DocumentCode :
2898894
Title :
Vertical instability at IPNS RCS
Author :
Wang, S. ; Brumwell, F.R. ; Dooling, J.C. ; Harkay, K.C. ; Kustom, R. ; McMichael, G. ; Middendorf, M.E. ; Nassiri, A.
Author_Institution :
ANL, Argonne
fYear :
2007
fDate :
25-29 June 2007
Firstpage :
2022
Lastpage :
2024
Abstract :
The rapid cycling synchrotron (RCS) of the intense pulsed neutron source (IPNS) at ANL accelerates > 3.0 times 1012 protons from 50 MeV to 450 MeV with 30-Hz repetition frequency. During the acceleration cycle, the rf frequency varies from 2.21 MHz to 5.14 MHz. Presently, the beam current is limited by a vertical instability. By analyzing turn-by-turn beam position monitor (BPM) data, large- amplitude mode 0 and mode 1 vertical beam centroid oscillations were observed in the later part of the acceleration cycle. The oscillations start in the tail of the bunch, build up, and remain localized in the tail half of the bunch. This vertical instability was compared with a head-tail instability that was intentionally induced in the RCS by adjusting the trim sextupoles. It appears that our vertical instability is not a classical head-tail instability [1]. More data analysis and experiments were performed to characterize the instability.
Keywords :
accelerator RF systems; neutron sources; particle beam bunching; particle beam diagnostics; particle beam stability; proton accelerators; synchrotrons; BPM; IPNS RCS; amplitude mode; centroid oscillations; electron volt energy 50 MeV to 450 MeV; frequency 30 Hz; intense pulsed neutron source; proton bunch; rapid cycling synchrotron; rf frequency; trim sextupoles; turn-by-turn beam position monitor; vertical instability; Acceleration; Frequency; Monitoring; Neutrons; Particle beams; Phase modulation; Protons; Signal processing; Synchrotrons; Tail;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Particle Accelerator Conference, 2007. PAC. IEEE
Conference_Location :
Albuquerque, NM
Print_ISBN :
978-1-4244-0916-7
Type :
conf
DOI :
10.1109/PAC.2007.4441132
Filename :
4441132
Link To Document :
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