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Lyman Alpha Photometer: a far-ultraviolet sensor for the study of hydrogen isotope ratio in the Martian exosphere


Affiliations
1 Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
 

The Lyman Alpha Photometer (LAP), developed for flight on the Mars Orbiter Mission (MOM) spacecraft in 2013, is primarily designed to measure deuterium to hydrogen abundance ratio of the Martian exosphere over a 6-month period from a 263 km × 71,358 km elliptical orbit around Mars. A set of ultrapure (99.999%) hydrogen and deuterium gas-filled cells comprising tungsten filaments, a 25 mm diameter collection lens and a solar-blind photomultiplier tube together with an 8 nm bandpass Lyman alpha filter are the principal electro-optical assemblies of the instrument. This article presents scientific objectives of LAP and its performance specifications along with details of instrument design. The ground characterization techniques to assess LAP operational performance are also presented. End-to-end test results and evaluation matrix of LAP were satisfactory, well within the desired specifications. The first LAP onboard operation was carried out during the cruise phase of MOM spacecraft journey to verify its functionality and all recorded on-board health parameters were satisfactory.

Keywords

Absorption gas cell, hydrogen isotope ratio, Martian exosphere, photometer
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  • Lyman Alpha Photometer: a far-ultraviolet sensor for the study of hydrogen isotope ratio in the Martian exosphere

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Authors

Raja V. L. N. Sridhar
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
M. V. H. Rao
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
K. Kalyani
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
Anand Chandran
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
Monika Mahajan
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
J. D. P. V. Tayaramma
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
K. V. S. Bhaskar
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
K. B. Pramod
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
L. V. Prasad
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
A. S. Laxmiprasad
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
P. Chakraborty
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
J. A. Kamalakar
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
G. Nagendra Rao
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India
M. Viswanathan
Laboratory for Electro-Optics Systems, Indian Space Research Organisation, Bengaluru 560 058, India

Abstract


The Lyman Alpha Photometer (LAP), developed for flight on the Mars Orbiter Mission (MOM) spacecraft in 2013, is primarily designed to measure deuterium to hydrogen abundance ratio of the Martian exosphere over a 6-month period from a 263 km × 71,358 km elliptical orbit around Mars. A set of ultrapure (99.999%) hydrogen and deuterium gas-filled cells comprising tungsten filaments, a 25 mm diameter collection lens and a solar-blind photomultiplier tube together with an 8 nm bandpass Lyman alpha filter are the principal electro-optical assemblies of the instrument. This article presents scientific objectives of LAP and its performance specifications along with details of instrument design. The ground characterization techniques to assess LAP operational performance are also presented. End-to-end test results and evaluation matrix of LAP were satisfactory, well within the desired specifications. The first LAP onboard operation was carried out during the cruise phase of MOM spacecraft journey to verify its functionality and all recorded on-board health parameters were satisfactory.

Keywords


Absorption gas cell, hydrogen isotope ratio, Martian exosphere, photometer

References





DOI: https://doi.org/10.18520/cs%2Fv109%2Fi6%2F1114-1120