Aditya-L1

Aditya L1(Sanskrit: आदित्य, lit: Sun,[7] pronunciation ) is a planned coronagraphy spacecraft to study solar atmosphere, currently being designed and developed by Indian Space Research Organisation (ISRO) and various other Indian research institutes.[1] It will be inserted in a halo orbit around the L1 point between Earth and Sun where it will study solar atmosphere, solar magnetic storms and it's impact on environment around Earth.

Aditya-L1
Aditya-L1 in deployed configuration
Mission typeSolar observation
OperatorISRO
Mission duration5 years (planned)[1]
Spacecraft properties
BusI-1K
ManufacturerISRO / IUCAA / IIA
Launch mass1,475 kg (3,252 lb) [2]
Payload mass244 kg (538 lb) [1]
Start of mission
Launch dateSept/Oct 2022 (planned) [2][3][4]
RocketPSLV-XL (PSLV-C56) [5][1]
Launch siteSatish Dhawan Space Centre
ContractorIndian Space Research Organisation
Orbital parameters
Reference systemSun–Earth L1
RegimeHalo orbit
Period177.86 days [6]
 

The spacecraft will study coronal heating, solar wind acceleration, coronal magnetometry, origin and monitoring of near-UV solar radiation and continuously observe photosphere, chromosphere and corona, solar energetic particles and magnetic field of the Sun.

First dedicated Indian mission to observe Sun, it is planned to be launched in Sept/Oct 2022 aboard a PSLV-XL launch vehicle.[2][3][5][8][9][4]

History

Aditya was conceptualised in January 2008 by the Advisory Committee for Space Research. It was initially envisaged as a small 400 kg (880 lb), low-Earth orbiting satellite with a coronagraph to study the solar corona. An experimental budget of 3 Crore INR was allocated for the financial year 2016–2017.[10][11][12] The scope of the mission has since been expanded and it is now planned to be a comprehensive solar and space environment observatory to be placed at the Lagrange point L1,[13] so the mission was renamed "Aditya-L1". As of July 2019, the mission has an allocated cost of ₹378.53 crore excluding launch costs.[14]

Overview

Lagrange points in the Sun–Earth system (not to scale) – a small object at any one of the five points will hold its relative position.

The Aditya-L1 mission will take around 109 Earth days after launch[15] to reach the halo orbit around the L1 point, which is about 1,500,000 km (930,000 mi) from Earth. The 1,500 kg (3,300 lb) satellite carries seven science payloads with diverse objectives, including but not limited to, the coronal heating, solar wind acceleration, coronal magnetometry, origin and monitoring of near-UV solar radiation (which drives Earth's upper atmospheric dynamics and global climate), coupling of the solar photosphere to chromosphere and corona, in-situ characterisations of the space environment around Earth by measuring energetic particle fluxes and magnetic fields of the solar wind and solar magnetic storms that have adverse effects on space and ground-based technologies.[1]

Aditya-L1 will be able to provide observations of Sun's photosphere, chromosphere and corona. In addition, an instrument will study the solar energetic particles' flux reaching the L1 orbit, while a magnetometer payload will measure the variation in magnetic field strength at the halo orbit around L1. These payloads have to be placed outside the interference from the Earth's magnetic field and hence could not have been useful in the low Earth orbit as proposed on the original Aditya mission concept.[16]

One of the major unsolved issues in the field of solar physics is that the upper atmosphere of the Sun is 1,000,000 K (1,000,000 °C; 1,800,000 °F) hot whereas the lower atmosphere is just 6,000 K (5,730 °C; 10,340 °F). In addition, it is not understood how exactly the Sun's radiation affects the dynamics of the Earth's atmosphere on shorter as well as on longer time scale. The mission will obtain near simultaneous images of the different layers of the Sun's atmosphere, which reveal the ways in which the energy may be channeled and transferred from one layer to another. Thus the Aditya-L1 mission will enable a comprehensive understanding of the dynamical processes of the Sun and address some of the outstanding problems in solar physics and heliophysics.

Payloads

  • Visible Emission Line Coronagraph (VELC): The coronagraph creates an artificial total solar eclipse in space by blocking the sunlight by an occultor. This telescope will have capabilities of spectral imaging of the corona in visible and infra-red wavelengths. The objectives are to study the diagnostic parameters of solar corona and dynamics and origin of coronal mass ejections (using three visible and one infra-red channels); magnetic field measurements of the solar corona down to tens of Gauss. Additional objectives are to determine why the solar atmosphere is so hot, and how the changes in the Sun can affect space weather and Earth's climate. The VELC payload weighs nearly 170 kg (370 lb).[17]
  • Aditya Solar wind Particle Experiment (ASPEX):[18] To study the variation and properties of the solar wind as well as its distribution and spectral characteristics.
  • Plasma Analyser Package for Aditya (PAPA): To understand the composition of solar wind and its energy distribution.
    • PI Institute: Space Physics Laboratory (SPL), VSSC
  • High Energy L1 Orbiting X-ray Spectrometer (HEL1OS): To observe the dynamic events in the solar corona and provide an estimate of the energy used to accelerate the solar energetic particles during the eruptive events.

See also

References

  1. Somasundaram, Seetha; Megala, S. (25 August 2017). "Aditya-L1 mission" (PDF). Current Science. 113 (4): 610. Bibcode:2017CSci..113..610S. doi:10.18520/cs/v113/i04/610-612. Archived from the original (PDF) on 25 August 2017. Retrieved 25 August 2017.
  2. International Space Conference and Exhibition - DAY 3 (video). Confederation of Indian Industry. 15 September 2021. Event occurs at 2:07:36–2:08:38. Retrieved 18 September 2021 via YouTube.
  3. Dutt, Anonna (17 September 2021). "India's first solar mission likely to launch next year". The Hindustan Times. Retrieved 18 September 2021.
  4. Kumar, Chethan (2 February 2022). "2 key Gaganyaan crew abort tests, Aditya top priority". The Times of India. Retrieved 2 February 2022.
  5. "Questions in the Lok Sabha (AU2587)" (PDF). Lok Sabha. 10 March 2021. Retrieved 18 September 2021.
  6. Sreekumar, P. (19 June 2019). "Indian Space Science & Exploration : Global Perspective" (PDF). UNOOSA. p. 8. Retrieved 30 June 2019.
  7. "Aditya". Spoken Sanskrit. Archived from the original on 19 July 2011. Retrieved 14 November 2008.
  8. "Aditya L1: Know Everything about ISRO's First Solar Mission". jagranjosh.com. 30 December 2019. Retrieved 31 December 2019.
  9. "8 pictures you must see to understand what ISRO's Aditya-L1 is looking for". Business Insider. Retrieved 31 December 2019.
  10. "Notes on Demands for Grants, 2016-2017" (PDF) (Press release). Department of Space. Archived from the original (PDF) on 17 September 2016. Retrieved 9 September 2016.
  11. "Aditya gets ready to gaze at the sun". The Hindu. Retrieved 25 August 2017.
  12. Gandhi, Divya (13 January 2008). "ISRO planning to launch satellite to study the sun". The Hindu. Retrieved 26 August 2017.
  13. Desikan, Shubashree (15 November 2015). "The sun shines on India's Aditya". The Hindu. Retrieved 12 August 2018.
  14. "Lok Sabha Unstarred Question No.1972" (PDF). Lok Sabha. 3 July 2019.
  15. "Department Of Space, Annual Report 2019-2020" (PDF). 14 February 2020. Archived (PDF) from the original on 7 October 2021. Retrieved 25 October 2021.
  16. "Aditya-L1 First Indian mission to study the Sun". isro.gov.in. Retrieved 19 June 2019.
  17. Desikan, Shubashree (26 November 2017). "Here comes the sun watcher, India's Aditya-L1". The Hindu. Retrieved 26 November 2017.
  18. Goyal, S. K. (18 April 2018). "Aditya Solarwind Particle EXperiment (ASPEX) onboard the Aditya-L1 mission". Planetary and Space Science. 163: 42–55. Bibcode:2018P&SS..163...42G. doi:10.1016/j.pss.2018.04.008. S2CID 125867275. Retrieved 18 May 2020.
  19. Yadav, Vipin K. (8 November 2017). "Science objectives of the magnetic field experiment onboard Aditya-L1 spacecraft". Advances in Space Research. 61 (2): 749–758. doi:10.1016/j.asr.2017.11.008. Retrieved 18 May 2020.
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