Experiments and prospects for induction linac drivers
Description
In the last three years, the US program in Heavy Ion Fusion has concentrated on understanding the induction linac approach to a power-plant driver. In this method it is important that the beam current be maximized throughout the accelerator. Consequently, it is crucial to understand the space-charge limit in the AG transport system in the linac and, also, to achieve current amplification during acceleration to keep pace with the kinematical increase of this limit with energy. Experimental results on both these matters and also on the use of multiple beams (inside the same accelerating structure) will be described. A new examination of the most attractive properties of the induction linac for a fusion driver has clearly pointed to the advantage of using heavy ions with a charge-state greater than unity - perhaps q = 3 may be an optimum. This development places even greater importance on understanding space-charge limits and mechanisms for emittance growth; also, it will require a new emphasis on the development of a suitable ion source
Availability note (English)
MF available from INIS under the Report Number; Available from NTIS, PC A02/MF A01; 1 as DE87006144.
Files
Additional details
Publishing Information
- Imprint Pagination
- 14 p.
- Report number
- LBL--21345-Rev
Conference
- Title
- Symposium on heavy ion inertial fusion.
- Dates
- 27-29 May 1986.
- Place
- Washington, DC (USA).
INIS
- Country of Publication
- United States
- Country of Input or Organization
- United States
- INIS RN
- 18084119
- Subject category
- S70: PLASMA PHYSICS AND FUSION TECHNOLOGY; S43: PARTICLE ACCELERATORS;
- Resource subtype / Literary indicator
- Conference
- Descriptors DEI
- BEAM EMITTANCE; HEAVY ION ACCELERATORS; INERTIAL CONFINEMENT; ION SOURCES; LINEAR ACCELERATORS; SPACE CHARGE
- Descriptors DEC
- ACCELERATORS; CONFINEMENT; PLASMA CONFINEMENT
Optional Information
- Notes
- Portions of this document are illegible in microfiche products.
- Secondary number(s)
- CONF-860510--17-Rev.