NLC
Status and Milestones
D. L. Burke
ISG9KEK
December 10-13, 2002
NLC
ISG9 OpeningD. L. Burke
Mission and Strategy
There is compelling reason to establish the X-Band technology soon.
– The international science community is taking on a 20-year mission to understand particle physics at the TeV energy scale.
– The LHC and a linear collider must have periods of concurrent operation to reinforce and guide each other, just as the case has been in the past.
– Construction and commissioning of a linear collider will take ~ 8 years.
Making a choice of linac technologies will enhance the probability that a linear collider is built and ready in time to meet this mission.
We must accelerate the demonstration of an X-Band rf system … and we must do it with no increase in level of funding.
NLC
ISG9 OpeningD. L. Burke
8-Pack Phase-I
klystrons
TE02
TE01
TE01
TE02
mode-preserving taper (TE02 cutoff at small end)
iris
Dual-Moded Pulse Compression System
mode mixer
cross potent
dual-mode directional coupler
load trees
reflective TE01 TE 02 mode converter / tuning plunger
jog-converter
dual-mode combiner
height taper
T/4
T/4
dual-mode-preserving taper
TE01
TE11or
TE01or
TE11(unSLEDed)
dual-mode splitter
bend -converter
circ-rect taper
E-plane bend
H-plane bend
TE11or
TE01(unSLEDed)
possible add-on
PPM Klystrons (75 MW 1.6 µsecs)
Dual-Mode SLED-II(4-fold compression in
time, factor 3.3 in power)
Power to loads in March 2003.
“Single Feed” RF Pulse(500 MW 400 nsec)
NLC
ISG9 OpeningD. L. Burke
NLC/JLC(X) SLED-II Baseline
• Phase-I of the 8-Pack will demonstrate the feasibility of a SLED-II rf system similar to that presently in use at the NLCTA.
• This demonstration will occur in 2003.
• JLC and NLC physicists presented to the world community (ILC-TRC) a SLED-II Baseline Design for an X-Band collider.
The “R1s”
» SLED-II Power Demonstration
» Structure Gradients
NLC
ISG9 OpeningD. L. Burke
The Test AcceleratorThe Test Accelerator
The NLCTA with 1.8 m accelerator structures (ca 1997).
Demonstrated ability to reach 500 GeV cms.
Accelerating gradient of 25 MV/m (loaded) with good wakefield control and energy spread.
Structures from KEK.
RF Power from SLAC
NLC
ISG9 OpeningD. L. Burke
X-Band RF Systems
NLCTASLED-II System
(1997)
– Conventional PFN modulator
– 50 MW/1.2s solenoid-focused klystrons
– SLED-II pulse compression
– 1.8m DDS structures at 40 MV/m
X-Band TeVSLED-II System(2002)
– Solid-state modulator
– 75 MW/1.6sPPM-focused klystrons
– Dual mode SLED-II pulse compression
– 0.9m DDS structures at 65 MV/m
NLC
ISG9 OpeningD. L. Burke
NLC/JLC SLED-II Baseline Test
NLCTA Housing
Solid-State Modulator
Solenoid-Focused Klystrons (to be replaced with PPM tubes).
Dual-Mode SLED-II
NLC
ISG9 OpeningD. L. Burke
SLED-II Demonstration Status
• Modulator is on-line and driving a pair of XL-4 klystrons.
• Third XL-4 klystron being installed, and fourth being conditioned in the Test Lab.
• All SLED-II designs passed microwave “cold tests” and components are in production.
On schedule for power tests to loads in March 2003.
Permanent magnet focused klystrons (one each from KEK and SLAC) scheduled for test in February.
NLC
ISG9 OpeningD. L. Burke
klystrons
TE02
TE01
TE01
TE02
mode-preserving taper (TE02 cutoff at small end)
iris
Dual-Moded Pulse Compression System
mode mixer
cross potent
dual-mode directional coupler
load trees
reflective TE01 TE 02 mode converter / tuning plunger
jog-converter
dual-mode combiner
height taper
T/4
T/4
dual-mode-preserving taper
TE01
TE11or
TE01or
TE11(unSLEDed)
dual-mode splitter
bend -converter
circ-rect taper
E-plane bend
H-plane bend
TE11or
TE01(unSLEDed)
possible add-on
Dual-Mode SLED IILow-Power (Cold) Tests
0
0.2
0.4
0.6
0.8
1
1.2
-200 -100 0 100 200 300 400 500
Reflected PulseInput Pulse
Ma
gn
itu
de
Time [ns]
320 ns
0
0.2
0.4
0.6
0.8
1
1.2
-200 -100 0 100 200 300 400 500
InputPulse Mag
Ma
gn
itu
de
Time [ns]
Input Pulse
(TE01)
First Reflection (TE02)
Second Reflection (TE01) 0
1
2
3
4
5
-2000 -1000 0 1000 2000
OutputInput
Po
we
rTime [ns]
NLC
ISG9 OpeningD. L. Burke
RF Pulse Heating
0
2
4
6
8
10 Distribution of Breakdowns(70 MV/m, 400 ns, 10 hr run)
T53VG3
RFRF
Beam’s eye view of input coupler.
SEM picture of input matching iris.Pulse heating in excess of 100° C.
Input coupler Output coupler58 Cells
Performance limited by pulse heating of coupler matching irises.
Rate in cells .1/hr
Autopsy performed after high-gradient testing.
NLC
ISG9 OpeningD. L. Burke
Mode Conversion (MC) Coupler
|Es|max= ~34 MV/m @ 48 MW
|Hs|max= ~98.4 kA/m @ 48 MW
Pulse Heating ~ 3° C
TM01 Mode Launcher
WC90
WR90
RF
Matching Cell
Mode Conversion Coupler
RF
NLC
ISG9 OpeningD. L. Burke
Unl
oade
d G
radi
ent (
MV
/m)
Time with RF On (hr)
Operations of T53VG3MC (Mode Conversion Couplers)
1Trip / 25 Hours
400 ns Pulse Width
1 Trip / 25 Hours
NLC/JLC Trip Requirement:< 1 per 10 Hours at 65 MV/m
NLC
ISG9 OpeningD. L. Burke
Test structures exceed the design goal of 65 MV/m for the JLC/NLC TeV collider.
Remains to complete fabrication and test of “NLC/JLC-Ready” structures with full detuning and damping.
• First tests of a/ = 0.18 structures (with bad couplers) look good, and testing of structures (with good couplers) is starting.
• Will start testing full-featured structures in May to satisfy TRC R1 items. There is a broadly-based line-up of structures in design and fabrication at SLAC, KEK, Fermilab, and CERN.
Schedule.
High-Gradient R&D Summary
NLC
ISG9 OpeningD. L. Burke
Bypass Linese.g. 50, 175, 250 GeV
X-Band Accelerator with Length for
500 GeV/Beam
32 k
m3.5 km
Injector Systems for 1.5 TeV
Why X-Band?
NLC
ISG9 OpeningD. L. Burke
NLC/JLC Energy Reach
The JLC/NLC Stage 2 design luminosity is
5 1033 cm-2 s-1 at 1.3 TeV cms.
CMS Energy (GeV)Site US Japan US Japan
Luminosity (1033) 20 25 30 25Repetition Rate (Hz) 120 150 120 100
Bunch Charge (1010)Bunches/RF PulseBunch Separation (ns)Loaded Gradient (MV/m)
Injected x / y (10-8)
x at IP (10-8 m-rad)
y at IP (10-8 m-rad)
x / y at IP (mm)
x / y at IP (nm)
x / y at IP (nm)
z at IP (um)
avePinch Enhancement
Beamstrahlung B (%)Photons per e+/e-Two Linac Length (km)
High Energy IP ParametersStage 1 Stage 2
500 1000
0.75
1.450
192
300 / 2
360
4
8 / 0.11
219 / 2.1
17 / 20
1.51
13.81.35.4
243 / 3.0
32 / 28
110
0.14
300 / 2
360
4
13 / 0.11
1.327.6
0.75
110
0.291.47
8.9
1921.450
Luminosity (1034
)
CM
S E
nerg
y (G
eV)
0 0.5 1 1.5 2 2.5 31000
1050
1100
1150
1200
1250
1300
1350
25 Bunches
192 Bunches
NLC
ISG9 OpeningD. L. Burke
Energy Goals
The energy reach of NLC/JLC is significantly greater than that of TESLA (for comparable cost).
This will be the central issue in the choice of technology.
– HEPAP 2001 “… 500 GeV … expandable to 800-1000 GeV …”
– ECFA 2001 “… 400 GeV …”
– ACFA 2001 “… initial 300-500 GeV … upgrade to greater than 1 TeV.”
The international community needs to reach a consensus on the importance of access to the highest energies.
NLC
ISG9 OpeningD. L. Burke
• “By the end of 2003, we hopefully should know if TESLA can reach 800 GeV at 35 MV/m.”
• “By the end of 2003, we hopefully should know if JLC/NLC can meet its main linac [TeV] RF system specifications.”
• “If yes, then the International Community could make a choice based on the other respective merits of these machines.”
ILC-TRC Interim ReportICFA
CERN, October 2002
NLC
ISG9 OpeningD. L. Burke
NLC-JLC Collaboration
Our job is to prepare for this technology choice.
• Complete the critical R&D (TRC R1 and R2)
• Update and document the X-Band Baseline design.
• Understand site requirements and cost estimates.
ISG9 will focus on this job.