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Imaging Infrared Spectrometer onboard Chandrayaan-2 Orbiter


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1 Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
 

Imaging Infrared Spectrometer (IIRS) is an imaging hyperspectral instrument for mineralogy of the lunar surface (including the hydroxyl signature). IIRS operates in the 0.8–5 μm spectral range with about 250 contiguous bands. It has 80 m ground sampling distance and 20 km swath at nadir from 100 km orbit altitude. Optical design is based on fore-optics and Offner (convex multi-blazed grating)-type spectrometer. Focal plane array is HgCdTe (mercury–cadmium–telluride)- based actively cooled to 90 K, having 500 × 256 pixels format with 30 μm pixel size. Electronics comprises proximity, logic and control, power supply and cooler drive electronics. Mechanical system is realized to house various subsystems, namely optics, detector, electronics and thermal components meeting the structural, opto-mechanical thermal component and alignment requirements. Thermal system is designed such that the instrument is cooled and maintained at fixed temperature to reduce and control instrument background. Aluminum-based mirror, grating and housing are developed to maintain structural as well as opto-mechanical and thermal requirements. This article presents IIRS realization and spectroradoimetric performance.

Keywords

Hyperspectral Imaging, Infrared Spectrometer, Moon, Orbiter.
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  • Imaging Infrared Spectrometer onboard Chandrayaan-2 Orbiter

Abstract Views: 427  |  PDF Views: 152

Authors

Arup Roy Chowdhury
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Arup Banerjee
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
S. R. Joshi
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Moumita Dutta
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Ankush Kumar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Satadru Bhattacharya
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Amitabh
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Sami Ur Rehman
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Sunil Bhati
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
J. C. Karelia
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Amiya Biswas
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Anish R. Saxena
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Satish Sharma
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Sandip R. Somani
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
H. V. Bhagat
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Jitendra Sharma
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
D. N. Ghonia
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
B. B. Bokarwadia
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India
Ajay Parasar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, India

Abstract


Imaging Infrared Spectrometer (IIRS) is an imaging hyperspectral instrument for mineralogy of the lunar surface (including the hydroxyl signature). IIRS operates in the 0.8–5 μm spectral range with about 250 contiguous bands. It has 80 m ground sampling distance and 20 km swath at nadir from 100 km orbit altitude. Optical design is based on fore-optics and Offner (convex multi-blazed grating)-type spectrometer. Focal plane array is HgCdTe (mercury–cadmium–telluride)- based actively cooled to 90 K, having 500 × 256 pixels format with 30 μm pixel size. Electronics comprises proximity, logic and control, power supply and cooler drive electronics. Mechanical system is realized to house various subsystems, namely optics, detector, electronics and thermal components meeting the structural, opto-mechanical thermal component and alignment requirements. Thermal system is designed such that the instrument is cooled and maintained at fixed temperature to reduce and control instrument background. Aluminum-based mirror, grating and housing are developed to maintain structural as well as opto-mechanical and thermal requirements. This article presents IIRS realization and spectroradoimetric performance.

Keywords


Hyperspectral Imaging, Infrared Spectrometer, Moon, Orbiter.

References





DOI: https://doi.org/10.18520/cs%2Fv118%2Fi3%2F368-375