Refine your search
Collections
Co-Authors
- R. P. Singh
- Somya S. Sarkar
- Manoj Kumar
- Anish Saxena
- U. S. H. Rao
- Arun Bhardwaj
- Jalshri Desai
- Jitendra Sharma
- Amul Patel
- Yogesh Shinde
- Hemant Arora
- A. R. Srinivas
- Jaya Rathi
- Hitesh Patel
- Meenakshi Sarkar
- Arpita Gajaria
- S. Manthira Moorthi
- Ashwin Gujrati
- Prakash Chauhan
- Kuriakose A. Saji
- D. R. M. Samudraiah
- A. S. Kiran Kumar
- Saurabh P. Vyas
- Mukesh Kumar
- Dhaval Kathiria
- Mandakini Jani
- Bimal K. Bhattacharya
Journals
A B C D E F G H I J K L M N O P Q R S T U V W X Y Z All
Pandya, Mehul R.
- Thermal Infrared Imaging Spectrometer for Mars Orbiter Mission
Abstract Views :291 |
PDF Views:244
Authors
R. P. Singh
1,
Somya S. Sarkar
1,
Manoj Kumar
1,
Anish Saxena
1,
U. S. H. Rao
1,
Arun Bhardwaj
1,
Jalshri Desai
1,
Jitendra Sharma
1,
Amul Patel
1,
Yogesh Shinde
1,
Hemant Arora
1,
A. R. Srinivas
1,
Jaya Rathi
1,
Hitesh Patel
1,
Meenakshi Sarkar
1,
Arpita Gajaria
1,
S. Manthira Moorthi
1,
Mehul R. Pandya
1,
Ashwin Gujrati
1,
Prakash Chauhan
1,
Kuriakose A. Saji
1,
D. R. M. Samudraiah
1,
A. S. Kiran Kumar
2
Affiliations
1 Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, IN
2 Indian Space Research Organisation, Bengaluru 560 231, IN
1 Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 058, IN
2 Indian Space Research Organisation, Bengaluru 560 231, IN
Source
Current Science, Vol 109, No 6 (2015), Pagination: 1097-1105Abstract
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.- Automated kharif rice mapping using SAR data and machine learning techniques in GEE platform
Abstract Views :169 |
Authors
Saurabh P. Vyas
1,
Mukesh Kumar
2,
Dhaval Kathiria
1,
Mandakini Jani
1,
Mehul R. Pandya
2,
Bimal K. Bhattacharya
2
Affiliations
1 College of Agricultural Information Technology, Anand Agricultural University, Anand 388 110, IN
2 Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, IN
1 College of Agricultural Information Technology, Anand Agricultural University, Anand 388 110, IN
2 Space Applications Centre, Indian Space Research Organisation, Ahmedabad 380 015, IN