar day as they lacked any Radioisotope heater unit (RHU) and were entirely dependent on solar power for operations.[69]

The Chandrayaan-2 was launched on 14 July 2019[33] and it attained the lunar orbit on 20 August 2019.[70] After five orbital reduction manoeuvres, the composite attained a near circular orbit of 127 km × 119 km (79 mi × 74 mi),[71] which was followed by the separation of Vikram on 2 September 2019.[72] After two de-orbiting manoeuvers, Vikram attained a final orbit of 95 km × 119 km (59 mi × 74 mi) after which the powered descent phase began on 7 September 2019. During the descent and landing, the onboard computers had complete control over the lander.[73] The initial descent and critical braking procedures underwent as intended but upon reaching 2.1 km (1.3 mi) altitude, the lander began deviating and lost its contact with the mission control after subsequent crash landing.[74] Upon analysis, it was found that the main engines had higher thrust than normal which led to errors being accumulated over time and this meant the lander could not change its attitude at such a fast pace due to safety constraints in the onboard computer that had a limit on the maximum rate with which it can change its attitude. Coarse throttling of main engines, error in computing the remaining time in the mission and a small landing site of 500 x 500 m were the other reasons attributed to the failure.[75][76]

However, the orbiter remained the sole successful part of the mission with its new mission duration being extended from one year to seven and a half years. The Orbiter High-Resolution Camera (OHRC) during the time remained the most advanced camera in the lunar orbit with a spatial resolution of 25 cm (9.8 in), four times higher than Chandrayaan-1 orbiter's 1 m (3 ft 3 in) resolution. The orbiter is also studying the lava tubes and caves which were previously spotted by the Chandrayaan-1 orbiter.[77][78]

Chandrayaan-3

Further information: Astronomy:Chandrayaan-3
Chandrayaan-3 encapsulated within LVM3's payload fairing

Two months after the failure of Chandrayaan-2's lander, fresh proposals were made for the third mission named Chandrayaan-3, which was a re-attempt to demonstrate the landing capabilities needed for the LUPEX mission, a proposed partnership with Japan that was planned for 2025-26 time frame.[79] With the Chandrayaan-2 orbiter already operational, the mission was primarily a soft landing and roving demonstration mission, with the propulsion module carrying a single payload in Spectro-polarimetry of Habitable Planet Earth (SHAPE). The SHAPE instrument would study Earth's atmosphere from distance and it would aid in the study of Exoplanets' atmospheres, which employs a similar technique.[80] The landing region was unchanged from the previous mission,[81] with the area of new site being expanded to 4 km × 2.5 km (2.5 mi × 1.6 mi) from previous 500 m × 500 m (1,600 ft × 1,600 ft). Other major changes in the new 'failure-based' approach included the removal of the fifth engine, an increase in fuel capacity, an increase in vertical velocity component, and other software changes.[82]

Vikram lander had undergone some major changes after its predecessor crash landed. There were now four instead of five main engines that provided 800 N (180 lbf) of thrust and had slew rate changing capabilities, unlike previously when the centrally mounted fifth engine lacked the capability. This enabled the lander to control the attitude and thrust during all phases of descent. The attitude correction rate was also increased from Chandrayaan-2's 10°/s to 25°/s with Chandrayaan-3. An additional laser Doppler velocimeter (LDV) was equipped that allowed attitude measurements in all three directions.[83][84] The impact legs were made larger and stronger relative to Chandrayaan-2. The OHRC onboard Chandrayaan-2 enabled the mission to have an expanded landing site with 10 km2 (3.9 sq mi) landing area. The lander underwent several tests including a helicopter drop test that helped in improving the structural rigidity. In the event of a failure during descent and landing, multiple contingency systems were added to improve the survivability chances of the lander. However, there were no changes made in the Pragyan rover and the scientific objectives remained unchanged since the previous mission.[85][84]

Chandrayaan-3 was launched on 14 July 2023 aboard LVM3[86] and on 16 August 2023, the composite attained a final lunar orbit of 113 km × 157 km (70 mi × 98 mi).[87] A day later, the Propulsion Module separated from the lander.[88] On 23 August 2023, the lander that had previously reduced its orbit to 25 km × 134 km (16 mi × 83 mi) via de-orbit burns,[89] began descending using all of its four engines after it reached near its Periselene at 30 km (19 mi). Roughly after eleven minutes of powered descent, the lander maintained the altitude of 7.5 km (4.7 mi) for 10 seconds before changing its attitude to vertical position for the final vertical descent phase. It then used two of its four engines to slow its descent to 150 m (490 ft) and then hovered twice for about thirty seconds before touching down on the chosen optimal spot.[90]

A few hours after the soft landing, the ramp was deployed for the Pragyan rover to touch down and begin its operations on the surface.[91] A few days later, the instruments were turned on and the rover moved 8 m (26 ft) on the surface, thus achieving the primary goal of the mission.[92] On 3 September 2023, with the lunar night approaching, the rover was shut down and put into 'sleep mode'. On the same day, before putting Vikram to sleep, ISRO conducted a hop on the lunar surface by firing Vikram's engines that moved it 40 cm (16 in) vertically as well as laterally before touching down again. The hop experiment proved to be the most significant test conducted by ISRO as the data would aid in future sample return missions under the programme. ISRO also attained a unique record of conducting its first vertical take-off and landing on an extraterrestrial surface before Earth; that was planned to be conducted under its Reusable technology demonstration programme.[93][94][95]

In another unique experiment, like the hop experiment on the Vikram Lander, the Propulsion Module (PM) of Chandrayaan-3 was moved from an orbit around Moon to an orbit around Earth.[96]

The initial plan was to operate this payload for about three months during the mission life of PM. The precise orbit injection by LVM3 and optimal earth / lunar burn maneuvers, resulted in the availability of over 100 kg of fuel in the PM after over one month of operations in the lunar orbit. It was decided to use the available fuel in the PM to derive additional information for future lunar missions and demonstrate the mission operation strategies for a sample return mission. In order to continue SHAPE payload for Earth observation, it was decided to re-orbit the PM to a suitable Earth orbit.This mission plan was worked out considering the collision avoidance such as preventing the PM from crashing on to the Moon’s surface or entering into the Earth’s GEO belt at 36000 km and orbits below that. Considering the estimated fuel availability and the safety to GEO spacecraft, the optimal Earth return trajectory was designed for October 2023 month.[96]

Phase III: On-site sampling

Further information: Astronomy:Lunar Polar Exploration Mission

With successful demonstration in soft landing and roving, the programme then moved into its next phase where a rover with greater scientific payload is to be sent to conduct on-site sample analysis. The first mission under this phase named Lunar Polar Exploration Mission (LUPEX), is suggested to be launched in the time frame of 2026–28.[97][98] India is collaborating with Japan in this mission but the mission is not yet well defined. It will be a lander-rover mission near lunar pole to perform on-site sampling and analysis of collected lunar material[99][100] and demonstrate lunar night survival technologies.[101][102]

Science

The Chandrayaan programme has been vastly regarded as successful, especially with the discovery of lunar water.[16] It continues to provide scientific data and high-resolution imagery thanks to Orbiter High Resolution Camera (OHRC) which is the most advanced lunar camera so far with 25 cm (9.8 in) spatial resolution and it is currently operational onboard Chandrayaan-2's orbiter.[77] Chandrayaan-1 lost its contact a year before its intended duration, however, the Chandrayaan-2's orbiter is carrying forward the research from the orbit and is expected to operate until 2026.[78] The first soft landing and on-site science mission of Chandrayaan-3 conducted the first experiments in the lunar south pole region thus contributing to the understanding of the region which holds the potential for a future crewed lunar base.[103]

Discovery of water on the Moon

Further information: Astronomy:Lunar water
Direct evidence of lunar water in the Moon atmosphere obtained by Chandra's Altitudinal Composition (ChACE) output profile
Second confirmation of water on Moon by Chandrayaan-1's Moon Mineralogy Mapper that observed reflectance spectra of water ice.

The presence of water on the Moon has always been a matter of intense debate since the last century. The first study for the lunar water was conducted in 1961 and it revealed that the polar regions, which have a high density of cold traps, have more probability of lunar water ice than the equatorial regions.[104] The samples returned from the equatorial region during Apollo programme failed to provide definitive evidence, reinforcing the need for research on the lunar poles. Since there hadn't been any missions to the lunar poles and since the poles had been speculated to harbour the water ice, Moon Impact Probe's impact site was chosen in the lunar south pole to search for firm evidence of the same in the lunar atmosphere.[6]

The Chandra's Altitudinal Composition (ChACE) was one of the three scientific instruments on board the Chandrayaan-1's Moon Impact Probe (MIP). It was a mass spectrometer that was developed to study the composition of the tenuous lunar exosphere through mass spectroscopy. On 12 November 2008, the MIP separated from the Chandrayaan-1 orbiter and began its descent to the surface, during which it detected the clear presence of molecules with atomic mass unit 18 i.e., water. The ionized water molecules (H₂O⁺) and their fragments (such as H⁺ and OH⁺ ions) were detected by ChACE. Three months later, the Moon Mineralogy Mapper (M3) an imaging spectrometer on board the Chandrayaan-1 orbiter also detected the presence of water. While observing the reflectance spectra of the Moon, it observed the absorption features of the water ice which are in the 1.0-2.5 µm wavelength region. The shadowed regions that received the reflected light were chosen for the study with water ice being found near the polar region.[105]

The ChACE profile indicates a steady rise in the concentration of water molecules starting from 20 degrees south to the poles, however, it peaks at 60-70 degrees south and then declines. Overlaying the M3 profile which begins at 43.1 degrees south depicts a complementary nature of the recordings, confirming the double evidence of lunar water near the south pole. However, the detection of water in every spectrum of ChACE coupled with the fact that it does not indicate either a steady rise or decline or a constant level in its profile, could possibly be due to contamination of water from Earth. Adding to the concerns was the M3's profile which showed a steady increase towards the south pole, unlike ChACE which saw a decline beyond 70 degrees south.[106] But according to Indian mathematician Ramaiyengar Sridharan, if the water ice acts as a source due to sublimation, which would be a strong function of temperature in the prevailing ultra high vacuum condition, then, in the absence of fresh sources during the measurement phase, the increase/decrease in the concentration measured by ChACE should be at the cost of what M3 has detected in the form of ice; which means, the peak measurement recorded may be due to the presence of many water ice sources and the decline may be due to fewer such sources and while M3 mapped the water ice sources on the surface the MIP detected the vapour generated from these sources, thus complementing each other.[107]

Despite the Chandrayaan-1 mission ending a year earlier than the intended duration of two years, the data recorded from the instruments onboard over 310 days were very useful even a decade later. In 2018, the data obtained from the M3 was used by the scientist at University of Hwaii, Dr. Shuai Li and his team to research lunar water in the dark craters of the poles. Since the data was patchy and hard for them to work with the dark craters, they used the traces of sunlight that had bounced off crater walls and analyzed the spectral data to find places where the three specific wavelengths (in the range of 1.0-2.5 µm) of near-infrared light were absorbed that indicated the presence of water ice. They conducted thorough statistical analysis to ensure that their findings were not influenced by random anomalies or errors in the instruments. "I consider this to be the most convincing evidence that you actually do have true water ice at the uppermost surface — what we call the optical surface — of the Moon", Li said on the results.[108][109]

Surface features

Further information: Selenography

Mapping and Studying the lunar surface features were the primary scientific objectives of Chandrayaan-1. The first images of the surface were acquired by the Terrain Mapping Camera (TMC) onboard the mission's orbiter. The CMOS camera with 5 m (16 ft) resolution and 40 km (25 mi) swath in the Panchromatic band, was activated on 29 October 2008 (within the earth's orbit) and it had captured over 70,000 images during its 3,000 orbits around the Moon.[110] While the other scientific missions at the time usually had a 100 m (330 ft) resolution, many of TMC's images had a sharp resolution of 5 m (16 ft) thus enabling the production of a detailed map of the Moon.[111]

During mapping Rilles and Lava tubes on the lunar surface, the TMC discovered a large lava tube near the equator (specifically in the Oceanus Procellarum, to the north of the rille named Rima Galilaei above the lunar equator). The tube measured about 2 km (1.2 mi) in length and 360 m (1,180 ft) in width. The lunar lava tubes are considered as potential habitation sites for future crewed outposts since they protect cosmic radiation, solar radiation, meteorites, micrometeorites, and ejecta from impacts. They are also insulated from the extreme temperature variations on the lunar surface.[112]

Summary

List of missions

Landing

  Intended hard landing
  Successful soft landing
  Unsuccessful soft landing

Map of Chandrayaan programme's landing locations (labels are clickable when viewing the original svg image).
Mission
 Launch Date
 Launch Vehicle
 Orbital Insertion Date Landing Date Return Date Status
Main
Mission 		Extended
Mission 		Expected Mission Duration Total Mission Duration Notes
Phase 1: Orbiter and impactor
Chandrayaan-1 22 October 2008 PSLV-XL 8 November 2008 14 November 2008 – Success 2 years 310 days First Indian Lunar mission; discovered water on the Moon.
Phase 2: Soft landers and rovers
Chandrayaan-2 22 July 2019 LVM3 20 August 2019 6 September 2019 – Partial success Ongoing 7.5 years 4 years, 10 months, 28 days elapsed First Indian Lunar lander and rover mission; lander crashed.
Chandrayaan-3 14 July 2023 5 August 2023 23 August 2023 – Success 12 days 12 days[lower-alpha 1] First Indian extraterrestrial soft landing; humanity's first soft landing near lunar south pole.
Phase 3: Onsite sampling
LUPEX TBD 2026–28 H3 TBD TBD – TBD TBD 6 months TBD Collaborative mission with JAXA. Precursor to Chandrayaan-4.[114]
Phase 4: Sample return
Chandrayaan-4 2028 LVM3 TBD TBD - TBD TBD 14 days TBD Planned sample return mission from Lunar south pole.[115]
  1. ↑ The lander and rover were hoped to turn back on for operation on 22 September 2023 had they survived the 14-earth-day lunar night, but they failed to do so, thus ending the mission.[113]

Named sites

Mission Craft Landing Date Name Region Coordinates
Chandrayaan-1 Moon Impact Probe 14 November 2008 Jawahar Point Lunar south pole

[ ⚑ ] 89°46′S 39°24′W / 89.76°S 39.40°W / -89.76; -39.40

Chandrayaan-2 Vikram 6 September 2019 Tiranga Point [ ⚑ ] 70°52′52″S 22°47′02″E / 70.8810°S 22.7840°E / -70.8810; 22.7840
Chandrayaan-3 Vikram 23 August 2023 Shiv Shakti Point [ ⚑ ] : 69°22′03″S 32°20′53″E / 69.367621°S 32.348126°E / -69.367621; 32.348126
Pragyan

Gallery

See also

References

  1. ↑ "Chandrayaan-2 mission cheaper than Hollywood film Interstellar – Times of India". 20 February 2018. https://timesofindia.indiatimes.com/home/science/chandrayaan-2-mission-cheaper-than-hollywood-film-interstellar/articleshow/62990361.cms. 
  2. ↑ "Question No. 2222: Status of Chandrayaan Programme". https://164.100.158.235/question/annex/243/Au2222.pdf. 
  3. ↑ "2003 – An Eventful Year for ISRO". https://www.isro.gov.in/update/29-dec-2003/2003-eventful-year-isro. 
  4. ↑ "Chandrayaan-2 FAQ". https://www.isro.gov.in/chandrayaan2-faq. "The name Chandrayaan means "Chandra- Moon, Yaan-vehicle", – in Indian languages (Sanskrit and Hindi), – the lunar spacecraft" 
  5. ↑ Monier Monier-Williams, A Sanskrit-English Dictionary (1899): candra: "[...] m. the moon (also personified as a deity Mn. &c)" yāna: "[...] n. a vehicle of any kind , carriage , wagon , vessel , ship , [...]"
  6. ↑ 6.0 6.1 6.2 Datta, Jayati; Chakravarty, S.C. (May 2004). "Chandrayaan-1: India's first scientific mission to the Moon.". http://shiksha.isro.gov.in/pdf/books/1.pdf. 
  7. ↑ "Spacecraft to place 525-kg satellite in polar orbit". The Times of India. 2003-08-16. ISSN 0971-8257. https://timesofindia.indiatimes.com/india/spacecraft-to-place-525-kg-satellite-in-polar-orbit/articleshow/133493.cms. 
  8. ↑ "India 'on course' for the Moon" (in en-GB). 2003-04-04. http://news.bbc.co.uk/2/hi/south_asia/2917271.stm. 
  9. ↑ "Indian space programme". October 2008. https://www.isro.gov.in/media_isro/pdf/ResourcesPdf/SpaceIndia/publication(6).pdf. 
  10. ↑ "When A Tip By APJ Abdul Kalam Helped India's 1st Moon Mission Chandrayaan-1". https://www.ndtv.com/india-news/chandrayaan-3-when-a-tip-by-apj-abdul-kalam-helped-indias-1st-moon-mission-chandrayaan-1-4321874. 
  11. ↑ "Moon Impact Probe (MIP)". ISRO. http://www.isro.org/chandrayaan/htmls/mip.htm. 
  12. ↑ "India's Moon Mission » pa". 2015-10-17. http://www.politicalaffairs.net/india-s-moon-mission/. 
  13. ↑ "India Launches First Unmanned Mission to Moon". 2009-08-01. http://www.voanews.com/english/archive/2008-10/2008-10-22-voa11.cfm. 
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  16. ↑ 16.0 16.1 16.2 "MIP detected water on Moon way back in June: ISRO Chairman" (in en-IN). The Hindu. 2009-09-25. ISSN 0971-751X. https://www.thehindu.com/sci-tech/science/MIP-detected-water-on-Moon-way-back-in-June-ISRO-Chairman/article16883362.ece. 
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  102. ↑ Neeraj Srivastava; S. Vijayan; Amit Basu Sarbadhikari (2022-09-27), "Future Exploration of the Inner Solar Syetem: Scope and the Focus Areas", Planetary Sciences Division (PSDN), Physical Research Laboratory 
  103. ↑ "SPACE.com -- The Moon's Malapert Mountain Seen As Ideal Site for Lunar Lab". 2006-02-13. http://www.space.com/scienceastronomy/solarsystem/moon_mountain_020326.html. 
  104. ↑ Watson, Kenneth; Murray, B. C.; Brown, Harrison (September 1961). "The Behavior of Volatiles on the Lunar Surface" (in English). Journal of Geophysical Research (Pasadena, California: Division of Geological Sciences, California Institute of Technology) 66 (9): 3033–3045. https://authors.library.caltech.edu/51509/. Retrieved 25 September 2023. 
  105. ↑ Pieters, C. M.; Goswami, J. N.; Clark, R. N.; Annadurai, M.; Boardman, J.; Buratti, B.; Combe, J.-P.; Dyar, M. D. et al. (2009-10-23). "Character and Spatial Distribution of OH/H 2 O on the Surface of the Moon Seen by M 3 on Chandrayaan-1" (in en). Science 326 (5952): 568–572. doi:10.1126/science.1178658. ISSN 0036-8075. https://www.science.org/doi/10.1126/science.1178658. 
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