Miniature thermal emission spectrometer for the Mars Exploration Rover
By S. Silverman, R. Peralta, Philip R. Christensen, G. Mehall. SPIE Optics + Photonics, 2002
207 citations recorded by the source corpus.
Subfields: Aerospace Engineering, Global and Planetary Change, Statistical and Nonlinear Physics
View Paper: https://www.semanticscholar.org/paper/0553db442a5a42fdd5277e1df2688b7303c7588c
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In Aerospace Engineering
- Francois Forget
- Michael J. Wolff
- Ehouarn Millour
- Robert J. Wilson
- B. Cantor
- Michael D. Smith
- Mark T. Lemmon
- L. Montabone
In Global and Planetary Change
- Michael D. Smith
- Robert J. Wilson
- Ehouarn Millour
- Francois Forget
- B. Cantor
- D. Kass
- Mark T. Lemmon
- S. Squyres
In Statistical and Nonlinear Physics
Citations in the corpus
- Mineralogy of the Martian Surface (2014, background): “…(Opportunity) Mini-TES Miniature Thermal Emission Spectrometer Rover Thermal infrared point spectroscopy (landed; 5–29 μm; 20 mrad; i.e., 20-cm spots at 10 m) Christensen et al. 2003 2004–present OMEGA Observatoire pour la Minéralogie, l’Eau, les Glaces, et l’Activité Orbit…”
- Athena MIMOS II Mossbauer spectrometer investigation (2003, methodology): “These spectra are obtained from the SRAM according to a pre-defined summation strategy.”
- The Thermal Emission Imaging System (THEMIS) for the Mars 2001 Odyssey Mission (2004, unknown): “The Rover payloads contain miniature versions of the MGS TES instrument (Silverman et al., 1999) covering the THEMIS spectral region.”
- Eight-year climatology of dust optical depth on Mars (2014, background): “During this period of time, the Thermal Emission Spectrometer (TES, Christensen et al., 2001) aboard MGS, the Thermal Emission Imaging System (THEMIS, Christensen et al., 2004) on ODY, and the Mars Climate Sounder (MCS, McCleese et al., 2007) on MRO provided global coverage of radiance observations ”
- High-resolution thermal inertia derived from the Thermal Emission Imaging System (THEMIS): Thermal model and applications (2006, unknown): “Changes in the 264instrument response function during launch and orbit inser265tion were minimal [Christensen et al., 2003a, 2004], and the 266nighttime temperatures are calibrated to within a precision of 2671.2 K and an absolute accuracy of!”