Change search
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf
Infrared Spectrometer for ExoMars: A Mast-Mounted Instrument for the Rover
Space Research Institute IKI, Moscow, Russia.
Space Research Institute IKI, Moscow, Russia.
Space Research Institute IKI, Moscow, Russia.
Space Research Institute IKI, Moscow, Russia.
Show others and affiliations
2017 (English)In: Astrobiology, ISSN 1531-1074, E-ISSN 1557-8070, Vol. 17, no 6-7, p. 542-564Article in journal (Refereed) Published
Abstract [en]

ISEM (Infrared Spectrometer for ExoMars) is a pencil-beam infrared spectrometer that will measure reflected solar radiation in the near infrared range for context assessment of the surface mineralogy in the vicinity of the ExoMars rover. The instrument will be accommodated on the mast of the rover and will be operated together with the panoramic camera (PanCam), high-resolution camera (HRC). ISEM will study the mineralogical and petrographic composition of the martian surface in the vicinity of the rover, and in combination with the other remote sensing instruments, it will aid in the selection of potential targets for close-up investigations and drilling sites. Of particular scientific interest are water-bearing minerals, such as phyllosilicates, sulfates, carbonates, and minerals indicative of astrobiological potential, such as borates, nitrates, and ammonium-bearing minerals. The instrument has an ∼1° field of view and covers the spectral range between 1.15 and 3.30 μm with a spectral resolution varying from 3.3 nm at 1.15 μm to 28 nm at 3.30 μm. The ISEM optical head is mounted on the mast, and its electronics box is located inside the rover's body. The spectrometer uses an acousto-optic tunable filter and a Peltier-cooled InAs detector. The mass of ISEM is 1.74 kg, including the electronics and harness. The science objectives of the experiment, the instrument design, and operational scenarios are described.

Place, publisher, year, edition, pages
Mary Ann Liebert, 2017. Vol. 17, no 6-7, p. 542-564
National Category
Aerospace Engineering
Research subject
Atmospheric Science
Identifiers
URN: urn:nbn:se:ltu:diva-65102DOI: 10.1089/ast.2016.1543ISI: 000406038400003PubMedID: 28731817Scopus ID: 2-s2.0-85025436062OAI: oai:DiVA.org:ltu-65102DiVA, id: diva2:1133318
Note

Validerad; 2017; Nivå 2; 2017-08-16 (andbra)

Available from: 2017-08-15 Created: 2017-08-15 Last updated: 2023-11-21Bibliographically approved

Open Access in DiVA

No full text in DiVA

Other links

Publisher's full textPubMedScopus

Authority records

Martin-Torres, JavierZorzano Mier, Maria-Paz

Search in DiVA

By author/editor
Martin-Torres, JavierZorzano Mier, Maria-Paz
By organisation
Space Technology
In the same journal
Astrobiology
Aerospace Engineering

Search outside of DiVA

GoogleGoogle Scholar

doi
pubmed
urn-nbn

Altmetric score

doi
pubmed
urn-nbn
Total: 96 hits
CiteExportLink to record
Permanent link

Direct link
Cite
Citation style
  • apa
  • ieee
  • modern-language-association-8th-edition
  • vancouver
  • Other style
More styles
Language
  • de-DE
  • en-GB
  • en-US
  • fi-FI
  • nn-NO
  • nn-NB
  • sv-SE
  • Other locale
More languages
Output format
  • html
  • text
  • asciidoc
  • rtf