HEND physical calibrations : status report

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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. - PowerPoint PPT Presentation

Transcript of HEND physical calibrations : status report

2001 Mars Odysseypage 1

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

HENDHEND physical physical calibrationscalibrations:: status status reportreport

A. Kozyrev, S. Charyshnikov, V. Grinkov,, M. Litvak, I. Mitrofanov, A. Sanin, V. Tret’yakov

Institute for Space Research

V. Shvetsov, G. Timoshenko, A. KrylovJoint Institute for Nuclear Research

2001 Mars Odysseypage 2

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Schematic design of HENDSchematic design of HEND

2001 Mars Odysseypage 3

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Schematic design of sensor LD (Left) and Schematic design of sensor LD (Left) and SD (Right) for epithermal neutronsSD (Right) for epithermal neutrons

2001 Mars Odysseypage 4

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Components of Components of SD and LD SD and LD

sensorssensors

2001 Mars Odysseypage 5

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

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

¼ Etotal

TRITON¾ Etotal

PROTON

2001 Mars Odysseypage 6

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Measured spectrum of counts

of MD sensor is represented in 16

channels

2001 Mars Odysseypage 7

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Schematic design Schematic design of stilbene and of stilbene and

CsI scintillation CsI scintillation detectorsdetectors

2001 Mars Odysseypage 8

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Neutron

Recoil protonRecoil proton

Registration of neutrons on recoil

protons 

2001 Mars Odysseypage 9

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

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

2001 Mars Odysseypage 10

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Photon

Distinguishing between neutron and gamma signal in

stilbene crystal is done by help of electronic pulse shape in the

stilbene crystal

2001 Mars Odysseypage 11

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

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

PerformancePerformance

2001 Mars Odysseypage 12

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

18/02/2002 24/07/2002 27/12/2002 01/06/2003

Maping(1 year 4 month )

First ThirdSecond

StabilityStability spectra and spectra and temperature during mappingtemperature during mapping

18/02/2002-18/04/20022 month

10/09/2002-10/11/20022 month

01/04/2003-01/06/20032 month

2001 Mars Odysseypage 13

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

LD MD

Stilbene CsI(Tl)

Stability Stability spectra spectra duringduring mapping mapping

2001 Mars Odysseypage 14

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Stability Stability temperature temperature duringduring mapping mapping

-15 < tHEND < +15

First Second Third

• t1- temperature of main electronic board

• t2- temperature of HV board

• t3- temperature of stilbene electronic board

-15

+15

2001 Mars Odysseypage 15

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Calibration FacilityCalibration Facility

2001 Mars Odysseypage 16

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Source of neutronsFlux ~ 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 FacilityCalibration Facility

2001 Mars Odysseypage 17

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Pu-Be source: 3.8 MeV(29.6+/-0.2)/r2n cm-2 s-1

Cf source: 2.1 MeV(13.2+/-0.2)/r2n cm-2 s-1

Calibration FacilityCalibration Facility

2001 Mars Odysseypage 18

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Calibration measurements resultsCalibration measurements results

2001 Mars Odysseypage 19

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

10-1 100 101

0.0

0.2

0.4

0.6

SIMULATION FU-1 FU-2

Response Function of MD sensor

S, c

m2

E, MeV

Calibration measurements resultsCalibration measurements results

2001 Mars Odysseypage 20

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Simulation response functionSimulation response function

10-7 10-6 10-5 10-4 10-3 10-2 10-1 100 101 1020.01

0.1

1

Response function for LD sensor

S, c

m2

E, MeV

SIMULATION FOR HEND AS AN ASSEMBLY SIMULATION SINGLE DETECTOR

2001 Mars Odysseypage 21

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Response functions of LD, MD and SC/neutron sensors allow to fit data of #2, #3 and #4 periapses

with function of type E-

HEND energy rangeHEND energy range

2001 Mars Odysseypage 22

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

Model neutron

spectra on Mars orbit

Response function

of HEND sensors

Calculation

Model count of HEND neutron sensor

Real count of HEND neutron sensor

Calculation (Pearson criteria)

Probability of aligning

model

Using response functionUsing response function

2001 Mars Odysseypage 23

W o r k s h o p H E N D - 2003

Institute for Space Research, June 9 - 11, 2003

ConclusionConclusion: 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: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