S. Aoki Kobe University OPERA Emulsion Workshop 2006/12/09 Gamma-ray Telescope
Photon Observation (pointing) Radio IR Visiblerefrectable optical imaging UV X-ray “MeV-γ”Compton scattering multi-Compton scattering “GeV-γ”pair creation initial e-track measurement “TeV-γ”air shower Čerenkov light imaging The best tracking detector becomes the best “GeV-γ” telescope.
2 mrad Current Situation in various wavelength range ex. Crab nebula (M1) Radio (VLA) Infra Red (2MASS) Visible (Palomar) Ultra Violet (UIT) X-ray (Chandra) “TeV” Gamma (HESS) “GeV” Gamma (EGRET) 30 mrad 100 mrad a lot of room to improve for “GeV-γ”
Converter Emulsion metal foil spacer Energy Measure ( Em + Pb ) Fiber Tracker ( X and Y ) γ Emulsion hybrid Gamma-ray Telescope Unit size is about 1 m 2 according to EGRET, Crab = 43 ev / 6hour ・ m 2 (E > 1GeV) Loaded on the Scientific Balloon ($0.1M/flight << satelite) Fiber Tracker for the “time stamp” Orientation monitor (gyro + “star camera”) should also be equipped, to know the direction w.r.t celestial sphere.
Balloon Sanriku 2004/May/30 Micro Segment Chamber
1.5mm 10.5cm 6.5cm hadron j et electroron shower g amma shower Balloon Sanriku 2004/May/30
290µm (.002X 0 ) 2mrad by single layer (290µm) [rad] “OPERA Film” tracker performance In current method, angular resolution is dominated by “stage (z-axis) noise”.
SPring-8 Laser Electron Photon Beam (by RCNP Osaka Univ.) ~ 70m
Angular Resolution RMS x = 2.6 mrad RMS y = 1.8 mrad
290µm (.002X 0 ) “OPERA Film” tracker performance 2mrad by single layer (290µm) 50mm c.f. GLAST 410µm (.004X 0 ) 1 mrad
readout error 0.3 m 0.2 m 0.1 m GLAST 1 mrad simulation
Thicker Base
Intrinsic Tracking Resolution Ag grain after development dx = 0.06 m Compton Electron Fog M.I.P. Track 100 m M.I.P. Track intrinsic tracking accuracy Original Crystal Size0.2 m single grain resolution0.2 m/ 12 = 0.06 m N grains resolution0.06 / N m Angular Resolution (200 m base) 0.06/ N * 2 / 200 = 0.4/ N mrad if N=9 0.4/ N mrad = 0.13 mrad
Summary We are developing Emulsion Hybrid Gamma-ray Telescope Test with Laser Electron Photon Beam (Max. 2.4GeV) Finding conversion point is OK By current methods, RMS = 1.8~2.6 mrad (= 6~9 arc min) and Outlook We shall improve angular resolution. At first, 1 day flight at Sanriku Japan to detect Crab nebula. If Solar flare happens during flight, we can see the point. (Apparent diameter of the Sun = 0.5 = 9 mrad) Next, Long Duration (1 week) Flight at south hemisphere to see the Galaxy center and other objects.
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Emulsion can measure … brightness (magnitude) color (wavelength) direction of the light. event rate (flux) energy (momentum) direction of the “GeV” photon. Emulsion can be good Telescope. Telescope observes …
plate Cu 50 m Pb 500 m plate Cu 50 m Pb 500 m ConverterEnergy Measure Test Chamber PMMA 15mm t
Detection and Measurement of Gamma-ray Net-scan reconstruction Manual Check e-pair confirmation Angle measurement 10 mrad distribution in angular space 39 events form 5mm×5mm area
Energy Measurement E < “ 700 MeV ” (beam halo) E > “ 700 MeV ”
x 0.1 GeV 1 GeV 10 GeV Angular Resolution (simulation) 68% 95% 68% readout error 0.3 m
x 0.1 GeV 1 GeV 10 GeV Angular Resolution (simulation) 68% 95% 68% readout error 0.1 m
Signal to Background estimation According to EGRET (ApJ.494, p734, 1998), Crub Flux = 2.0 10 7 photons cm 2 sec 1 > 1.0GeV) During 24 hours flight, Crab is above the detector 6 hours with 45º aperture # of arriving photon is 43 photons with 1m 2 area. # of Signal event will be 21 ev. with 50% X 0 depth. According to BETS, atmospheric gamma-ray flux is 63 photons m 2 sec 1 sr 1 > 1.0GeV, 25g/cm 2 height) 1.3 10 3 photons cm 2 sec 1 sr 1 > 1.0GeV, 5g/cm 2 height) In the size of Crab nebula (1 1mrad 2 = 4.0 10 6 sr) 1.2 10 9 photons cm 2 sec 1 During 24 hours flight, # of arriving photon is 1.1 photons with 1m 2 area # of Backgound event will be 0.6 ev. with 50% X 0 depth.
“TeV” Gamma Observation by HESS (Imaging Air Cerenkov Telescope) PSF 1°× 1 ° Crab nebula (M1) Galactic Sources “morphology” has become possible “TeV” Gamma region
dE/dx measurement dE/dx (a.u.) p ( = 0.79, dE/dx = 1.23 MIP ) ( = 0.99, dE/dx = 1.08 MIP ) “OPERA film” KEK-PS 1.2 GeV/c beam (29 films)
momentum (p ) measurement by multiple Coulomb scattering MDM = 5.9 GeV/c with =0.21 m p (GeV/c) p (GeV/c) 1.2 GeV/c 4 GeV/c
Balloon Sanriku 2004/May/ m MSC (40cm 50cm 8X 0 ) “hinge” for shifter
flight path 503km the north latitude the east longitude
T= t 0 T=t 1 T=t 2 “shifter” to get time information MSC Air-Bag hinge
altitude [km] shifter displacement [0.1mm] level flight at 36km displacement by atmospheric pressure change air bag #1 air bag #3 air bag #2 (slow change) “boomerang” flight at 14km Flight Altitude vs. Displacement
expected track density vs. before launch FLUX=10 -2 cm2/sr/sec T=6.5day=5.6x10 5 sec W=0.5sr(<0.4rad) 2.8x10 3 /cm FLUX=2.1x10 -1 T=4hour =1.4x10 4 sec W= x10 3 /cm FLUX=4x10 -2 T=14hour=5.0x10 4 sec W= x10 3 /cm 2 projection
measured track density vs. displacement projection track displacement across the air-bag
measured vs. expected
@0km before launch