4
33 RD I NTERNATIONAL COSMIC RAY CONFERENCE,RIO DE JANEIRO 2013 THE ASTROPARTICLE PHYSICS CONFERENCE Super-TIGER 2012/2013 In-flight Instrument Performance and Preliminary Results M. SASAKI 1,6 , W. R. BINNS 2 , R. G. BOSE 2 , D. L. BRAUN 2 , T. J. BRANDT 1 , W. M. DANIELS 1 , G. A. DE NOLFO 1 , P. F. DOWKONTT 2 , S. P. FITZSIMMONS 1 , D. J. HAHNE 1 , T. HAMS 1,6 , M. H. ISRAEL 2 , J. KLEMIC 3 , A. W. LABRADOR 3 , J. T. LINK 1,6 , R. A. MEWALDT 3 , J. W. MITCHELL 1 , P. MOORE 2 , R. P. MURPHY 2 , M. A. OLEVITCH 2 , B. F. RAUCH 2 , K. SAKAI 1,6 , F. SAN SEBASTIAN 1 , G. E. SIMBURGER 2 , E. C. STONE 3 , C. J. WADDINGTON 4 , J. E. WARD 2 , M. E. WIEDENBECK 5 1 NASA/Goddard Space Flight Center, Greenbelt, MD 20771, USA 2 Washington University, St. Louis, MO 63130, USA 3 California Institute of Technology, Pasadena, CA 91125, USA 4 University of Minnesota, Minneapolis, MN 55455, USA 5 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 6 Center for Research and Exploration in Space Science and Technology (CRESST), Greenbelt, MD [email protected] Abstract: The Super Trans-Iron Galactic Element Recorder (Super-TIGER) is a large area instrument designed to measure the abundances of elements in the interval 30 Z 40 with an unprecedented combination of individual element resolution and statistical precision and to extend exploratory measurements up through Z=56. Super- TIGER consists of two identical modules, each comprised of scintillating fiber hodoscopes, three scintillator counters, an acrylic Cherenkov counter and an aerogel Cherenkov counter. The hodoscope determines the trajectory of incident particles. The scintillators and Cherenkov counters determine the particle charge and energy. Super- TIGER was launched on December 8th, 2013 from Williams Field near McMurdo Station in Antarctica, and flew for 55 days. More than 67 million cosmic ray events were sent to the ground through the Tracking and Data Relay Satellite System (TDRSS). Initial data processing and calibration are on-going. The charge resolution of the instrument is evaluated after gain correction of PMTs and area mapping corrections. Preliminary instrument performance and charge resolution results are reported here. Keywords: Super-TIGER, Ultra Heavy Cosmic rays, Balloon. 1 Introduction Super-TIGER is a large-area instrument designed to make precision measurements of the elemental composition of ultra-heavy cosmic rays (UHCR) with atomic number Z 30, built on the heritage of the Trans-Iron Galactic El- ement Recorder (TIGER), successfully flown on two bal- loons launched in Antarctica in December of 2001 and 2003 [1]. The principal objective of the Super-TIGER program is to measure the abundances of nuclei with 30 Z 42 with clear individual element resolution and high statistical precision. A secondary objective is to accurately measure the energy spectra of the more abundant light elements with 12 Z 28. The abundance measurements provide sensi- tive tests and clarification of the OB-association model of galactic cosmic-ray origins, and will test models for atomic processes by which nuclei are selected for acceleration to cosmic ray energies. Details of these are discussed in [2]. 2 Super-TIGER Instrument Fig.1 shows the Super-TIGER instrument. Super-TIGER consists of two identical modules, each comprised of scintillating fiber hodoscopes, three scintillator counters, an acrylic Cherenkov counter and an aerogel Cherenkov counter. The hodoscope determines the trajectory of inci- dent particles. The scintillators and Cherenkov counters determine the particle charge and energy. Details of each detector are descried below. Figure 1: The Super-TIGER instrument. 2.1 Hodoscopes Fig.2 shows the photo of the Hodoscopes without the light shield. The Hodoscopes use a coded readout scheme originally developed for TIGER to limit the number of PMTs needed. Each hodoscope plane uses two orthogonal

Super-TIGER 2012/2013 In-flight Instrument Performance and ...€¦ · 5 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 6 Center for Research

  • Upload
    others

  • View
    0

  • Download
    0

Embed Size (px)

Citation preview

Page 1: Super-TIGER 2012/2013 In-flight Instrument Performance and ...€¦ · 5 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 6 Center for Research

33RD INTERNATIONAL COSMIC RAY CONFERENCE, RIO DE JANEIRO 2013THE ASTROPARTICLE PHYSICS CONFERENCE

Super-TIGER 2012/2013 In-flight Instrument Performance and PreliminaryResultsM. SASAKI1,6, W. R. BINNS2 , R. G. BOSE2 , D. L. BRAUN2, T. J. BRANDT1, W. M. DANIELS1,G. A. DE NOLFO1 , P. F. DOWKONTT2 , S. P. FITZSIMMONS1 , D. J. HAHNE1 , T. HAMS1,6 , M. H. ISRAEL2 ,J. KLEMIC3, A. W. LABRADOR3 , J. T. LINK1,6, R. A. MEWALDT3, J. W. MITCHELL1 , P. MOORE2,R. P. MURPHY2, M. A. OLEVITCH2, B. F. RAUCH2, K. SAKAI1,6, F. SAN SEBASTIAN1,G. E. SIMBURGER2 , E. C. STONE3 , C. J. WADDINGTON4, J. E. WARD2, M. E. WIEDENBECK5

1 NASA/Goddard Space Flight Center, Greenbelt, MD 20771, USA2 Washington University, St. Louis, MO 63130, USA3 California Institute of Technology, Pasadena, CA 91125, USA4 University of Minnesota, Minneapolis, MN 55455, USA5 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA6 Center for Research and Exploration in Space Science and Technology (CRESST), Greenbelt, MD

[email protected]

Abstract: The Super Trans-Iron Galactic Element Recorder (Super-TIGER) is a large area instrument designed tomeasure the abundances of elements in the interval 30 ≤ Z ≤ 40 with an unprecedented combination of individualelement resolution and statistical precision and to extend exploratory measurements up through Z=56. Super-TIGER consists of two identical modules, each comprised of scintillating fiber hodoscopes, three scintillatorcounters, an acrylic Cherenkov counter and an aerogel Cherenkov counter. The hodoscope determines the trajectoryof incident particles. The scintillators and Cherenkov counters determine the particle charge and energy. Super-TIGER was launched on December 8th, 2013 from Williams Field near McMurdo Station in Antarctica, andflew for 55 days. More than 67 million cosmic ray events were sent to the ground through the Tracking and DataRelay Satellite System (TDRSS). Initial data processing and calibration are on-going. The charge resolution ofthe instrument is evaluated after gain correction of PMTs and area mapping corrections. Preliminary instrumentperformance and charge resolution results are reported here.

Keywords: Super-TIGER, Ultra Heavy Cosmic rays, Balloon.

1 IntroductionSuper-TIGER is a large-area instrument designed to makeprecision measurements of the elemental composition ofultra-heavy cosmic rays (UHCR) with atomic number Z≥ 30, built on the heritage of the Trans-Iron Galactic El-ement Recorder (TIGER), successfully flown on two bal-loons launched in Antarctica in December of 2001 and 2003[1]. The principal objective of the Super-TIGER programis to measure the abundances of nuclei with 30 ≤ Z ≤42with clear individual element resolution and high statisticalprecision. A secondary objective is to accurately measurethe energy spectra of the more abundant light elements with12 ≤ Z ≤ 28. The abundance measurements provide sensi-tive tests and clarification of the OB-association model ofgalactic cosmic-ray origins, and will test models for atomicprocesses by which nuclei are selected for acceleration tocosmic ray energies. Details of these are discussed in [2].

2 Super-TIGER InstrumentFig.1 shows the Super-TIGER instrument. Super-TIGERconsists of two identical modules, each comprised ofscintillating fiber hodoscopes, three scintillator counters,an acrylic Cherenkov counter and an aerogel Cherenkovcounter. The hodoscope determines the trajectory of inci-dent particles. The scintillators and Cherenkov countersdetermine the particle charge and energy. Details of each

detector are descried below.

Figure 1: The Super-TIGER instrument.

2.1 HodoscopesFig.2 shows the photo of the Hodoscopes without thelight shield. The Hodoscopes use a coded readout schemeoriginally developed for TIGER to limit the number ofPMTs needed. Each hodoscope plane uses two orthogonal

Page 2: Super-TIGER 2012/2013 In-flight Instrument Performance and ...€¦ · 5 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 6 Center for Research

Super-TIGER Instrument Performance33RD INTERNATIONAL COSMIC RAY CONFERENCE, RIO DE JANEIRO 2013

layers of square scintillating fibers covering a fiducial areaof 2.4m×1.16m. Long-axis fibers are 1.4 mm square whileshort fibers are 1 mm. The fibers are formatted into tabsof 6 (long) or 8 (short) fibers, so segmentation is 8 mm.Groups of 12 adjacent tabs at one end of each layer areviewed by a single Hammamatsu R1924A PMT to givecoarse spatial resolution. The tabs on the opposite endsof the fibers are sequentially routed to PMTs so each tabwithin a coarse group is viewed by a different PMT. Thisacts as a vernier for single-tab localization. A good eventhas a hit at both coarse and fine ends, so the uncertaintyin position is σrms = 8mm/

√12 = 2.3mm. Averaged over

the effective opening angle of the instrument, for Z=40 theresulting uncertainty in the secant correction contributesonly σtra j=0.003 c.u. to σZ . The PMT signals are pulse-height analyzed so that large signals from heavy nuclei canbe readily distinguished from knock-on electrons. [3]

Figure 2: Photo of the Hodoscopes without the light shield.

2.2 Scintillation DetectorsFig.3 shows the photo of the half-module Scintillation De-tector without the aluminized myler. Each half-module Scin-tillation Detector uses a sheet of 1.16 m x 1.16 m x 1 cmELJEN Technology EJ-208B plastic scintillator. The scin-tillation light produced is carried to the edges of the sheetby total internal reflection and is coupled through a thin airgap to four EJ-280 wavelength-shifter (WLS) bars aroundits perimeter. Each WLS bar is read out by HamamatsuR1924A 2.54 cm diameter PMTs coupled to both ends us-ing optical epoxy. Two such detector units were used ineach module layer to provide both dE/dx measurements andthe event trigger. The scintillators were the largest sheetsthat could be produced with the required uniformity. TheScintillation Detector enclosures were floored with an ultra-low density Al-foam composite developed at GSFC. ThisAl-foam composite was also used to support the hodoscopesand as floors for the Cherenkov enclosures. The tops of bothScintillation Detector and Cherenkov Detector enclosureswere 0.1 mm hard Al foil. Overall the use of the foil andAl/foam composites reduced interactions by ∼20% com-pared to the materials used in TIGER. The scintillatorssit on thin layers of Depron foam. Sheets of highly reflec-tive aluminized mylar above and below the scintillators de-

couple the internal reflection surfaces from the foam andimprove light collection and uniformity. The PMT basesused radically tapered voltage dividers providing nearly lin-ear response to 2×105 photoelectrons (p.e.) and an effec-tive dynamic range of 2× 104 to cover the charge range10≤ Z ≤ 56 including the variations in light reaching eachPMT due to particle incident position and angle. The basesincorporated charge-sensitive preamplifiers (CSA) to elimi-nate pick-up noise that might reduce the resolution of themeasurement. The PMTs were wrapped with a single 0.1mm thick layer of mu-metal foil to cancel the varying ef-fects of the Earth’s magnetic field with instrument locationand orientation. [4]

Figure 3: Photo of the Scintillation Detectors without thealuminized mylar.

2.3 Cherenkov DetectorsThe Cherenkov Detectors for Super-TIGER were basedon the extensive experience of the collaboration with theIMAX, ISOMAX, TIGER, BESS, HEAO-3 and BESS-Polar silica-aerogel and acrylic Cherenkov Detector. Lightintegration volumes lined with highly reflective GORE DRPLight-Reflective Material of 0.25 mm thickness collectingthe Cherenkov light produced by the silica-aerogel (C0)and acrylic (C1) radiators. Each optical volume has anaperture of 118 cm x 240 cm and is 20 cm tall. Theenclosures are divided into two half-module structures forrecovery, but these are open at one end and so create aunified optical system. Each detector is read out by 4212.7 cm Hamamatsu R877-100 PMTs with Super-Bialkaliphotocathodes for high quantum efficiency. Fig.3 shows thephoto of the C0 module. Each C0 module contains eightaerogel blocks, each approximately 55 cm x 55 cm and 3cmtall. Three of the four half-modules contain aerogel blockswith n = 1.043 (12 blocks total), while one half-modulecontains four blocks of index 1.025. These have thresholdsof 2.5 GeV/nucleon and 3.3 GeV/nucleon, respectively.The aerogel blocks are mounted on thin composite palletscovered in GORE DRP and are held in position by a layerof polyethylene terephthalate, similar to Saran wrap, using atechnique adapted from BESS/BESS-Polar. C1 uses acrylicradiators with bis-MSB wavelength shifter added that werecast for Super-TIGER by Polycast. This material has anindex of refraction of 1.49, corresponding to a threshold of0.3 GeV/nucleon. In each module the radiator consists oftwo 1.16 m x 1.16 m sheets meeting near the midline of the

Page 3: Super-TIGER 2012/2013 In-flight Instrument Performance and ...€¦ · 5 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 6 Center for Research

Super-TIGER Instrument Performance33RD INTERNATIONAL COSMIC RAY CONFERENCE, RIO DE JANEIRO 2013

detector. The Cherenkov Detector PMTs were mounted incustom hydroformed 0.3 mm thick mu-metal sleeves thatserved as magnetic shields, mechanical support and lightclose-out. Their bases used voltage dividers that were evenmore radically tapered than those for the scintillators andcould measure from 10 to ∼ 2×105 pe (dynamic range of2× 104) with only 2% non-linearity in order to span the10 ≤ Z ≤ 56 range. As with the scintillators, the voltagedividers incorporated integrated CSAs.[5]

Figure 4: Photo of the Aerogel Cherenkov Detector withthe top lid off.

3 Flight ConditionSuper-TIGER was launched on Dec. 8, 2012 (UTC), fromWilliams Field, Antarctica. In about 2.7 circumnavigationsof Antarctica, it flew for over 55 days at altitudes from about35.2 km to 39.7 km (Fig. 5). The flight was terminated onFeb. 1, 2013 due to concerns about increasing instabilityin the high-altitude winds and safety margins in a CSBFballoon termination battery which was rated for 60 dayswith 10% margin. Termination was carried out over-the-horizon at a location on the West Antarctic Ice Sheet (WAIS)with 82◦14′44.40′′ South latitude and 81◦54′40.80′′ Westlongitude, 1625 km from McMurdo and 600 km from thenearest long-term US camp (WAIS Divide). As a result ofthe flight termination occurring very late in the Antarcticseason, and long distance from McMurdo, we were not ableto recover this season or even get overflight photos of theinstrument. Recovery is planned for the 2013/2014 AustralSummer. The flight trajectory is shown in Fig. 6. The flightset duration records for heavy scientific payloads and forheavy-lift scientific balloons.

4 Instrument Performance and PreliminaryResults

The instrument returned excellent data on over 67× 106

cosmic-ray nuclei above the trigger threshold at ∼ Z ≥ 10.Nearly all high-priority data (Z ≥ 22) could be sent throughTDRSS when satellite view angles supported transmissionrates as low as 20kbs. Large fractions of lower priority data(10 ≤ Z ≤ 22) were also returned. Overall, considering out-ages and very-low-rate periods, TDRSS data transmissionwas about 80% efficient, giving the equivalent of 44 days of

Figure 5: Flight altitude of the Super-TIGER. The floataltitude is from about 35.2 km to 39.7 km.

1d

ay

2day

3day

4day

5day

6day

7day

8d

ay

9d

ay

10day

11day

12day

13day

14day

15day

16d

ay

17d

ay

18day

19day

20day

21day

22day

23day

24day

25d

ay

26d

ay

27da

y

28day

29day

30day

31day 32day

33d

ay

34d

ay

35day

36day37d

ay

38d

ay

39day

40day

41day

42day

43day

44day

45day

46d

ay

47d

ay

48d

ay

49day

50day

51day

52day

53day

54day

Launch (Williams Field)

Super­TIGER55day: Landing

Figure 6: Flight trajectories of the Super-TIGER. Greenline indicated the first revolution, blue line indicated thesecond revolution, and red line indicated the third revolu-tion.

data recorded. All triggered events occurring during the twoLOS (line-of-sight) periods at the beginning of the flightand the end of the first orbit/beginning of the second, werereturned. Since we were not able to recover the instrumentthis season, our analysis has been performed only for theTDRSS data and LOS data at the moment. The healthinessof each packet in the telemetry data has been examined bythe checksum. We took pedestal data every 20 minutes dur-ing the flight and performed gain calibration by using Feevents about every 2 hours depends on the data transmis-sion rates. Particle charge is measured using both [dE/dxvs. CK] and [high-n-CK vs. low-n-CK] techniques. Anglesof incidence and instrument response maps are correctedusing particle trajectories measured by the hodoscopes. Theresponse maps were obtained by accumulating the all Feevents during the flight. For low-energy events, below thelow-index (n=1.043 and n=1.025) aerogel CK (C0) thresh-olds and extending slightly above the C0 threshold, the sumof two scintillator signals (ST=S1+S2), with a small ve-

Page 4: Super-TIGER 2012/2013 In-flight Instrument Performance and ...€¦ · 5 Jet Propulsion Laboratory, California Institute of Technology, Pasadena, CA 91109, USA 6 Center for Research

Super-TIGER Instrument Performance33RD INTERNATIONAL COSMIC RAY CONFERENCE, RIO DE JANEIRO 2013

locity correction from the high-index (n=1.49) acrylic CK(C1) signal, is used to determine Z. Our data are shown inFig.7 showing a scatter plot of S1 vs C1 in one module forevents with Z ≥ 10. The charge bands are clearly visible.The S3 signal helps identify and reject nuclei interacting inthe instrument but is not used in the primary charge mea-surement.

Figure 7: Cross-plots of Super-TIGER data for Scintillationcounter (S1) vs Acrylic Cherenkov (C1).

For high-energy events, above the C0 threshold, the C1signal, with a small correction from the C0 signal, is usedto measure charge. These data are shown in Fig.8 showinga scatter plot of C1 vs C0 in one module for events with Z≥ 10. Again, the charge bands are clearly visible. Althoughthe underlying measurement technique at low energies is[dE/dx vs CK], the use of organic scintillators means thatthe technique is actually [dL/dx vs CK] where L is thelight produced by particle energy loss in the scintillatormaterial. Although dE/dx ∝ Z2, L exhibits saturation effectsat high specific dE/dx, [6] the scintillator response becomesmore complicated. However, the Z resolution σZ ≤ 0.25needed to resolve the relatively rare odd-Z elements canstill be achieved by correcting the non-Z2 behavior of thescintillators for velocity and particle charge dependence.The [C1 vs C0] technique gives better charge resolution than[ST vs C1] because the CK signals have pure Z2 dependenceand do not suffer saturation effects.

The excellent performance of Super-TIGER is shownin Fig.9, which is a very preliminary charge histogram for10 ≤ Z ≤ 32 events for the low- and high-energy branchessummed, using the maps and gain corrections developedfrom in-flight analysis. The high-priority data are drawnwith blue line and all data are drawn with black line in thefigure. We note the clear peaks at 30Zn and 32Ge. The chargeresolution at Fe is 0.22 at the momemt. The resolutionwill improve with development of detailed gain correctionsand response maps. We expect that odd-Z nuclei adjacentto high-abundance nuclei, such as 27Co and 29Cu, will beresolvable using these improved corrections and selectionof data, as they were in TIGER.

Figure 8: Cross-plots of Super-TIGER data for AcrylicCherenkov (C1) vs Aerogel Cherenkov (C0).

Charge10 12 14 16 18 20 22 24 26 28 30 32

Cou

nts

1

10

210

310

410

510

610

Prelim

inary

Peak : 25.99

Sigma : 0.22

All Events

High Priority Events

Figure 9: Histogram of combined lower- and upper-energybranches of selected data

Acknowledgment: The Super-TIGER program is supported byNASA. We wish to thank the Columbia Scientific Balloon Facility(CSBF) personnel and the Wallops Balloon Program Office (BPO)for their excellent efforts that resulted in our highly successfullong-duration balloon flight. We also wish to thank the NationalScience Foundation Office of Polar Programs for their outstandinglogistical support which made this investigation possible.

References[1] Rauch, B.F. et al., The Astrophysical Journal, Volume 697,

Issue 2, pp. 2083-2088 (2009) 2083-2088doi:10.1088/0004-637X/697/2/2083.

[2] Binns. W.R. et al., ICRC 2013 Proceedings (2013).[3] Ward. J.E. et al., ICRC 2013 Proceedings (2013).[4] Link. J.T. et al., ICRC 2013 Proceedings (2013).[5] Murphy. R.P. et al., ICRC 2013 Proceedings (2013).[6] Salamon, M.H. and Ahlen, S. P., Nucl. Inst. and Meth., 195,

pp. 557-568 (1982)