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Title: GammaRay Astrophysics


1
Gamma-Ray Astrophysics
  • Nicola Omodei
  • INFN Pisa

2
A brief history...
  • ... of the gamma-ray astronomy (in space...)
  • OSO-3 (1967-1969) 621 photons detected over 50
    MeV, first full sky survey.
  • SAS-2 (1972-1973) first detailed information on
    the gamma-ray sky, diffuse background few point
    sources.
  • COS-B (1975-1982) very successful mission,
    performance comparable with SAS-2.
  • EGRET (1991-1996) first detailed full sky
    survey, hundreds of point sources discovered.
  • GLAST - to be coming soon(er or later)!
  • Keep in mind...
  • CGRO (Compton Gamma Ray Observatory), including
    EGRET (Energetic Gamma Ray Experiment Telescope,
    10 MeV10 GeV) and BATSE (Burst And Transient
    Source Experiment, 10 keV10 MeV) onboard.
  • GLAST (Gamma Ray Large Area Space Telescope).

3
Outline
  • Introduction to gamma astrophysics
  • Experimental technique
  • Ground vs. space.
  • Gamma-ray astronomy in space.
  • The heritage of the previous missions.
  • The design of a gamma-ray telescope basic ideas.
  • GLAST design and performance.
  • Zoology of the gamma-ray sky (EGRET vs. GLAST!)
  • Point sources vs. diffuse background.
  • Active Galactic Nuclei.
  • Gamma Ray Bursts.
  • Pulsars

4
  • Part I

5
Introduzione ordini di grandezza
Il risultato delle interazioni che avvengono
all'interno dei lontani corpi celesti è
l'emissione di radiazione luminosa. Più un
fenomeno è violento maggiore è la quantità di
energia che viene rilasciata sotto forma di luce.
Il tipo di luce che viene emessa non è solo
visibile ma può avere energie anche molto
superiori. Lo studio della luce altamente
energetica (radiazione gamma) permette di avere
informazioni sui processi fisici che riguardano
oggetti molto energetici e molto lontani da noi.
Le grandezze studiate da questo ramo
dell'astrofisica arrivano fino a 1052 erg al
secondo ovvero potenze paragonabili a 1019 soli
(circa dieci miliardi di miliardi di soli), le
distanze sono dell'ordine dei milioni di anni
Luce (MLY) ovvero 1018 centimetri (un miliardo di
miliardi di centimetri).
6
Absorptions propagation
  • A photon produced in the deep universe may be
    absorbed by
  • Diffuse background (gamma-gamma interaction)
  • Earth Atmosphere (gamma-Nuclei interaction)
  • The photons point directly to the source!
  • They are not deviated by the Magnetic Fields
    (GMF)
  • Cosmic Rays (charged particles) are deviated by
    the magnetic fields and loose information on the
    production site.
  • High Energy Cosmic Rays (HECR) need strong
    acceleration processes.
  • The CR emission is related to emission of High
    Energy Gamma-Rays due to the Radiation-Matter
    Interaction (Synchrotron, Compton)
  • The only way to understand where CR are produced
    is to observe gamma-rays!

7
Diffuse background absorption
Pair production
Optical depth, tau gt 1 gt Opaque tau lt 1 gt
Transparent
Mannheim, Hartmann Funk, 1996
8
Atmospheric absorption
Transparent
Balloon-rockets satellites
Transparent
Balloon-rockets satellites
O2 O3
Oxygen and Nitrogen
H2O CO2 O3
9
The photon cross section
g
e-
g
e-
g
g
e-
e-
  • Energy lt 100 keVPhotoeletric effect gt X-Ray
    astronomy
  • Energy lt 10 MeV Compton Scattering gt Soft
    gamma-Ray astronomy
  • Energy gt 10 MeV Pair Production gt gamma-ray
    astronomy

10
Gamma-ray astronomy space based...
  • Detection technique
  • Pair conversion is the dominating interaction
    process for gamma-rays.
  • Electron/positron pair provides the information
    about the gamma direction.
  • Electron/positron pair provides a clear signature
    for background rejection.
  • Basic structure of a pair conversion telescope
  • Tracker/converter (detection planes high Z
    foils) photon conversion and reconstruction of
    the electron/positron tracks.
  • Calorimeter energy measurement.
  • Anti-coincidence shield backgound rejection
    (cosmic rays flux 104 higher than the gamma
    flux).

11
... and ground based
  • Detection technique
  • Ultra high energy gamma-rays interact with the
    atmosphere and generate showers.
  • Cherenkov light provides spectral and directional
    information.
  • Gamma and cosmic rays induced showers have
    different shapes high beckground rejection power.

12
Ground-based vs. Space-based
  • Ground-based detectors
  • Advantages
  • Huge effective area (10000 m2).
  • Excellent angular resolution (0.02).
  • Good energy resolution (10-15 ).
  • Wide energy range (50 GeV-100 TeV).
  • Disadvantages
  • Small field of view (few degrees). Pointing
    device.
  • Not sensitive below few tens of GeV (not enough
    Cherenkov light).
  • Short duty cycle (10)
  • Space-based detectors
  • Disadvantages
  • Small effective area (1 m2).
  • Not sensitive above few hundreds of GeV (lack of
    photons).
  • Advantages
  • Good angular resolution (0.1-1).
  • Good energy resolution (10-15 ).
  • Wide energy range (10 MeV-300 GeV).
  • Huge field of view (2.5 sr). Scanning device.
  • Long duty cycle (100)

Sometimes words have two meanings... (Led
Zeppelin, 1972)
13
Ground and space
  • Complementarity between ground and space
  • GLAST will match the sensitivity of the new
    generation of ground-based experiments.
  • Crucial for multi-wavelenght campaigns.
  • Overlap for the brighter sources
    cross-calibration of the absolute energy scale
    and alerts.

14
Instruments for space-based gamma-ray astronomy
  • SAS-2 (1972 - 1973)
  • Energy range 30 MeV 1GeV
  • Energy resolution 100
  • Peak effective area 100 cm2
  • Field of view 0.25 sr
  • EGRET (1991 - 1996)
  • Energy range 20 MeV 30GeV
  • Energy resolution 15
  • Peak effective area 1500 cm2
  • Field of view 0.5 sr

1970
1980
1990
2000
Time
  • COS-B (1975 - 1982)
  • Energy range 30 MeV 5GeV
  • Energy resolution 40
  • Effective area 70 cm2
  • Field of view 0.25 sr

Balloon flights, Small satellites ( 621 photons
above 50 MeV detected by OSO-3!)
15
Basic definitions the IRFs
  • The Instrument Response Function
  • Allow to evaluate the detector response (in terms
    of the measured quantities E and W) to a know
    flux F (function of the true quantities E and
    W).
  • Effective area Aeff.
  • Energy response DE.
  • Point Spread Function (PSF) angular resolution.
  • Usually NEEDED to go the other direction from
    the measured counting rate to the real flux!
  • Excellent knowledge of the IRF crucial for the
    overall normalization of the flux. The IRF depend
    not only on the instrument design, but also on
    the reconstruction algorithms!

16
Basic definitions the effective area
  • The effective area
  • Determines the REAL RATE of detecting a signal,
    given a source flux, after ALL detector,
    reconstruction and background rejection effects
  • It can be written as the product of geometric
    area, conversion probability, efficiency of the
    detector and of the reconstruction algorithms.

17
Basic definitions the FOV
  • The Field Of View
  • It is defined as the integral of the Effective
    area over the solid angle divided by the peak
    effective area.
  • If the angular response does NOT depend on the
    angle, the FOV is 4p (the whole sky).
  • In the case of a planar detector (Aeff(q)
    A0cosq), the FOV is p (1/4 of the sky).
  • The FOV basically depends on the Aspect Ratio of
    the instrument (height/width).

TKR
Low aspect ratio Large FOV
High aspect ratio Small FOV
TKR
CAL
CAL
18
Basic definitions the PSF
  • The Point Spread Function
  • It is the effective angular resolution after all
    detector, reconstruction and background rejection
    effect.
  • For a purely gaussian response, 2D 68
    containment angle is 1.41 times the 1D error and
    the 95 containment angle is 1.6 times the 68
    containment angle.
  • The response is typically NOT gaussian and the
    crucial parameter is the PSF95/PSF68.

19
Flown instruments SAS-2
  • Basic design
  • Tracking system based on spark chambers (upper
    set, interleaved with conversion foils, and lower
    set).
  • Triggered by external scintillators.
  • No calorimeter (energy information derived by the
    measurement of the multiple scattering).
  • Monolithic anticoincidence shield.
  • Last Solid State Recorder failed after 6 months
    of mission...
  • SAS-2 (1972 - 1973)
  • Energy range 30 MeV 1GeV
  • Energy resolution 100
  • Peak effective area 100 cm2
  • Field of view 0.25 sr

20
Flown instruments COS-B
  • Basic design
  • Tracking system based on spark chambers. Sensible
    degradation in performance after few years.
  • Triggered by external scintillators.
  • No calorimeter (energy information derived by the
    measurement of the multiple scattering).
  • Monolithic anticoincidence shield.
  • COS-B (1975 - 1982)
  • Energy range 30 MeV 5GeV
  • Energy resolution 40
  • Effective area 70 cm2
  • Field of view 0.25 sr

21
Flown instruments EGRET
  • Basic design
  • Tracking system based on spark chambers (upper
    set, interleaved with conversion foils, and lower
    set). 100 ms dead time per event.
  • Triggered by external scintillators. Time Of
    Flight (TOF) improve background rejection
    capabilities.
  • Monolithic calorimeter (8 radiation lenghts!).
  • Monolithic anticoincidence shield (high energy
    effective area drops down because of the self
    veto due to albedo electrons from the
    calorimeter).
  • EGRET (1991 - 1996)
  • Energy range 20 MeV 30GeV
  • Energy resolution 15
  • Peak effective area 1500 cm2
  • Field of view 0.5 sr

22
How should a conversion telescope look like?
  • Basic features
  • Large effective area (but remember the
    ground-based detectors..)
  • Large Field Of View.
  • Good angular resolution.
  • Good energy resolution over a wide energy range.
  • Short instrumental dead time (i.e. NO spark
    chambers).
  • No consumables (again NO spark chambers).
  • Operation in space requires
  • Modular, robust, redundant design.
  • Mass budget.
  • Power budget.

23
Overall design drivers
  • Mission divers
  • Allocated space on the launcher
  • Forces the maximum possible lateral dimension
    (and geometric area).
  • Power budget
  • Restricts the number of readout channels in the
    tracker (i.e. strip pitch, number of layers).
  • Mass budget
  • Basically bounds the total depth of the
    calorimeter.
  • Science drivers
  • Background rejection
  • Drives the ACD design.
  • Also impact on TKR/CAL design.
  • Effective area and PSF
  • Drive the converter thicknesses and layout.
  • PSF also drives sensor performance, layers
    spacing and overall tracker design
  • Energy range/resolution
  • Drive the thickness/design of the calorimeter.
  • Field of view
  • Basically sets the aspect ratio (width/height).

24
Design drivers the tracker
  • Tracker/converter design determines the PSF
  • Low energy PSF completely dominated by multiple
    scattering effects ( 1/E).
  • High energy PSF set by hit resolution/lever arm.
  • Converter foils layout/detectors design/layers
    spacing determine the rollover energy and the
    asymptotic value of the PSF _at_ high energy.
  • Complex trade off
  • Converter foils thickness detection efficiency
    vs. multiple scattering degrading the PSF _at_ low
    energy.
  • Spacing between conversion foils multiple
    scattering vs. aspect ratio.
  • Spacing between tracking planes high energy
    angular resolution (big lever arm) vs. aspect
    ratio.
  • Pitch of the readout hit resolution vs. number
    of channels (i.e. power consumption).

25
The GLAST design
  • Overall modular design
  • 4x4 array of identical towers - each one
    including a Tracker, a Calorimeter and an
    Electronics Module.
  • 3000 kg, 650 W.
  • Surrounded by an Anti-Coincidence shield.
  • Anti-Coincidence (ACD)
  • Segmented (89 tiles).
  • Self-veto _at_ high energy limited.
  • 0.9997 detection efficiency (overall).
  • Tracker/Converter (TKR)
  • Silicon strip detectors.
  • W conversion foils.
  • 80 m2 of silicon (total).
  • 106 electronics chans.
  • High precision tracking, small dead time.
  • Calorimeter (CAL)
  • 1536 CsI crystals.
  • 8.5 radiation lengths.
  • Hodoscopic.
  • Shower profile reconstruction (leakage
    correction)

Tower DAQ (TEM)
26
Trigger and onboard data processing
  • Level 1 trigger
  • Hardware trigger, single-tower level.
  • Three_in_a_row three consecutive tracker x-y
    planes in a row fired. Workhorse g trigger.
  • Cosmic rays in the L1T! 13 kHz peak rate.
  • Upon a L1T the LAT is read out within 20 ms.
  • On-board processing
  • Identify g candidates and reduce the data
    volume.
  • Full instrument information available to the
    on-board processor.
  • Use simple and robust quantities.
  • Hierarchical process (first make the simple
    selections requiring little CPU and data
    unpacking).

x
x
x
  • Level 3 trigger
  • Final L3T rate 30 Hz on average.
  • Expected average g rate few Hz
  • (g rate cosmic rays rate 1 few).
  • On-board science analysis (flares, bursts).
  • Data transfer to the spacecraft.

27
GLAST vs. EGRET
  • 1After background rejection.
  • 2Single photon, 68 containment, on axis.
  • 31s, on axis.
  • 41s radius, high latitude source with 10-7
    cm-2s-1 integral flux above 100 MeV.
  • 51 year sky survey, high latitude, above 100 MeV.

28
Tracker construction work flow
  • SSD procurement and testing
  • Ladders assembly
  • Towers assembly

18
10,368
342
2592
  • Trays assembly and test

648
  • Panels fabrication
  • Readout electronics fabrication, test and burn-in

29
Assembly of tower 0
30
Assembly of tower 0
31
Test of tower 0
32
  • Part II

33
The sky above 100 MeV
  • The heritage of EGRET
  • Diffuse extragalactic background ( 1.5x10-5
    cm-2s-1sr-1 integral flux).
  • Much larger (100 times) backgound on the
    galactic plane.
  • Few hundreds of point sources (both galactic and
    _at_ high latitude).
  • Essential characteristics variability in time.

34
The sky map EGRET vs. GLAST
  • 3rd EGRET catalog
  • 271 point sources, based on 5 years of data.
  • GLAST 1 year sky survey (simulated)
  • Thousands of sources will be discovered.
  • All EGRET sources detected in one day!
  • Detailed study of galactic and extragalactic
    background.

Integral Flux (Egt100 MeV) cm-2s-1
35
Unidentified sources I
  • What do we know about it?
  • 170 unidentified sources in the 3rd EGRET
    catalog.
  • No counterpart at other wavelenghts.
  • High Lg/Lradio, Lg/Loptical, Lg/Lx.
  • Some are variable, others are steady, both in the
    galactic plane and at high latitude.

Counting stats not included.
36
Unidentified sources II
  • What do we need?
  • Better angular resolution (smaller error bars).
  • Excellent spectral and timing capabilities to
    detect typical signatures (flares, spectral
    features, pulsation) and make the identification
    easier.

Cygnus region 15o x 15o, E gt 1 GeV
Counting stats not included.
GLAST and EGRET 95 containment regions
superimposed on a portion of the 1.4 GHz NRAO VLA
sky survey.
37
Diffuse background I
  • According to EGRET...
  • Apparently isotropic, extragalactic flux of
    gamma-rays (already discovered by SAS-2) above 30
    MeV.
  • Removal of point sources (impossible with COS-B
    and SAS-2 data) very difficult due to the large
    EGRET uncertainties.
  • What remains after the removal of point sources?
  • 1) Nothing the background is nothing but
    composite light of many faint sources. GLAST will
    surely resolve most of the diffuse background
    into point sources.
  • 2) Relic radiation from high energy processes in
    the early universe. Exciting perspectives for
    cosmology.

38
Diffuse background II
  • Removal of point sources galactic flux
  • Analysis conducted with EGRET data.
  • Contribution of point sources removed (difficult
    due to the large size of the Point Spread
    Function).
  • Contribution of galactic diffuse emission (mainly
    due to the interaction of cosmic rays with the
    interstellar nuclei and photons) also subtracted
    (difficult, as well).
  • The remaining flux...
  • Well described by a power law with spectral index
    a 2.1 0.3 over the EGRET energy range.
  • Apparently isotropic (but with large statistical
    uncertainties!) on a fairly large scale (30).
  • Spectral index compatible with the average
    spectral index of EGRET blazars.
  • Data somehow support the hypotesis 1), but still
    difficult to infer the fraction of diffuse
    background due to point sources.

39
Diffuse backgrund III
  • Particle decays in the early universe
  • Energy spectrum of this component should be
    different from the AGN contributions.
  • Statistically significant detection of this
    contribution impossible with EGRET.

40
Diffuse background IV
  • Possibility of lines from dark matter
    annihilation
  • Neutralino (c) is a good candidate for the dark
    matter of the universe.
  • LSP (Lightest Supersimmetric Particle) it is
    neutral and stable if R-parity is not violated.
  • Current viable models with Mc in the 30 GeV 10
    TeV range.
  • Possible scenario dark matter made of
    non-relativistic neutralinos gamma-ray lines in
    the
  • cc -gt gg (Eg Mc)
  • cc -gt gZ (Eg 1mZ2/4Mc2)

41
AGNs
  • Basic phenomenology
  • Vast amount of energy (1049 erg/s) emitted from a
    compact central volume.
  • Energetic, highly collimated, relativistic
    particles jets.
  • Significant fraction of the radiation emitted in
    the gamma-rays.
  • Blazars
  • Constitute most of the EGRET point sources.
  • Highly variable (hour timescale).
  • Strongly polarized (in the radio band!).
  • Prevailing idea
  • Accretion onto supermassive black holes.

42
Spectra
  • Add fv, vfv, e2 fv

43
Blazars
  • Blazars models
  • nFn spectra generally show two distinct
    components.
  • Low frequency (peaking between radio and x-rays)
    substantially polarized, believed to be
    synchrotron emission from high energy electrons.
  • BTW it would be interesting to perform
    polarimetry in the x/gamma rays!
  • High frequency peaking in the gamma-rays.

44
Blazar jets electrons vs. adrons
  • Leptonic models
  • High energy gamma-ray emission due to Compton
    scattering of soft photons on high energy
    electrons and positrons in the jet (ICS, Inverse
    Compton Scattering).
  • Where do the soft photons come from?
  • SSC (Synchrotron Self Compton) low energy g from
    synchrotron emission of the leptons themselves.
  • ECS (External Compton Scattering) photons from
    an accretion disk enter the jet directly.
  • Adronic models
  • If the jets include hadrons, they can interact
    with surrounding matter/radiation producing
    secondary pions and electrons.
  • e/e- and p can in turn initiate electromagnetic
    cascades through Compton scattering and
    synchrotron emission leading to emerging power
    law spectra.

45
Blazar jets
  • Things to do...
  • Evolution of synchrotron/gamma-ray components
    during flares can discriminate between models.
  • Need of time-resolved spectroscopy!

46
GRBs I
  • Basic phenomenology
  • Flashes of high energy photons in the sky
    (typical duration is few seconds).
  • Isotropic distribution in the sky (surprise from
    BATSE).
  • Cosmological origin accepted (furthest GRBs
    observed _at_ z5 billions of light-years).
  • Not repetitive, as far as we know. Never seen two
    GRBs from the same location (destructive
    phenomenon?).
  • Extremely energetic and short (the greatest
    amount of energy released in a short time after
    the big bang).
  • Sometimes x-rays and optical radiation observed
    after days/months (afterglows).

47
GRB observations
  • First detected...
  • ... in early 70 by military satellites.
  • Originally connected with Neutron Stars (NSs) in
    the Milky Way.
  • Interpreted as powerful but NOT spectacular
    flashes.
  • Then CGRO came...
  • EGRET (10 MeV-10 GeV) 1 burst per year.
  • BATSE (10 keV-10 MeV) 1 burst per day.
  • Distribution in the sky found to be isotropics.
  • Cosmological origin.
  • The afterglow era...
  • BeppoSax X-ray afterglows.
  • Keck optical afterglow.

48
GRBs distribution in the sky
  • No correlation with the galactic plane
  • Cosmological origin

49
GRBs timescale
  • Prompt emission
  • Burst duration 1-100 sec.
  • Bimodal distribution (IMPORTANT short bursts vs.
    long bursts).
  • Afterglow
  • Gamma-ray 1 hour.
  • X-rays 1 day.
  • Optical 1 month.
  • Radio...

50
Light curves
  • Variability
  • Timescales as short as few ms.
  • Shape of the light curves
  • Very various phenomenology.
  • One smooth peak.
  • One short spike.
  • Several peaks.
  • Intermittent activity.
  • NO PERIODICITY observed.

51
GRBs Power Density Spectra
  • PDS
  • Ligth curves very different, similar PDS (sample
    of 527 light curves of long bursts, T90 gt 100 s).
  • PDS are, with good approximation, power laws with
    a spectral index of -5/3.
  • Non trivial dependence of spectral index upon the
    energy bin.
  • GRBs can be interpreted as random short
    realizations of a standard process.

52
Energy dependence of light curves I
  • BATSE data in 4 energy bins
  • Harder pulses are shorter.

20-50 KeV
50-100 KeV
100-300 KeV
gt 300 KeV
53
Energy dependence of light curves II
WFWHM of ACF
Burst duration
  • Scaling law
  • General shape for the ACF.
  • WFWHM 3.2E-0.42.

54
High energy spectra
  • High energy behavior of GRBs
  • Still poorly known.
  • Need of more sensitive instrumentation!

55
GRB physics
  • The standard fireball model
  • Central engine emits shells of matter (e/e-)
    with Lorentz factors up to 1000.
  • Inelastic shocks between fast and slow shocks.
  • Particles acceleration on the shock front, Self
    Synchrotron production of high energy gamma-rays.
  • Afterglows interpreted as interaction with the
    interstellar medium (External Shock).

56
The central engine
  • The debate is still opened
  • Merging of compact objects (NS-NS, NS-BH, BH-BH).
    Observed within our galaxy.
  • Supernovae massive stars collapsing into
    spinning black holes. Identification with SN
    explosion observed at least in one case.

57
Pulsars
  • Phenomenology
  • First point sources detected in the gamma rays.
  • Extraordinary cosmic laboratories.
  • Extreme gravitational fields.
  • Extreme magnetic fields.
  • Pulsars studied in all the regions of the
    electromagnetic spectrum.

58
Polar Cap vs. Outer gap
59
Quantum Gravity
  • Lorentz invariance breaking
  • Considered within various theoretical frameworks.
  • In its simpler form
  • E2 m2 p2 f(p2, E, m Mp)
  • Mp is a mass scale (1019 GeV).
  • Photons propagating in vacuum may exibit a non
    trivial refractive index.

Easiest case NO intrinsic delay (
)
E1
E1
E2
E2
tti
ttf
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