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Indian Mini Satellite bus

March 03, 2023

Indian Mini Satellite (IMS) is a family of modular[1] mini satellite buses developed by the Indian Space Research Organisation (ISRO).[2][3]

Variants

Indian Mini Satellite (Variants)
Feature IMS-1[4][5][6][predatory publisher] IMS-2[6][7] IMS-3 (Planned IMS-2 Derivative)[8]
Launch Mass 100 kilograms (220 lb) 450 kilograms (990 lb) 450 kilograms (990 lb)
Maximum bus mass 70 kilograms (150 lb) 250 kilograms (550 lb) 250 kilograms (550 lb)
Payload mass 30 kilograms (66 lb) 200 kilograms (440 lb) 200 kilograms (440 lb)
Propellant 3.5 kilograms (7.7 lb) 21 kilograms (46 lb)
Design lifetime 2 years 5 years
Raw bus voltage 28-33 Volts 28-33 Volts 28-42 Volts
Solar Array Power 330 Watts (EOL) 675 Watts (EOL)
850 Watts (BOL) 		850 Watts (BOL)
Payload power 30 Watts (Continuous)
70 Watts (Duty Cycle) 		250 Watts (Continuous)
600 Watts (Duty Cycle) 		250 Watts (Continuous)
400 Watts (Duty Cycle)
Attitude Control 3-axis stabilized
Four Reaction Wheels
Single 1N thruster 		3-axis stabilized
Four Reaction Wheels
Mono-propellant RCS
Four 1N thrusters
Four 0.2N thrusters
Pointing Accuracy ±0.1° (3σ) (all axes) ± 0.1° (all axes) ± 0.1° (all axes)
SSR Storage 32 Gb 32 Gb (SDRAM)
256 Gb (Flash Memory) 		32 Gb (SDRAM)
256 Gb (Flash Memory)
Payload data storage ≤ 16 Gb ≤ 32 Gb
Downlink ≤ 8 Mbit/s DL rate ≤ 105 Mbit/s DL rate ≤ 160 Mbit/s DL rate
Missions IMS-1[9]
Youthsat[10]
Microsat-TD[11]		 SARAL[12]
ScatSat-1[13]
EMISAT[14]
HySIS

XPoSat (Planned)

 
IMS-1

See also

References

  1. ^ "63rd International Astronautical Congress 2012 : 19th SYMPOSIUM ON SMALL SATELLITE MISSIONS (B4) : Generic Technologies for Small/Micro Platforms (6A)" (PDF). Iafastro.net. Retrieved 10 August 2017.
    - "SARAL - eoPortal Directory - Satellite Missions". Directory.eoportal.org. Retrieved 10 August 2017.
  2. ^ (PDF). Archived from the original (PDF) on 8 March 2014. Retrieved 7 February 2014.{{cite web}}: CS1 maint: archived copy as title (link)
  3. ^ Thyagarajan, K; Raghava Murthy, D.V.A. (3 June 2009). "Micro- and mini-satellites of ISRO—technology and applications". Acta Astronautica. 65 (9, 10): 1375–1382. Bibcode:2009AcAau..65.1375T. doi:10.1016/j.actaastro.2009.03.050.
  4. ^ "IMS-1 - eoPortal Directory - Satellite Missions". directory.eoportal.org. Retrieved 2018-11-05.
  5. ^ "Interest Exploratory Note: Indian Mini Satellite-1 (IMS-1) Bus" (PDF). 15 March 2022. (PDF) from the original on 15 March 2022. Retrieved 15 March 2022.
  6. ^ a b (PDF). International Journal of Pure and Applied Mathematics. 118 (17): 273–288. 6 January 2018. Archived from the original (PDF) on 4 November 2018. Retrieved 5 Nov 2018.
  7. ^ "SARAL - Satellite for Argos and AltiKa" (PDF). MOSDAC. Retrieved 5 Nov 2018.
  8. ^ Annadurai, Mylswamy (22 January 2015). (PDF). NRSC.gov.in. Archived from the original (PDF) on 27 March 2015.
  9. ^ "IMS-1 - ISRO". isro.gov.in. Retrieved 28 October 2015.
  10. ^ "YouthSat (IMS 1A)". Space.skyrocket.de. Retrieved 28 October 2015.
  11. ^ . ISRO. Archived from the original on 25 January 2018. Retrieved 12 January 2018.
  12. ^ . isro.gov.in. Archived from the original on 31 July 2017. Retrieved 28 October 2015.
    - "Old Faithful does it again". The Hindu. 2013-02-27. Retrieved 28 October 2015.
  13. ^ "SCATSat-1 (Scatterometer Satellite-1)". Directory.eoportal.org. Retrieved 10 August 2017.
  14. ^ Krebs, Gunter. "EMISAT". Gunter's Space Page. Retrieved 24 January 2018.


 

This article about one or more spacecraft of India is a stub. You can help Wikipedia by expanding it.

March 03, 2023
indian, mini, satellite, indian, mini, satellite, family, modular, mini, satellite, buses, developed, indian, space, research, organisation, isro, variants, editindian, mini, satellite, variants, feature, predatory, publisher, planned, derivative, launch, mass. Indian Mini Satellite IMS is a family of modular 1 mini satellite buses developed by the Indian Space Research Organisation ISRO 2 3 Variants EditIndian Mini Satellite Variants Feature IMS 1 4 5 6 predatory publisher IMS 2 6 7 IMS 3 Planned IMS 2 Derivative 8 Launch Mass 100 kilograms 220 lb 450 kilograms 990 lb 450 kilograms 990 lb Maximum bus mass 70 kilograms 150 lb 250 kilograms 550 lb 250 kilograms 550 lb Payload mass 30 kilograms 66 lb 200 kilograms 440 lb 200 kilograms 440 lb Propellant 3 5 kilograms 7 7 lb 21 kilograms 46 lb Design lifetime 2 years 5 yearsRaw bus voltage 28 33 Volts 28 33 Volts 28 42 VoltsSolar Array Power 330 Watts EOL 675 Watts EOL 850 Watts BOL 850 Watts BOL Payload power 30 Watts Continuous 70 Watts Duty Cycle 250 Watts Continuous 600 Watts Duty Cycle 250 Watts Continuous 400 Watts Duty Cycle Attitude Control 3 axis stabilizedFour Reaction WheelsSingle 1N thruster 3 axis stabilizedFour Reaction WheelsMono propellant RCSFour 1N thrustersFour 0 2N thrustersPointing Accuracy 0 1 3s all axes 0 1 all axes 0 1 all axes SSR Storage 32 Gb 32 Gb SDRAM 256 Gb Flash Memory 32 Gb SDRAM 256 Gb Flash Memory Payload data storage 16 Gb 32 GbDownlink 8 Mbit s DL rate 105 Mbit s DL rate 160 Mbit s DL rateMissions IMS 1 9 Youthsat 10 Microsat TD 11 SARAL 12 ScatSat 1 13 EMISAT 14 HySIS XPoSat Planned IMS 1See also Edit Spaceflight portalComparison of satellite busesReferences Edit 63rd International Astronautical Congress 2012 19th SYMPOSIUM ON SMALL SATELLITE MISSIONS B4 Generic Technologies for Small Micro Platforms 6A PDF Iafastro net Retrieved 10 August 2017 SARAL eoPortal Directory Satellite Missions Directory eoportal org Retrieved 10 August 2017 Archived copy PDF Archived from the original PDF on 8 March 2014 Retrieved 7 February 2014 a href Template Cite web html title Template Cite web cite web a CS1 maint archived copy as title link Thyagarajan K Raghava Murthy D V A 3 June 2009 Micro and mini satellites of ISRO technology and applications Acta Astronautica 65 9 10 1375 1382 Bibcode 2009AcAau 65 1375T doi 10 1016 j actaastro 2009 03 050 IMS 1 eoPortal Directory Satellite Missions directory eoportal org Retrieved 2018 11 05 Interest Exploratory Note Indian Mini Satellite 1 IMS 1 Bus PDF 15 March 2022 Archived PDF from the original on 15 March 2022 Retrieved 15 March 2022 a b Small Satellites in Inclined Orbits to Increase Observation Capability Feasibility Analysis PDF International Journal of Pure and Applied Mathematics 118 17 273 288 6 January 2018 Archived from the original PDF on 4 November 2018 Retrieved 5 Nov 2018 SARAL Satellite for Argos and AltiKa PDF MOSDAC Retrieved 5 Nov 2018 Annadurai Mylswamy 22 January 2015 Earth Observation amp Small Satellite Systems User Interaction Meet 2015 PDF NRSC gov in Archived from the original PDF on 27 March 2015 IMS 1 ISRO isro gov in Retrieved 28 October 2015 YouthSat IMS 1A Space skyrocket de Retrieved 28 October 2015 Microsat ISRO Archived from the original on 25 January 2018 Retrieved 12 January 2018 SARAL ISRO isro gov in Archived from the original on 31 July 2017 Retrieved 28 October 2015 Old Faithful does it again The Hindu 2013 02 27 Retrieved 28 October 2015 SCATSat 1 Scatterometer Satellite 1 Directory eoportal org Retrieved 10 August 2017 Krebs Gunter EMISAT Gunter s Space Page Retrieved 24 January 2018 This article about one or more spacecraft of India is a stub You can help Wikipedia by expanding it vte Retrieved from https en wikipedia org w index php title Indian Mini Satellite bus amp oldid 1134888715, wikipedia, wiki, book, books, library,

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