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HEND physical calibrations : status report. A. Kozyrev, S. Charyshnikov, V. Grinkov,, M. Litvak, I. Mitrofanov, A. Sanin, V. Tret’yakov Institute for Space Research V. Shvetsov, G. Timoshenko, A. Krylov Joint Institute for Nuclear Research. Schematic design of HEND.
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HEND physicalcalibrations: status report A. Kozyrev, S. Charyshnikov, V. Grinkov,, M. Litvak, I. Mitrofanov, A. Sanin, V. Tret’yakov Institute for Space Research V. Shvetsov, G. Timoshenko, A. Krylov Joint Institute for Nuclear Research
Schematic design of sensor LD (Left) and SD (Right) for epithermal neutrons
He3+n→H3+p+ Etotal Etotal = 0.764 MeV E(H3) = 1/4 Etotal = 0.191 MeV E(p) = 3/4 Etotal = 0.573 MeV ¼Etotal TRITON ¾Etotal PROTON
Measured spectrum of counts of MD sensor is represented in 16 channels
Schematic design of stilbene and CsI scintillation detectors
Registration of neutrons on recoil protons Neutron Recoil proton
Separation between background and recoil protons is done by help of anticoincidence circuit based on CsI crystal which surrounds stilbene detector in direction of open space Proton
Distinguishing between neutron and gamma signal in stilbene crystal is done by help of electronic pulse shape in the stilbene crystal Photon
Performance • Energy range: • LD:10.0 eV- 1.0 MeV • MD:0.4 eV-100.0 keV • SD:0.4 eV- 1.0 keV • IN/SC/N: 850 keV – 15.0 MeV • IN/SC/G:60 keV– 2.0 MeV • OUT/SC:30 keV – 1.0 MeV
Stabilityspectra and temperature during mapping 18/02/2002-18/04/2002 2 month 01/04/2003-01/06/2003 2 month 10/09/2002-10/11/2002 2 month
Stability spectra during mapping LD MD CsI(Tl) Stilbene
Stability temperature during mapping Second First Third +15 -15 • t°1- temperature of main electronic board • t°2- temperature of HV board • t°3- temperature of stilbene electronic board -15 < t°HEND < +15
Calibration Facility Source of neutrons Flux ~ 106 n cm2 /sec d(T,n) (15 MeV n) d(D,n) 3He (5 MeV n) 7Li(p,n)7Be (< 1 MeV n)
Calibration Facility Cf source: 2.1 MeV (13.2+/-0.2)/r2n cm-2 s-1 Pu-Be source: 3.8 MeV (29.6+/-0.2)/r2n cm-2 s-1
HEND energy range Response functions of LD, MD and SC/neutron sensors allow to fit data of #2, #3 and #4 periapses with function of type E-
Using response function Model neutron spectra on Mars orbit Model count of HEND neutron sensor Calculation Response function of HEND sensors Calculation (Pearson criteria) Probability of aligning model Real count of HEND neutron sensor
Conclusion: • During mapping, spectra of HEND sensors were stable • During mapping, temperature of HEND instrument were lie in the range of +/- 15 °C • HEND numerical model as an assembly were simulated for neutron LD, MD and SD sensor • Future task: • Building of HEND numerical model with taking into account the spacecraft model • Physical calibration and simulation of SC sensor to establishing of corresponds between Flight and Qualification units • Physical calibration of HEND instrument with respect to gamma-rays and charge particles