|
V. A. Dolgashev et al., “Status of X-band Standing Wave Structure Studies at SLAC”, in Proc. 20th Particle Accelerator Conf. (PAC'03), Portland, OR, USA, May 2003, paper TPAB031, pp. 1264-1266. |
|
V. Ivanov et al., “Simulating Accelerator Structure Operation at High Power”, in Proc. 20th Particle Accelerator Conf. (PAC'03), Portland, OR, USA, May 2003, paper WPPG032, pp. 2664-2666. |
|
S. Doebert et al., “High Gradient Performance of NLC/GLC X-Band Accelerating Structures”, in Proc. 21st Particle Accelerator Conf. (PAC'05), Knoxville, TN, USA, May 2005, paper ROAC004, pp. 372-374. |
|
J. W. Wang et al., “Studies of Room Temperature Accelerator Structures for the ILC Positron Source”, in Proc. 21st Particle Accelerator Conf. (PAC'05), Knoxville, TN, USA, May 2005, paper RPPP044, pp. 2827-2829. |
|
L. Xiao, R. F. Boyce, D. Dowell, Z. Li, C. Limborg-Deprey, and J. F. Schmerge, “Dual Feed RF Gun Design for the LCLS”, in Proc. 21st Particle Accelerator Conf. (PAC'05), Knoxville, TN, USA, May 2005, paper TPPE058, pp. 3432-3434. |
|
Z. Li et al., “Coupler Design for the LCLS Injector S-Band Structures”, in Proc. 21st Particle Accelerator Conf. (PAC'05), Knoxville, TN, USA, May 2005, paper TPPT031, pp. 2176-2178. |
|
C. Limborg-Deprey, D. Dowell, Z. Li, J. F. Schmerge, and L. Xiao, “Modifications on RF Components in the LCLS Injector”, in Proc. 21st Particle Accelerator Conf. (PAC'05), Knoxville, TN, USA, May 2005, paper TPPT032, pp. 2233-2235. |
|
S. Doebert et al., “Beam Position Monitoring Using the HOM-Signals from a Damped and Detuned Accelerating Structure”, in Proc. 21st Particle Accelerator Conf. (PAC'05), Knoxville, TN, USA, May 2005, paper TPPT044, pp. 2804-2806. |
|
J. S. Sekutowicz et al., “Design of a Low Loss SRF Cavity for the ILC”, in Proc. 21st Particle Accelerator Conf. (PAC'05), Knoxville, TN, USA, May 2005, paper TPPT056, pp. 3342-3344. |
|
D. V. Neuffer et al., “Accelerator Design for the High-Power Industrial FEL”, in Proc. 16th Particle Accelerator Conf. (PAC'95), Dallas, TX, USA, May 1995, paper FAA25, pp. 243-245. |
