shu zhang (on behalf of the hxmt team) institute of high energy physics, chinese academy of science...
TRANSCRIPT
Shu Zhang(on behalf of the HXMT team)
Institute of High Energy Physics, Chinese Academy of Science
The current status of HXMT and its calibrations
Satellite Facts:Weight: ~2800 kgOrbit: 550 km, 43°Attitude: 3-Axis Stabilized precision 0.1 °Lifetime: 4 yearsObservation modes: Scan and pointing
HXMT collaborationInstitute of High Energy Physics (PI institute, payloads, scientific operation)Chinese Academy of Space Technology (satellite platform)National Space Science Center, CAS (space environment monitor, mission operation)Tsinghua University (participation in payloads and scientific operation)
HE: NaI/CsI, 20-250 keV, 5000 cm2
Size : 1900×1650×1000 mm
ME:Si-PIN
,5-30 keV, 952 cm2
LE:SCD,1-15 keV, 384 cm
2
Star tracker
12/2012
12/2013 2015
We are here .
News of the mission & progress of payload
Launch date: end of 2015
The mechanical model of the satellite in dynamical environment tests
The electric model of HXMT’s payloads in testing.
The payloads before the vacuum thermal balance tests
Progress of the payload
6/23
2013 July 29- August 21,
ME&LE : Energy response, QE and their T
dependences
LE: PSF measurement, QE, linearity
Panter calibration
We calibrated the energy linearity, energy resolution, quantum efficiency of one Si-PIN detector in PANTER X-Ray Test-Facility from July 29 to August 21, 2013.
• Left is the energy linearity of ME detector at -6 .℃• Right is the slope of energy linearity in different temperature.
Facility for HE We have successfully finished (in 2013) a calibration facility for HE togather with China National Institute of Metrology. (10-150 keV)
X-ray machine
Double crystal monochromator
Background shielding box for the calibrated detector
Monoenergy peaks
Mono-energy fraction >90%
Monochromaticity <1%
Instrument Calibration We are building on IHEP campus the calibration facility for ME and LE. It will be finished in middle 2014. ( 1-30 keV)
Vacuum charmber
X tube DCM Vacuum tube
See details of calibration issues in the later talk, which will be handled in SGS the background, the calibration dataset and software.
Thank you for your attention!
4. Summary
Detectors LE: SCD, 384 cm2;ME : Si-PIN, 950 cm2
HE : NaI/CsI, 5000 cm2
Energy Range LE: 1-15 keV;ME: 5-30 keV;HE: 20-250 keV
Time Resolution HE: 25μs; ME: 180μs;LE: 1ms
Working Temperature
HE: 18±1 ; ME: -50~-20 ; LE: -80-45℃ ℃ ℃
Energy Resolution LE: 2.5% @ 6 keV ME: 14% @ 17.8 keV HE: 19% @ 60 keV
Field of View of one module
LE: 6°×1.6°; 6°×4°; 60°×3°; blind;ME: 4°×1°; 4°×4°; blind;HE: 5.7°×1.1°; 5.7°×5.7° ; blind
Source Location <1' (20σ source)
Characteristics of the HXMT Mission
prototype for observation program draw up HXMT mission movement trajectory Observation visibility study
Monitoring of payload working status
The detailed design of the scientific ground segments and the software requirements have been finished. We are writing the codes of the softwares, which will be finished in the first season of the next year.
Observation Schedule
3. Project status and schedule
Orbit Altitude: ~550 km ; Inclination: ~43°
Attitude Three-axis stabilizedControl precision: ±0.1°Measurement accuracy: ±0.01°
Data Rate LE: 3 Mbps; ME: 3 Mbps; HE: 300 kbps
Payload Mass ~1000 kg
Nominal Lifetime 4 years
Working Mode Scan survey, small region scan, pointed observation
Total background of HE varying with time
Different background components of HE
Background components of ME Background components of LE
Simulation of the in-orbit background of HXMT
Test the performance of the automatic gain control by changing the angle between the main detector and the geomagnetic field.
With out the gain control , the amplitude variation of the same energy incident photons can reach 10.6% , and it decreased to 0.243% using the AGC, the effect on the energy resolution is as small as 1.31%。
Automatic Gain Control
The sensitivities of the three telescopes of HXMT. The sensitivities of NuSTAR, INTEGRAL/IBIS and RXTE/HEXTE were reprinted from Koglin et al. (2005)3.
2. Introduction to the payloads
HXMT/LE
HXMT/ME
HXMT/HENuSTAR
INTEGRAL/IBIS
RXTE/HEXTE
25
2. Introduction to the payloads
HXMT RXTE INTEGRAL/IBIS SWIFT NuSTAR
Energy Band (keV)
LE: 0.8-15ME: 5-30HE: 15-250
PCA: 2-60HEXTE: 15-250
15-10000 XRT: 0.5-10BAT: 10-150
3-79
Detection Area (cm2)
LE: 384ME: 950HE: 5000
PCA: 6000 HEXTE: 1600
2600 XRT: 110BAT: 5200
847 @ 9 keV60 @ 78 keV
Energy Resolution (eV)
150@ 6 keV2500@ 20 keV10000@60 keV
1200@6keV10000@60 keV
8000@ 100 keV
150 @ 6 keV3300 @ 60 keV
900 @ 60 keV
Time Resolution (ms)
LE: 1ME: 0.18HE: 0.012
PCA: 0.001HEXTE: 0.006
0.06 XRT: 0.14, 2.2,2500 BAT: 0.1
0.1
Sensitivity (@100keV, 3σ ,105s, mCrab)
0.5 1.5 3.8 9 0.03 @ 20 keV
Comparison between HXMT and other major hard X-ray telescopes