ISEM (Infrared Spectrometer for ExoMars)
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1 ISEM (Infrared Spectrometer for ExoMars) Optical Box (OB) ISEM Electronic Box (EB) ISEM O. Korablev (PI), A. Ivanov (PM) A. Fedorova, N. Evodokimova, S. Mantsevich and the ISEM Team IKI - Space Research Institute, Moscow MIPT - Moscow Institute of Physics and Technology, Dolgoprudniy Vernadsky Institute of Geochemistry and Analytical Chemistry, Moscow
2 Science Team Oleg Korablev, Andrei Ivanov, Nadia Evdokimova, Anna Fedorova, Mikhail Gerasimov, Daniel Rodionov (Payload Manager) (IKI), Ruslan Kuzmin (Vernadsky) + Jean- Pierre Bibring (IAS) + TBD PanCam Co- Is, Andrew Coates TBD ExoMars Co- Is ISEM Team Technical Team Alexander Stepanov, Andrei Titov, Nick Semena, Oleg Kozlov, TaPana Kozlova, Nikita Vyazovetsky, Alexander Kiselev, Sergey Mantsevich, Julia Zhirnova, Vadim Arefiev, Michael Buntov (IKI), Yurii Kalinnikov (VNIIFTRI) PI: O. Korablev, IKI Project Manager: A. Ivanov, IKI Russian Payload Manager: D. Rodionov, IKI Science Team AOTF Yu. Kalinnikov, KBSP Thermal N Semena, IKI Electronics A. Titov, Astron Data interface and sowware: A. Stepanov, IKI Mechanics T. Kozlova, O. Kozlov, IKI
3 Science objec2ves of ISEM Geological invespgapon and study a composipon of MarPan soils in the uppermost few millimeters of the surface. CharacterizaPon the composipon of surface materials, discriminapng between various classes of silicates, oxides, hydrated minerals and carbonates. IdenPficaPon and mapping of the distribupon of aqueous alterapon products on Mars. Real- Pme assessment of surface composipon in selected areas, in support of idenpfying and selecpon of the most promising drilling sites Studies of variapons of the atmospheric dust properpes and of the atmospheric gaseous composipon (hampered by limited number of observapon cycles)
4 NIR reflectance spectra of different minerals Rockforming minerals Carbonates Spectral resolution ~2.5 nm (18-20 cm -1 )
5 ISEM main parameters OpPcal Box (OB) ISEM Electronic Box (EB) ISEM Spectral range µm Field of view 1 OpPcal point detector Spectral resolupon Power consumppon InAs (Hamamatsu P ), Two stage thermoelectrically cooled Ø1 mm 25 cm W OperaPng temperatures С. Storage temperatures Output interface Overall dimension С (TBD) RS х160х66 mm (oppcal box) 80х84х55 mm (electronic box) Mass (espmapon) 0.9 kg (oppcal box including 5m cable). 0.4 kg (electronic box)
6 ISEM OB: 3D model and optical scheme
7 Detector InAs Hamamatsu P
8 Instrument deployment. Optical box OB ISEM PanCam HRC ISEM optical block Spectral range µm FOV 1 HRC: high-resolution camera
9 Instrument deployment. Electronics box Estimation of harness length 5 meters
10 ISEM: observation scenario and data volume Current scenario: one point spectrum measurement with each of 8 HRC images on 2 sols as per Reference Surface Mission, total 16 point spectrum measurements per Measurement Cycle. Best current estimation of data volume is 100 kbits per one spectrum measurement, uncompressed No compression is in principle necessary (TBD) WAC HRC & ISEM x HRC ISEM WAC
11 Prototypes LIS (Lunar Infrared Spectrometer) More details in
12 Status. Prototypes Lunar mission Luna-Globe LIS (Lunar Infrared Spectrometer) Electrical Interface Model Optical Box Optical Box Electronics Box
13 Status. Prototypes Lunar mission Luna-Globe launch 2015 LIS (Lunar Infrared Spectrometer) laboratory prototype Entrance optics AOTF Detector and readout electronics AOTF Controller electronics
14 ISEM PanCam/HRC collaboration The optical axes of ISEM and HRC shall be aligned in the same direction within 1 and ISEM s field of view shall be inside HRC s field of view (from a distance of 2 meters). Verification of FOV co-alignment by observation of target in IR as well as in visible wavelength
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