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Balloon-borne experiment for deep sky survey of MeV gamma rays using an Electron-Tracking Compton Camera S. Komura , T. Tanimori, H. Kubo, A.Takada, S. Iwaki, Y. Matsuoka, S. Miyamoto, T. Mizumoto, Y. Mizumura, K. Nakamura, S. Nakamura, M. Oda,


  1. Balloon-borne experiment for deep sky survey of MeV gamma rays using an Electron-Tracking Compton Camera S. Komura , T. Tanimori, H. Kubo, A.Takada, S. Iwaki, Y. Matsuoka, S. Miyamoto, T. Mizumoto, Y. Mizumura, K. Nakamura, S. Nakamura, M. Oda, J. D. Parker, S. Sonoda, T. Takemura, D.Tomono (Kyoto Univ.) K. Miuchi (Kobe Univ.), T. Sawano (Kanazawa Univ.) , S. Kurosawa (Tohoku Univ.) S ub- M eV gamma-ray I maging L oaded-on-balloon E xperiment SMILE-I gas-TPC Now planning (Sep., 2006 ) SMILE-II (1 day flight) Crab Nebula, Cygnus X-1 SMILE-III (1 month flight) ・ more faint sources Pixel ・ polarization measurements Scintillators

  2. Contents 1. Status and problems in MeV gamma-ray astronomy 2. How to challenge by using ETCC 3. Current and near-future ETCC  Performances  Polarization measurement  Summary 34th ICRC Hague, 4 August 2015 2

  3. Status of MeV gamma-ray astronomy Fermi > 1 GeV map COMPTEL 1-30 MeV map ~30 objects/10 years ~3000 objects/4 years NASA/DOE/ Fermi LAT Collaboration V. Schönfelder+ (A&AS, 2000) F. Acero+ (ApJS, 2015) Interesting science ❏ Nucleosynthesis in SNR ❏ Particle acceleration in AGN ❏ Early universe probe with GRB etc. MeV gamma-ray region is unexplored frontier! 34th ICRC Hague, 4 August 2015 3

  4. Problems  Unclearness of Imaging COMPTEL did not measure direction of recoil electron. => Imaging by superposition of event circles wide-spread Point Spread Function (PSF) needs of optimization algorithm as like ML-EM  Huge backgrounds in space TOF between Radioactivation of detectors by cosmic rays two detectors BG rejection in COMPTEL was not sufficient. => ~ 1/3 of the expected sensitivity Reliable PSF and Powerful BG rejection are needed. G. Weidenspointner+ (A&A, 2001) 34th ICRC Hague, 4 August 2015 4

  5. Electron-Tracking Compton Camera (ETCC) By measuring electron tracks, ETCC overcome the problems ! gas-TPC  Well-defined PSF without ML-EM 3D-track & energy  Powerful BG rejection using dE/dx  No shield => Wide field of view ~ 6sr T.Tanimori et al., ApJ (2015) accepted, Pixel arXiv: 1507.03850 [astro-ph.IM] Scintillators position & energy Particle ID by dE/dx Conventional method Electron Tracking method SPD p + n Recoil electron 34th ICRC Hague, 4 August 2015 5

  6. Current and near-future performance SMILE-II Flight model Effective Area Effective Area SMILE-III TPC  40 cm-cubic  CF 4 gas @3atm Scinti.  3 R.L. scintillator Points: measured Points: measured SMILE-II Lines : simulated Lines : simulated Pressure [keV] vessel 1 m PSF: angle containing half of all photons SMILE-II, III 7-15º Gas Ar-based @1atm SPD 30-100º Gas volume 30 cm-cubic (energy dependence) 800 μm Track sampling Near future ~ 1º Scintillator GSO:Ce 1 Radiation length SPD < 10º Energy 10%@662 keV  more precise resolution (FWHM) track sampling Field of View ~ 6 sr 34th ICRC Hague, 4 August 2015 6

  7. Detection sensitivity (4.5 years) (5 years)  SMILE-II : Crab nebula > 5σ (middle latitude, @ 40 km, 4 hours)  SMILE-III : 10 times better sensitivity (polar region, @ 40 km, 1 month) ~10 celestial objects, extragalactic and galactic plane survey  Satellite : reach 1 mCrab sensitivity ( 50 cm-cubic ETCC x 4 ) 34th ICRC Hague, 4 August 2015 7

  8. as a Polarimeter linearly polarized γ -ray Asymmetric distribution of the scattered photons 1.5 = 𝑛𝑏𝑦−𝑛𝑗𝑜 Modulation max Counts [a.u.] Factor 𝑛𝑏𝑦+𝑛𝑗𝑜 1 ~ 0.6@200 keV, 0.5 min ~ 0.5@500 keV 0 -200 -100 0 100 200 (Geant4 simulation) Azimuthal angle Φ [deg] Minimum detectable polarization (MDP) Signal [cm -2 sec -1 ] Effective area [cm 2 ] S A Background [sec -1 ] B M Modulation Factor [%] T Observation time [sec] 𝐶 M 𝐸𝑄 ∝ 𝛤 ≫ 𝛣𝑇 Sensitivity is limited by the background rate. 𝐵𝑇  Powerful background rejection ETCC has a large advantage  Imaging with wide FOV ~ 6sr 34th ICRC Hague, 4 August 2015 8

  9. Beam test 2 Counts [a.u.] 0 deg. 1 Peak ~ 130 keV 0 -22.5 deg. 2 1 Counts [/sec/keV] 1 ~ 96% polarized 123-148 keV 0 10 -2 2 -45 deg. Al target ON Al target OFF 1 Subtracted 10 -4 0 0 50 100 150 200 250 2 -90 deg. Energy [keV] rotation Polarization 1 M  M ~ 0.6@130 keV [deg.] angle [deg.] 0 0.3 ± 1.3 0 0.57 -180 deg.  Polarization angle 2 -22 ± 1.0 -22.5 0.59 ≒ Rotation angle 1 -45 -44 ± 0.7 0.60 -90 ± 1.1 -90 0.57 Modulation Factor is consistent 0 -200 -100 0 100 200 -2.3 ± 1.1 -180 0.60 with the simulation results. Azimuthal angle [degree] 34th ICRC Hague, 4 August 2015 9

  10. Summary ETCC has the potential to overcome the problems in MeV band. ❏ Well-defined PSF without ML-EM ❏ Powerful background rejection by dE/dx  SMILE-II ETCC ~ 1 cm 2 @ 200 keV  detectable Crab nebula with > 5σ level (middle latitude, 4 hours at 40 km)  Future Plan: SMILE-III ETCC (~10 times better sensitivity)  ~ 10 celestial objects (polar region, 1 month at 40 km)  Polarization sensitivity : 3σ MDP Crab nebula ~ 15 %, Cyg X-1 ~ 20 % (half-day flight) GRBs ~ 6% for 10 -6 erg/cm 2 s (2-3 GRBs/month) ~ 20% for 10 -7 erg/cm 2 s (~10 GRBs/month)  Future Plan: SMILE-satellite (~ 1mCrab sensitivity in 10 6 sec) 34th ICRC Hague, 4 August 2015 10

  11. Thank you for your attention! Details are discussed in T.Tanimori+2015 accepted for publication in ApJ. [arXiv: 1507.03850] Report of polarization measurement will be submitted within the year. 34th ICRC Hague, 4 August 2015 11

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