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Helge Ravn CERN Muon week,

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Target and Pion Collection System and Support Facility. CERN Target and Horn working group ... Liquid at ambient temperature (no liquid-to-solid phase change issues) ... – PowerPoint PPT presentation

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Title: Helge Ravn CERN Muon week,


1
Target and Pion Collection System and Support
Facility
  • CERN Target and Horn working group

CERN 10 May 2001
Http//cern.ch/Helge.Ravn/files/Muon week Talk
2
The E951 Collaboration
CERN Target and Horn working group
A. AUTIN, A. BALL, A. BERNADON, L. BRUNO, A.
FABICH, G. GRAWER, S. GILHARDONI, T. KURTYKA, J.
LETTRY, J.-M. MAUGAIN, H. RAVN, M. SILARI, P.
SIEVERS, N.VASSILOUPOULOS, V. VLACHOUDIS, H.
VINCKE and F. VOELKER
3
CERN reference scenario
  • In order to produce 1021 neutrinos/year proton
    beams with a power of 1-4 MW needs to interact
    with a high Z target.
  • Proton energy 2.2 GeV.
  • Repetition rate 50 Hz
  • Pulse duration 3.3 ms.
  • Pulse intensity 1.5 1014/pulse
  • Average beam power 4 MW
  • Target absorbed power 1 MW
  • Liquid Hg-jet target Diam. 10 mm
  • Pion collection by means of a magnetic horn.

4
Heat load comparison
  • Radioactivity laboratory and support facility
    similar to.
  • EURISOL
  • RIA
  • ESS, SNS
  • Nuclear waste transmutation

5
Thermal expansion waves in ISOLDE targets
  • Splashes threshold (Pb, Sn and La targets 1993)
  • 1?1013 protons per pulse, 20 bunches (h5)
  • 0.5 ? 1012 protons per bunch (60ns, 1GeV)

ISOLDE target system
6
Thermal expansion wave and cavitation
7
Simulations
Surface evolution due to the interaction with
proton pulses
(R. Samulyak)
8
Why a Mercury-Jet
  • High pion yield (high Z)
  • High source brightness (high density)
  • Flowing liquid have excellent power handling
    capabilities
  • No water radiolysis
  • Liquid at ambient temperature (no liquid-to-solid
    phase change issues)
  • Minimal waste stream (compared to solid
    alternatives)
  • Passive removal of decay heating
  • No dominant long-lived radiotoxic products
  • No confinement tubing (free flowing jet)
  • No beam windows (differential pumping
    confinement)

9
Hg-jet system
  • Power absorbed in Hg-jet 1 MW
  • Operating pressure 100 Bar
  • Flow rate 2 t/m
  • Jet speed 30 m/s
  • Jet diameter 10 mm
  • Temperature- Inlet to target 30 C- Exit from
    target 100 C
  • Total Hg inventory 10 t
  • Pump power 50 kW

10
BNL CERN Trough test
  • Perpendicular velocities of Hg-drops via high
    speed cameras (8000 frame/s, 25ms aperture and up
    to 1000 kframe/s, 0.15ms aperture)
  • 0.5-4.0?1012 protons per bunch,
  • Bunch length 100 ns
  • Proton energy 26 GeV
  • Results (preliminary)
  • 6 to 75 m/s splashes measured (under atm.
    pressure)
  • Scales with the number of protons in the bunch
  • Questions
  • Response to a multi-bunch pulse (CERN scenario)
  • Response to a bunch length reduced to 3-5 ns
  • Response to other dE/dx

11
BNL E-951 trough test8 kHz camera
1st P-bunch 1.8?1012 ppb 150 ns
Vsplash 20-40 m/s
Timing 0.0, 0.5, 1.6, 3.4 ms, shutter 25 ms
12
BNL E-951 trough test 1MHz camera
Timing ms 0.0, 0.2, 0.4 0.6, 0.8, 1.0 shutter
150 ns
P-bunch 4.0?1012 ppb 150 ns
Vsplash 75 m/s
13
BNL Hg-jet chamber
  • P-bunch26 Gev,
  • spot size r1.6x0.8 mm (rms),
  • intensity lt4 1012 protons per bunch
  • bunch length 150 ns
  • Hg- jet diameter 1cm jet-velocity 3
    m/sprep. velocity 10 m/s

14
Jet test at BNL E-951 4 25th April 2001
Pictures timing ms 0.000 0.250 0.500 0.175 0.425
0.975 3.000
P-bunch 3.8?1012 ppb 100 ns to 0.45
ms Hg- jet diameter 1cm jet-velocity 3
m/s prep. velocity 10 m/s
15
Jet test at BNL E-951 1125th April 2001
Pictures timing ms 0.00 0.75 4.50 13.00
P-bunch 2.7?1012 ppb 150 ns to 0.45
ms Hg- jet diameter 1cm jet-velocity 3
m/s prep. velocity 5 m/s
16
Magnet field injection test 13T
17
13T Magnet field map
Grenoble high magnetic field laboratory vertical
Solenoid Bmax13 T observed maximum gradient
dB/dz49.5 T/m pulsed mercury jet, d4mm, v4-15
m/s Measurements in 20 T field planned for Sept.
01
Mirrors
18
Simulations
Surface evolution due to the interaction with
magnetic field
(R. Samulyak)
19
Comparison without/with magnetic field
- pictures taken with 0,1 ms shutter-speed (at
1000 fps) - all frames 48 ms after trigger of
valve
without field 0 T, v 4.6 m/s
with field
49.5 T/m, v 4 m/s
20
CERN Trough test
1/5 of the Neutrino factory beam power-densities
can be obtained in the 1.4 GeV BOOSTER/ISOLDE
p-beam
PSB-ISOLDE 3.2?1013 protons per pulse, 20,8,4
bunches (h5,2,1 ) Pulse length 2.4 ms (-20 ms
staggered extraction) Proton energy 1 GeV Trough
test at CERN Hg tight sealing 40 pulses.
Response to bunch up to 8?1013 ppB. Response to
beam size and beam energy. Disposal of Hg via
amalgams ?
21
CERN/ISOLDE In-Beam Experiment
- at ISOLDE Target Area
frontend
p beam
Hg container
camera
mirror
22
Nufact 140 bunches 1.15?1012
ppB bunch length 5 ns p-energy 2.2 GeV Pulse
duration 3.2 ms Pulse intensity 1.6?1014 ppp
velocities-pressure benchmarks for simulation
PSB-ISOLDE 4 bunches 8.0?1012 ppB bunch
length 200 ns p-energy 1,1.4 GeV Pulse
duration 3.2 ms Pulse intensity 3.2?1013 ppp
23
Radiation safety of trough test
24
Magnetic Horn
  • Units H40-400
  • Type mm 40-400
  • Waist radius mm 40
  • Peak current in horn kA 300
  • Total capacitance
  • for 1 switching section µF 1453
  • Duty cycle Hz 50
  • Pulse duration
  • (half period) µs 93
  • Charging voltage V 6283
  • Voltage on horn V 4200
  • r.m.s. current in horn kA 14.5
  • PH Mean power dissipation
  • in horn by current kW 39.
  • Water flow needed
  • in l/min with ?? w 15C l/min 3power
    dissipation due to beam absorption to be added

25
Water-cooled granular target
  • P. Sievers/CERN

Ta-Spheres, r 16.8 g/cm R 1mm Packing density
60 (140 spheres/cm3) R 10g/cm3 Small spheres
good for cooling surface/volume1.R Water
coolingv 6m/s through 20 of cross-section V
11l/s DT 18K (20 of 4MW, S. Gilardoni) DT
36K DP 4-5 Bar Re 104
26
Continuation of RD
  • Test the Hg-jet in a 20 T magnetic field
  • Systematic trough tests in the ISOLDE 1- 1.4 GeV
    proton beam
  • Development of jet hydrodynamic models
  • Improve the speed and hydrodynamic stability of
    the Hg-jet
  • Building of a prototype horn and test heat
    transfer coefficient at the inner conductor and
    if possible the lifetime.
  • Start preliminary engineering study of the
    integration of the plumbing of the target and the
    spent beam absorber in the horn.
  • Design and build a continuos flowing Hg-jet set
    up for in-beam tests.
  • Continue the study of alternative target concepts
    like radiation cooled solids and the water cooled
    granular target.
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