Superconducting Magnet Development for me Conversion Experiments

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Presentation transcript:

Superconducting Magnet Development for me Conversion Experiments NuFACT 2012 July 23-28, 2012 Michael Lamm Fermilab

Outline Muon Conversion Experiments Magnet Elements Issues for Future Experiments Summary Thanks to Makoto Yoshida (KEK) for slides on COMET magnets Other slides from “Radiation Effects in Superconducting Magnet Materials” (RESMM’12) February 2012 see: https://indico.fnal.gov/conferenceDisplay.py?confId=4982

Muon Conversion Experiments m Ne- N experiments date back to the 1950’s, making incremental improvements on observation limits: Summary of “modern” experiments: Past (1990’s) 10-13 sensitivity SINDRUM II The Present (2010’s) 10-17 sensitivity COMET MU2e The Future (2020’s ?) ~10-19 sensitivity PRISM Project X-ERA at Fermilab

Magnetic Elements Modern muon-electron conversion experiments all work on a similar principle: 1) Generate large number of “stop-able” muons 2) A mono-energetic 104 MeV conversion electron is created from the coherent process: m Ne- N They utilizes three Basic Magnetic Elements: Capture Solenoid to collect pion and muon secondaries from primary target Large aperture, highest possible fields Heat and radiation from interaction secondaries Muon Transport Maximum transports efficiency Eliminate background Eliminate Line of Sight for neutral background Dispersion and collimation for momentum selection Avoid trapped particles. Keep muons “in time” Muon Stopping Target and Electron Spectrometer Efficient muon collection Electron Momentum measurement with minimal background

Example: Mu2e 8 meters 24 meters Transport Solenoid (TSu,TSd) Sign/momentum Selection Negative Axial Gradient in straight sections to suppress trapped particles Curved sections disperse beam by momenta Transport Solenoid (TSu,TSd) 8 GeV P Production Solenoid (PS) 8 GeV P hit target. Reflect and focus p/m’s into muon transport Strong Axial Gradient Solenoid Field Detector Solenoid (DS) Graded field to collect conv. e- Uniform field for e- Spectrometer 8 meters 24 meters

Example : COMET apparatus Pion Capture Solenoid Muon Transport Solenoid Spectrometer Detector proton beam pion production target radiation shield COMET Superconducting Magnet System A series of long solenoids from end to end pion capture & decay muon transport electron focus spectrometer detector

Mu2e Solenoids and Supporting Infrastructure Production Solenoid (PS) Transport Solenoid (TSu,TSd) Detector Solenoid (DS) Cryogenic Distribution Power Supply/Quench Protection Cryoplant Field Mapping Ancillary Equipment Installation and commissioning

Comet Magnet Design The magnet system is separated in 3 cryostats: proton beam Cryostat-1 target station LHe Transfer Tube outside Iron Yoke The magnet system is separated in 3 cryostats: Cryostat-1: CS+UpstreamTS Cryostat-2: DownstreamTS Cryostat-3: ST+SS+DS Concrete Cryostat-2 LHe Control Dewar experimental hall Cryostat-3 Purpose of separation: At concrete wall Different radiation control level Movable Cryostat-2 for install / maintenance Vac. separation window / antip absorber at mid. of TS Beam monitors At stopping target inject electron beam into ST Muon beam monitor

Mu2e Production Solenoid Concept 4.6T 2.5 T Axial Gradient Features: 1.6 m aperture, 4 m long Operating current ~9kA 3 coils “3-2-2” layers High strength aluminum stabilized NbTi superconductor (similar to ATLAS Central Solenoid) Aluminum outer support shells Thermal Siphon Cooling Mechanically supports Heat and Radiation Shield

Comet Capture Solenoid Layout Superconducting solenoid magnets with Al-stabilized conductor High field 5T to capture p- Large bore 1300mm High radiation env. Decreasing field to focus trapped pions Thick radiation shielding 450mm Proton beam injection 10°tilted Simple mandrel CS0 CS1 MS1 MS2 Length (mm) 175 1350 1800 380 Diameter (mm) 662 Layer 9 5 8 Thickness (mm) 144 80 128 Current density (A/mm2) 35 Maximum field (T) 5.7 4.0 3.9 Hoop stress (MPa) 59 51 30 proton beam 1300 950 1920 380 625 300 700 1000 360 t=100 Radiation shield Target Superconducting coils CS1 MS1 MS2 CS0

Mu2e Transport Solenoid TS1,TS3,TS5: Straight sections with axial gradient TS2/TS4: approximate toroidal field Accomplished by 52 solenoid rings of different amp-turns TS2 TS1 Two cryostats: TSu, TSd TS3:  TS3u, TS3d. Wider coils to compensate for gap Rotatable Collimator, P-bar window TS3 Coil fabrication similar to MRI coils TS4 TS5

Al-stabilized superconductor NbTi Rutherford cable with aluminum stabilizer “TRANSPARENT” to radiation Less nuclear heating Doped cold worked aluminum High RRR (>500) and High offset yield point at 4K > 85 MPa 30 mm x 5.5 mm COMET design value for Capture Solenoid Al/Cu/SC: 7.3/0.9/1 14 SC strands: 1.15mm dia. Mu2e design value for PS Al/Cu/SC: 6.0/0.9/1 36 SC strands: 1.30 mm dia.

Ongoing R&D PS demonstration coil at Toshiba US-Japan Collaboration PS demonstration coil at Toshiba 4-layer 8 turns using prototype cable Al-Al internal joint To be tested at Fermilab in 2013

Ongoing R&D Splice Tests Chemically removed Al stabilizer Part of the US Japan Collaboration Splice Tests Chemically removed Al stabilizer NbTi-NbTi splice joint

Radiation Studies at KUR M. Yoshida et al, ICMC2011 Radiation Studies at KUR Al-Cu-Mg Resistivity change with accumulated dose Fully recovered with room temp. anneal Mu2e will have to warm up ~1/year to repair aluminum stabilizer

Issues for Future Experiments Higher intensity muon beams will be required to increase limit sensitivity/discovery. More Demands on the Pion Capture Solenoid Higher intensity primary proton beams Increase capture efficiency with larger aperture, higher field higher field on superconductor Larger flux of secondaries higher heat load + high radiation on coil (superconductor, stabilizer and insulation)

HTS Needed for High Fields Peter Lee, FSU-NHMFL

Mu2e and Comet Capture Solenoids are near the limit in several areas Peak field on conductor is >5.5 T. Limited SC phase space especially since experiment demands large temperature and thermal margin for quench-free operation Near the limit of what is practical with NbTi Nb3Sn or HTS conductor is a possible upgrade path Brittle conductor Generally Nb3Sn solenoids are possible because of simpler mechanical forces, may not be true in this case. Radiation limits on stabilizer and insulation will demand more effective heat shield in bore of magnet Tungsten ($$$$) replaces copper Frequent room temperature anneals to repair stabilizer Consider radiation resistant epoxies (cyanide ester) HTS is purported to have good radiation qualities

Future Capture Solenoids may resemble muon collider concepts Kirk McDonald RESMM’12 Present Target Concept Superconducting magnets Resistive magnets Proton beam and Mercury jet Be window Tungsten beads, He gas cooled Mercury collection pool With splash mitigator 5-T copper magnet insert; 15-T Nb3Sn coil + 5-T NbTi outsert. Desirable to replace the copper magnet by a 20-T HTC insert.

Summary The conceptual design for the Mu2e and COMET solenoids has been completed Both use indirectly cooled NbTi conductor stabilized with Aluminum Designs are appropriate for sensitivity goals Peak Fields and dynamic heating are near the limit of what can be practically achieved with NbTi. Future experiments will likely require magnets built with Nb3Sn, HTS and radiation hardened insulators.