The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on Mars

We describe the parameters that drive the design and modeling of the Rover Environmental Monitoring Station (REMS) Ground Temperature Sensor (GTS), an instrument aboard NASA’s Mars Science Laboratory, and report preliminary test results. REMS GTS is a lightweight, low-power, and low cost pyrometer f...

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Main Authors: Miguel Ramos, Eduardo Sebastián, Carlos Armiens, Javier Gómez-Elvira, María P. Zorzano, Jesus Martinez-Frias, Blanca Esteban
Format: Article
Language:English
Published: MDPI AG 2010-10-01
Series:Sensors
Subjects:
Online Access:http://www.mdpi.com/1424-8220/10/10/9211/
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spelling doaj-6a60c71d5b5646cbbd2e1dc980fc6ca62020-11-24T20:58:11ZengMDPI AGSensors1424-82202010-10-0110109211923110.3390/s101009211The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on MarsMiguel RamosEduardo SebastiánCarlos ArmiensJavier Gómez-ElviraMaría P. ZorzanoJesus Martinez-FriasBlanca EstebanWe describe the parameters that drive the design and modeling of the Rover Environmental Monitoring Station (REMS) Ground Temperature Sensor (GTS), an instrument aboard NASA’s Mars Science Laboratory, and report preliminary test results. REMS GTS is a lightweight, low-power, and low cost pyrometer for measuring the Martian surface kinematic temperature. The sensor’s main feature is its innovative design, based on a simple mechanical structure with no moving parts. It includes an in-flight calibration system that permits sensor recalibration when sensor sensitivity has been degraded by deposition of dust over the optics. This paper provides the first results of a GTS engineering model working in a Martian-like, extreme environment. http://www.mdpi.com/1424-8220/10/10/9211/IR ground temperature sensorsensor thermal modelspacecraft instrumentationin-flight calibration
collection DOAJ
language English
format Article
sources DOAJ
author Miguel Ramos
Eduardo Sebastián
Carlos Armiens
Javier Gómez-Elvira
María P. Zorzano
Jesus Martinez-Frias
Blanca Esteban
spellingShingle Miguel Ramos
Eduardo Sebastián
Carlos Armiens
Javier Gómez-Elvira
María P. Zorzano
Jesus Martinez-Frias
Blanca Esteban
The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on Mars
Sensors
IR ground temperature sensor
sensor thermal model
spacecraft instrumentation
in-flight calibration
author_facet Miguel Ramos
Eduardo Sebastián
Carlos Armiens
Javier Gómez-Elvira
María P. Zorzano
Jesus Martinez-Frias
Blanca Esteban
author_sort Miguel Ramos
title The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on Mars
title_short The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on Mars
title_full The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on Mars
title_fullStr The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on Mars
title_full_unstemmed The Rover Environmental Monitoring Station Ground Temperature Sensor: A Pyrometer for Measuring Ground Temperature on Mars
title_sort rover environmental monitoring station ground temperature sensor: a pyrometer for measuring ground temperature on mars
publisher MDPI AG
series Sensors
issn 1424-8220
publishDate 2010-10-01
description We describe the parameters that drive the design and modeling of the Rover Environmental Monitoring Station (REMS) Ground Temperature Sensor (GTS), an instrument aboard NASA’s Mars Science Laboratory, and report preliminary test results. REMS GTS is a lightweight, low-power, and low cost pyrometer for measuring the Martian surface kinematic temperature. The sensor’s main feature is its innovative design, based on a simple mechanical structure with no moving parts. It includes an in-flight calibration system that permits sensor recalibration when sensor sensitivity has been degraded by deposition of dust over the optics. This paper provides the first results of a GTS engineering model working in a Martian-like, extreme environment.
topic IR ground temperature sensor
sensor thermal model
spacecraft instrumentation
in-flight calibration
url http://www.mdpi.com/1424-8220/10/10/9211/
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