3 MeV test stand measurement plans A. Lombardi for the LINAC4 team 10/01/2013BCC 41 - 3MeV test...

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3 MeV test stand measurement plans A. Lombardi for the LINAC4 team 10/01/2013 BCC 41 - 3MeV test stand measurements 1

description

LINAC end-to-end Location and causes of e growth and losses: LEBT solenoids (divergent beam from the source). 45 keV MEBT transport (abrupt change of phase advance). 3 MeV BOTH ARE UNAVOIDABLE but they must be controlled

Transcript of 3 MeV test stand measurement plans A. Lombardi for the LINAC4 team 10/01/2013BCC 41 - 3MeV test...

Page 1: 3 MeV test stand measurement plans A. Lombardi for the LINAC4 team 10/01/2013BCC 41 - 3MeV test stand measurements1.

BCC 41 - 3MeV test stand measurements 1

3 MeV test stand measurement plans

A. Lombardi for the LINAC4 team

10/01/2013

Page 2: 3 MeV test stand measurement plans A. Lombardi for the LINAC4 team 10/01/2013BCC 41 - 3MeV test stand measurements1.

Scope Validate • Source and LEBT design• RFQ design • Chopper

Ultimate goal is to demonstrate

70 mA H-

400 µs

1 Hz

3 MeV

0.4 mm mrad

0.15 deg KeV

Chopped and matched to the DTL

Source 45 keV

RFQ 3 MeV

Chopper

Diagnostic line

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LINAC end-to-end

0

20

40

60

80

100

120

140

160

180

0 10 20 30 40 50 60 70 80

Kinetic Energy [MeV] vs. lenght (m)

RFQ DTL 3-50 MeV

CCDTL 50-100 MeV

PIMS 100-160 MeV

2.00E-07

2.50E-07

3.00E-07

3.50E-07

4.00E-07

4.50E-07

0 10 20 30 40 50 60 70 80

Normalised RMS transverse emittance (PI m rad)

x

y

transition

transition

Location and causes of e growth and losses:

LEBT solenoids (divergent beam from the source). 45 keVMEBT transport (abrupt change of phase advance). 3 MeV

BOTH ARE UNAVOIDABLE but they must be controlled

0.00E+00

2.00E+00

4.00E+00

6.00E+00

8.00E+00

1.00E+01

1.20E+01

1.40E+01

1.60E+01

1.80E+01

2.00E+01

0 10 20 30 40 50 60 70 80

aper

ture

/rm

s bea

m si

ze

meters

aperture/rms beam size vs lenght

DTL : FFDD and FODOLEBT RFQ MEBT CCDTL : FODO PIMS : FODO

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Emittance 0-3 MeV

2.00E-07

2.50E-07

3.00E-07

3.50E-07

4.00E-07

4.50E-07

5.00E-07

5.50E-07

6.00E-07

0 2 4 6 8 10 12

normalised RMS-Emittance [m.rad] vs lenght

(X,BGX') RMS-Emittance [m.rad]

(Y,BGY') RMS-Emittance [m.rad]

Symmetry x,y in LEBT, if source is symmetric

Losses in the RFQ, emittance decreases

Losses and emittance increase when matching to the DTL

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BCC 41 - 3MeV test stand measurements 5

bench

10/01/2013

Spectrometer (0.2 %)Slit and Grid EmittanceToF (calibration)Bunch Shape MonitorHalo Monitor (chopping eff.)TransformersFeshenko

EDMS – 1004908 G. Bellodi

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BCC 41 - 3MeV test stand measurements 6

Measurement plan – 1/2

10/01/2013

Stage 1 – after the RFQ 9 parameters : 2 solenoids, RFQ amplitude, 2 quads , 2 steerers

Scan Minimum beam

1) RFQ Transmission Solenoids, RF power Initially I =20 mA (min) Emi= 0.5 (max)

Needs I=70 mAEmi = 0.25 to fully validate.

2) RFQ emittance Solenoids, RF power

3) RFQ energy spread/longitudinal emitt

Solenoids, RF power

NEED TO ACHIEVE TRANSMISSION THROUGH THE RFQ OF 80% TO GO TO THE NEXT STAGE (NOMINAL TRANSMISSION IS 92%)

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Measurement plan – 2/2

10/01/2013

Stage 2 – after the chopper30 parameters : stage 1 parameters + 11 quads, 3 RF ampli, 3 RF phases, chopper voltage, 2 steerers

Scan Minimum beam At RFQ input

1) Transmission All parameters Initially I =50 mA (min) Emi= 0.4 (max)

Needs I=70 mAEmi = 0.25 to fully validate.

2) CHOPPING Pencil beamAll quads

3) Transverseemittance4) Longitudinal plane Buncher settings

FULL CHARACTERISATION IS NOT POSSIBLE, BUT GIVE PRIORITY TO THE MORES CRITICAL ITEMS

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Pencil beam All elements on Chooper on (top) Chopper off (bottom)

With this we validate :1) Chopper voltage2) Optics

we do not validate : 3) Space charge4) Rise/fall time

MOST IMPORTANT MEAS

BEAM AT THE ws JUST BEFORE THE INLINE DUMP

Page 9: 3 MeV test stand measurement plans A. Lombardi for the LINAC4 team 10/01/2013BCC 41 - 3MeV test stand measurements1.

OP DAY - 26th January 2012 Archamps 9

Measurement 2011 – p from DESY

RFQ acceptance vs. Measured emittance Measured after source vs. Measured at the RFQ input plane and backtracked to the source

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Protons• Already discussed – EDMS 1096658 • Measurement with Desy source in proton mode (2011)

gave an excellent insight into LEBT dynamics and solenoid modelling

To be done before protons are usable : • optimise to reach a min of 50-60 mA after the first

solenoid, • measure emittance vs. solenoid settings (5-10) and back-

trace to source input : create a beam for simulating/optimising the whole test stand.

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Sharing the test stand- proposal(change over takes ½ day to 1 day)

• Run in proton mode until the emittance metre has to be dismantled

• Source development till RFQ ready for beam• Share 2:1 between 3 MeV measurements and

source development, over 3 weeks period or as best convenient.

• DO NOT FORGET COMMISSIONING TIME FOR DIAGNOSTICS

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Proposal - • 3 MeV beam commissioning must be done in 2 sessions/day

on the basis 5 days/week . E.g. 7:00- 14:00 and 14-21

• We (BD team) are 3 staff + 3 visitors

• Daily brief meeting with the people on the field + 1 by-weekly meeting in the control room to take decisions – CALLED BY GB

• Need experts available as much as possible (in 2011 we “took it easy” but it took 6 months to measure the LEBT!)

10/01/2013

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Something has to give…• Laser stripping measurements ( make sure that BI is made aware)• Halo measurements under different matching• Matching to the DTL • Buncher optimisation • Pencil beam scans • Calibration of TOF vs. spectrometre…….. And many more

10/01/2013

The time presently allocated for commissioning in the tunnel is not sufficient-need 6 months

We should repeat the measurements after the RFQ in the tunnel