??????? ??????????? ????? HELLAS-SAT - PowerPoint PPT Presentation

About This Presentation
Title:

??????? ??????????? ????? HELLAS-SAT

Description:

Title: HELLAS-SAT Author: Ryzhkov Last modified by: Created Date – PowerPoint PPT presentation

Number of Views:29
Avg rating:3.0/5.0
Slides: 20
Provided by: Ryzh
Category:
Tags: hellas | sat | galactic | halo

less

Transcript and Presenter's Notes

Title: ??????? ??????????? ????? HELLAS-SAT


1
Spectrum-Roentgen-Gammaastrophysical
project, current status
Mikhail Pavlinsky (IKI, Moscow) on behalf of SRG
team
X-RAY Astronomy 2009, Bologna, 11 September, 2009
2
News August 18, 2009, Roscosmos (Russia) and
DLR (Germany) signed an Agreement On cooperation
in the framework of Spectrum-Roentgen-Gamma
orbital astrophysical project
3
  • Roscosmos, Russia
  • Space Research Institute, IKI, Moscow, Russia
  • Lavochkin Association, Khimki, Russia
  • VNIIEF, Sarov, Russia
  • Max-Planck-Institute for Astrophysics, MPA,
    Garching, Germany
  • Istitut fur Astronomie und Astrophysik, Univ.
    Tubingen, Germany
  • Astrophysikalishes Institut Potsdam, Germany
  • University Erlangen-Nuernberg, Germany
  • Hamburg University, Germany
  • Max-Planck-Institute for Extraterrestrial
    Physics, MPE, Garching, Germany
  • DLR, Germany

4
  • S/C to be launched in 2012 from Baikonur
  • Rocket Soyuz-2/1b buster Fregat, with gravity
    manoeuvre around the Moon
  • Halo-orbit around L2
  • Platform Navigator (Lavochkin Association)
  • S/C total mass 2200 kg
  • Payload - 1110 kg, 800 W
  • eROSITA (MPE, DLR, Germany), X-ray mirror
    telescopes, 0.5-10 keV
  • ART-XC (IKI VNIIEF, Roscosmos, Russia), X-ray
    mirror telescopes, 6-30 keV
  • Life time - 7 years

5
June, 2008
2009
6
Navigator
S/C dry mass 900 kg S/C propellant up to 300
kg PL mass 2000 kg PL power 1500 W (HEO) PL
power 600 W (LEO) Pointing 2? Stabilization
5? Stabilization rate 0.36?/s Reappointing
rate 0.25?/s Life time 7 years
On-board control system, radio system and TMS
equipment
Flywheel engines
Body
Solar panels drive mechanism
Tank
Solar panels
Propulsion system
Radiator
7
(No Transcript)
8
Observing strategy
  • The three months flight to L2, verification and
    calibration of payload
  • 4 years an all sky survey
  • 3 years on follow-up pointed observations of a
    selection of the most interesting galaxy clusters
    and AGNs.

9
eROSITA _at_ ART-XC on-axis effective area and grasp
2500 cm2 _at_ 1.4 keV 510 cm2 _at_ 7 keV
1100 cm2?deg2 _at_ 1.4 keV 45 cm2?deg2 _at_ 7 keV
10
The scientific goals of the SRG/eROSITA all-sky
survey
  • The study of the large-scale structure of the
    Universe ? with 100 000 galaxy clusters
  • The exploration of the growth and cosmological
    evolution of supermassive Black holes in the
    Universe ? with sample ?3 million AGNs
  • ?3.5?1014 M? (T?4.5 keV) up to z2
  • ?2.3?1014 M? (T?3.5 keV) up to z1
  • ?1014 M? (T ?2 keV) up to z0.4

11
and with ART-XC complementary instrument
  • All-sky survey at 6 ? 11 keV energy band with
    sensitivity
    ?3 ? 10-13 erg s-1 cm-2 keV-1 ? discovery at
    local Universe several thousands new AGNs
  • Study of massive nearby galaxies clusters with T
    ? 5 keV in the pointing observation mode
  • Study of intrinsically heavily absorbed/Compton
    thick AGNs ( NH ?
    3 ? 1023 ??-2)
  • Survey of galactic black holes and neutron stars
    with low luminosity
  • Study heavily obscured galactic X-ray binary
    systems
  • Study broad band spectra of Galactic objects
    (including binary systems, anomalous pulsars,
    SNRs) up to 30 keV, spectroscopy and timing of
    point sources
  • Study of cyclotron lines features of X-ray
    pulsars with energy resolution 1.5 keV up to 30
    keV

11
12
????????? ?????? ????? ???? eROSITA
Survey
13
eROSITA (MPE, DLR)
  • Number of mirror systems 7
  • Number of nested mirror shells 54
  • FOV 1?
  • On-axis angular resolution 15? (1 keV)
  • Energy range 0.2 12 keV
  • Diameter of 1 mirror system 358 mm
  • Form of shell Wolter-1
  • Focal length 1600 mm
  • Material of mirror shells Nickel
  • Mirror coating Gold
  • Total weight 760 kg
  • Power consumption 405 W

14
eROSITA (MPE, DLR)
  • Detector principle pn-CCD, Si
  • Size 28.8?28.8 mm2
  • Energy resolution 130 eV _at_ 6 keV
  • Pixels 384?384
  • Pixel size 75?75 µm2
  • Circle time 50 msec
  • Working temperature ? 80? C

14
15
ART-XC (IKI, VNIIEF, Roscosmos)
  • Number of mirror systems 7
  • Number of nested mirror shells 28
  • FOV ?32?
  • On-axis angular resolution ?1?
  • Energy range 6 30 keV
  • Diameter of mirror system 148 mm
  • Form of shell cone-cone
  • Length of shell 580 mm
  • Focal length 2700 mm
  • Material of mirror shells Nickel
  • Mirror coating Iridium
  • Total weight 350 kg
  • Power consumption 300 W

15
16
ART-XC, detector
Am241
  • Number of detectors 7
  • Detector principle DSSD CdTe
  • CdTe manufacturer ACRORAD
  • Size 25.6?25.6 mm2
  • Thickness 1 mm
  • Number of strips 64?64
  • Strip pitch 0.4 mm
  • Energy resolution ?10 _at_ 14 keV
  • Time resolution 1 ms
  • Working temperature ? 40? ? ? 35? C
  • Entrance window 100 ?m, Be
  • ASIC VA64TA
  • Background 10-2 cnt s-1 cm-2 keV-1

Prototype with 32 pixels
16
17
ART-XC
17
18
ART-XC
Exposition time map for ½ year all-sky survey.
The rotational axis is directed on Sun constantly.
The minimal 4-year exposition is ?1900 sec deg-2.
The survey poles position are coincide with
ecliptic poles. The total size of 2 zones with
exposition larger than 8000 sec deg-2 (near the
survey poles) is ?1260 deg2.
18
19
ART-XC
19
Write a Comment
User Comments (0)
About PowerShow.com