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Schematic diagram of the RAL radiation cooled rotating toroidal tantalum target rotating toroid proton beam solenoid magnet toroid at 2300 K radiates heat to water-cooled surroundings toroid magnetically levitated and driven by linear motors
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Parameters of the NF TargetProton Beam pulsed 10-50 Hz pulse length 1-2 s energy 2-30 GeV average power ~4 MW
Target (not a stopping target)
mean power dissipation 1 MW energy dissipated/pulse 20 kJ (50 Hz) energy density 0.3 kJ/cm3 (50 Hz)
2 cm
20 cm
beam
Schematic diagram of the RAL radiation cooled rotating toroidal tantalum target
rotating toroid
proton beam
solenoid magnet
toroid at 2300 K radiates heat to water-cooled surroundings
toroid magnetically levitated and driven by linear motors
The New ProgrammeSince NuFact04 the R&D programme has altered significantly: 1. Simulate shock by passing a pulsed current through a wire.2. Measure the radial motion of the wire to evaluate the constitutive equations (with 3.).3. Use a commercial package, LS-DYNA to model the behaviour.4. Life time/fatigue test. 50 Hz for 12 months.5. Investigate the possibility of widely spaced micro- bunches of proton beam to reduce the shock impact.
Proposed R&D (2004)1. Calculate the energy deposition, radio-activity for the target, solenoid magnet and beam
dump. Calculate the pion production (using results from HARP experiment) and calculate
trajectories through the solenoid magnet.2. Model the shock a) Measure properties of tantalum at 2300 K. b) Model using hydrocodes developed for explosive applications at LANL, LLNL, AWE, etc. c) Model using dynamic codes developed by ANSYS.3. Radiation cooled rotating toroid
a) Calculate levitation drive and stabilisation system.b) Build a model of the levitation system.
4. Individual bars a) Calculate mechanics of the system. b) Model system.5. Continue electron beam tests on thin foils, improving the vacuum.6. In-beam test at ISOLDE - 105 pulses.7. In-beam tests at ISIS – 107 pulses.8. Design target station.
Shock, Pulse Length and Target SizeWhen a solid experiences a temperature rise the material expands. Because of mass inertia there will always be a slight lag in the expansion. This causes pressure waves to ripple through the material. When the temperature rise is relatively large and fast, the material can become so highly stressed that there is permanent distortion or failure - shock.Short high intensity beam pulses will give rise to shock in a target.The shock wave travels through matter at the speed of sound,
where E is Young's modulus of elasticity and ρ is the density.
Es
The time taken for the wave to travel from the outer surface to the centre is given by
If the beam pulse (τp) is long compared to the characteristic time τs, then little energy goes into the target in this time and the shock wave in the target is reduced.
If the target is small compared to the beam pulse length the shock is reduced.
If No problem!
Must have sufficient pulsed energy input!
psd
sd
s
The Proton Pulse
macro-pulse
micro-pulse
Proton beam “macro-pulses” and “micro-pulses”.Traditionally we have considered the micro-pulses as ~1 ns wide and the macro-pulses as ~1 s wide. The temperature rise per macro-pulse is ΔT ~ 100 K.For the tantalum bar target, radius 1 cm and length 20 cm, then: The time for the shock wave to travel a radius is 3 ms The time for the shock wave to travel a half the length is 30 ms
However, in the RAL proton driver scheme with ~10 micro-pulses, it is likely that they could be spaced apart by ~40 s, thus reducing the effective thermal shock to only ΔT ~ 10 K.
Effect of 10 micro-pulses in 1 and 5 s long macro-pulses.
NF Target:
1 cm radius
20 cm long
= 3 s
Total temperature rise:
T = 100 K
Goran Skoro, Sheffield University
Pulse HeatingPulsed ohmic-heating of wires can replicate pulsed proton
beam induced shock.
current pulse
tantalum wire
Energy density in the wire needs to be ε0 = 300 J cm-3 to correspond to 1 MW dissipated in a target of 1 cm radius and 20 cm in length at 50 Hz.
Transient Conditions•Assume an electric field E is instantaneously applied across a conducting wire. •Apply Maxwell’s equations. •This produces a diffusion equation:
In cylindrical coordinates, where j is the current density.•The solution is:
rj
rrj
tj
zz 112
2
0
1 1
00
221n nn
ntzz aJ
rJe
ajj n
= 1/0
The Velocity of the Shock Wave• Shock travels at the Speed of Sound.
• Can only use small diameter wires of up to ~0.4 mm to get current penetration into the wire.• “Choose a better material”
151- s cm 3.3x10 ns μm 3.3 -Es
2aI v
as
Characteristic Times for the shock to travel across the radius and for the current to penetrate the wire (square pulse).
Ips
τsτIns
a, mm 10.1
10
100
10000
1000
Doing the TestThe ISIS Extraction Kicker Pulsed Power Supply
Time, 100 ns intervals
Voltage waveform
Rise time: ~100 ns Voltage peak: ~40 kV Repetition rate up to 50 Hz.
Flat Top: ~300 ns Current Peak: ~8 kA There is a spare available for use.
Exponential with 20 ns rise time fitted to the waveform
Solution for the case of an exponential rise in current
tejj 10
12
1
0
2
0
2
0
0
2
21n n
nn
nt
e
aJ
a
earJ
ae
aJ
rJ
jj
tan
0 0.2 0.4 0.6 0.8 10
0.2
0.4
0.6
0.8
1
0 0.2 0.4 0.6 0.8 10
0.2
0.4
0.6
0.8
1
r/a
j/j0
30 ns
10 ns 1 ns
100 ns1000 ns
Current density versus radius at different times. Wire radius, a = 0.3 mm.
0 2 10 8 4 10 8 6 10 8 8 10 8 1 10 70
0.2
0.4
0.6
0.8
1
t0 2 10 8 4 10 8 6 10 8 8 10 8 1 10 7
0
0.2
0.4
0.6
0.8
1
0 2 10 8 4 10 8 6 10 8 8 10 8 1 10 70
0.2
0.4
0.6
0.8
1
t
Current density at r = 0 versus time (t, s), for different wire radii (a, mm).
0.1 mm 0.2 mm 0.3 mm 0.4 mm
0.6 mm
te 1j/j0
, s
The average current density over the wire cross section versus time (t, s), for various wire radii, (a, mm).
a
e drtarrjM0
),,(2
1 10 9 1 10 8 1 10 7 1 10 60
0.2
0.4
0.6
0.8
1
t1 10 9 1 10 8 1 10 7 1 10 60
0.2
0.4
0.6
0.8
1
t
te 1
1 mm
0.5
0.4
0.3
0.2
0.1
Effect of different pulse lengths (shown by arrows), for exponential current rise of 30 ns.
Goran Skoro, Sheffield University.
Effect of different pulse lengths (shown by arrows), for exponential current rise of 30 ns.
Goran Skoro, Sheffield University.
Radiusmm
Characteristic timeτs, ns
Energy densityMJ m-3
0.1 30 3230.2 60 690.3 90 210.4 120 80.5 150 3.40.6 180 1.60.7 210 0.80.8 240 0.40.9 270 0.21.0 300 0.1
The energy density dissipated at the centre of the wire, within a time τs fordifferent wire radii, with I0 = 10000 A.
t e dtjE0
2
Energy Density in the Wire
Radiusmm
Characteristic timeτs, ns
CurrentI0, kA
0.1 30 100.2 60 210.3 90 370.4 120 610.5 150 940.6 180 1380.7 210 1970.8 240 2730.9 270 3731.0 300 499
02
0 jaI
Pulse Current Requirements
The current, I0, required to dissipate 300 MJ m-3 at the centre of the wire within a time τs, for different wire radii.
to vacuum pumpor helium gas cooling
heater
test wire
insulators
to pulsed power supply
to pulsed power supply
water cooled vacuum chamber
Schematic diagram of the test chamber and heater oven.