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Considerations for improvements to the 25 TW Saturn high-current driver

IEEE International Pulsed Power Conference

Savage, Mark E.; Struve, Kenneth W.; Austin, Kevin N.; Coffey, S.K.; Jones, Peter A.; Joseph, Nathan R.; Kirschner, Debra S.; Lott, John A.; Oliver, Bryan V.; Spielman, Rick B.

The Saturn X-ray generator is a 2.5 megavolt, 10 megampere electrical driver at Sandia National Laboratories. Saturn has been in operation for more than 30 years. Work is underway to identify key areas of the machine, improvement of which would benefit operational efficiency and reproducibility of the system. Saturn is used to create high-dose, short-pulse intense ionizing radiation environments for testing electronic and mechanical systems. Saturn has 36 identical modules driving a common electron beam bremsstrahlung load. Each module utilizes a microsecond Marx generator, a megavolt gas switch, and untriggered water switches in a largely conventional pulse-forming system. Achieving predictable and reliable radiation exposure is critical for users of the facility. Saturn has endured decades of continual use with minimal opportunities for research, improvements, or significant preventive maintenance. Because of degradation in components and limited attention to electrical performance, the facility has declined both in the number of useful tests per year and their repeatability. The Saturn system resides in a cylindrical tank 33m in diameter, and stores 5.6 MJ at the nominal operating Marx charge voltage. The system today is essentially identical to that described by Bloomquist in 1987. [1] Advances in technology for large pulsed power systems affords opportunities to improve the performance and more efficiently utilize the energy stored. Increased efficiency can improve reliability and reduce maintenance. The goals for the Saturn improvement work are increased shot rate, reduced X-ray dose shot-To-shot dose fluctuation, and reduced required maintenance. Major redesign with alternate pulsed power technology is considered outside the scope of this effort. More X-ray dose, larger exposure area, and lower X-ray endpoint energy are also important considerations but also deemed outside the scope of the present project due to schedule and resource constraints. The first considerations, described here, are improving the present design with better components.

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Three-Dimensional Model of the Saturn Accelerator Water Tri-Plate Transmission Line Connection to the Vacuum Insulator Stack

IEEE International Pulsed Power Conference

Struve, Kenneth W.; Ulmen, B.

Calculation of the power flow from the 36 pulse forming lines to the vacuum region of Saturn has always been complicated by the three-dimensional structure of the rod and bottle connections to the vacuum insulator stack. Recently we have completed a 3-D calculation of the bottle configuration and found a large error in previous impedance estimates. We have used this calculation to determine impedance and to construct a 2-D model of each of the 36 bottles of each level of the insulator using the Transmission Line Matrix (TLM) technique. These TLM models are then used in a 2-D model for each of the three levels of the insulator. Each model starts at a measured forward-going pulse in the water tri-plate and ends at the Brehmstrahlung load at the center of the machine. Because of long transmission line lengths and short pulse lengths, each level can be considered independent of the others. A combination of the three models then represents a quasi-3-D model of the load region of the machine. The results of these calculations agree well with measurement and thereby provide confidence in simulation predictions for those areas where measurements are not possible. Details of the 3-D bottle calculation, the TLM model, and results of the load region simulations using this model are given.

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Daily operation of Z: an 80 TW 36-module pulsed power driver

Savage, Mark E.; Cuneo, M.E.; Davis, Jean-Paul D.; Hutsel, Brian T.; Jones, Michael J.; Jones, Peter A.; Kamm, Ryan J.; Lopez, Michael R.; Matzen, M.K.; McDaniel, D.H.M.; McKee, George R.; Maenchen, J.E.M.; Owen, A.C.O.; Porter, John L.; Prestwich, K.R.P.; Schwarz, Jens S.; Sinars, Daniel S.; Stoltzfus, Brian S.; Struve, Kenneth W.; Stygar, William A.; Wakeland, P.; White, William M.

Abstract not provided.

Results 1–25 of 109
Results 1–25 of 109