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Thermal Infrared Imaging Spectrometer for Mars Orbiter Mission


Affiliations
1 Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
2 Indian Space Research Organisation, Bengaluru 560 231, India
 

Thermal Infrared Imaging Spectrometer (TIS), which operates in the infrared spectral region (7-13 μm), is one of the five instruments on-board the Mars Orbiting Mission (MOM). TIS was designed to detect emitted thermal infrared radiation from the Martian environment, which would enable the estimation of ground temperature of the surface of Mars and also map its surface composition. TIS instrument is a grating-based spectrometer which has spatial resolution of 258 m at periapsis (372 km). TIS hardware was realized with light-weight miniaturized components (total weight 3.2 kg) with power requirement of 6 W. Observations from TIS instrument were carried out during Earth-bound manoeuvres and cruise phase operations of MOM and the results were found to be in agreement with the laboratory measurements.

Keywords

Aerosol Optical Thickness, Mars Orbiter, Minerals Detection, Thermal Infrared Spectroscopy.
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  • Thermal Infrared Imaging Spectrometer for Mars Orbiter Mission

Abstract Views: 351  |  PDF Views: 265

Authors

R. P. Singh
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Somya S. Sarkar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Manoj Kumar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Anish Saxena
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
U. S. H. Rao
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Arun Bhardwaj
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Jalshri Desai
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Jitendra Sharma
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Amul Patel
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Yogesh Shinde
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Hemant Arora
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
A. R. Srinivas
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Jaya Rathi
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Hitesh Patel
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Meenakshi Sarkar
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Arpita Gajaria
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
S. Manthira Moorthi
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Mehul R. Pandya
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Ashwin Gujrati
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Prakash Chauhan
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
Kuriakose A. Saji
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
D. R. M. Samudraiah
Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, India
A. S. Kiran Kumar
Indian Space Research Organisation, Bengaluru 560 231, India

Abstract


Thermal Infrared Imaging Spectrometer (TIS), which operates in the infrared spectral region (7-13 μm), is one of the five instruments on-board the Mars Orbiting Mission (MOM). TIS was designed to detect emitted thermal infrared radiation from the Martian environment, which would enable the estimation of ground temperature of the surface of Mars and also map its surface composition. TIS instrument is a grating-based spectrometer which has spatial resolution of 258 m at periapsis (372 km). TIS hardware was realized with light-weight miniaturized components (total weight 3.2 kg) with power requirement of 6 W. Observations from TIS instrument were carried out during Earth-bound manoeuvres and cruise phase operations of MOM and the results were found to be in agreement with the laboratory measurements.

Keywords


Aerosol Optical Thickness, Mars Orbiter, Minerals Detection, Thermal Infrared Spectroscopy.



DOI: https://doi.org/10.18520/cs%2Fv109%2Fi6%2F1097-1105