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Title: The liquid annular reactor system (LARS) propulsion

Conference · · AIP Conference Proceedings (American Institute of Physics); (United States)
DOI:https://doi.org/10.1063/1.40114· OSTI ID:5489262
; ; ; ;  [1];  [2]
  1. Brookhaven National Laboratory, Department of Nuclear Energy, Upton, NY (USA)
  2. SDIO The Pentagon, Washington, DC (USA)

A new concept for very high specific impulse ({gt}2000 seconds) direct nuclear propulsion is described. The concept, termed LARS (Liquid Annular Reactor System) uses liquid nuclear fuel elements to heat hydrogen propellant to very high temperatures ({similar to}6000 K). Operating pressure is moderate ({similar to}10 atm), with the result that the outlet hydrogen is virtually 100% dissociated to monatomic H. The molten fuel is contained in a solid container of its own material, which is rotated to stabilize the liquid layer by centripetal force. LARS reactor designs are described, together with neutronic and thermal-hydraulic analyses. Power levels are on the order of 200 megawatts. Typically, LARS designs use 7 rotating fuel elements, are beryllium moderated and have critical radii of {similar to}100 cm (core L/D{approx}1.5).

DOE Contract Number:
AC02-76CH00016
OSTI ID:
5489262
Report Number(s):
CONF-910116-; CODEN: APCPC
Journal Information:
AIP Conference Proceedings (American Institute of Physics); (United States), Vol. 217:2; Conference: 8. symposium on space nuclear power systems, Albuquerque, NM (United States), 6-10 Jan 1991; ISSN 0094-243X
Country of Publication:
United States
Language:
English