Assessment of the Fission Power Level in Fuel Rods Irradiated in the High Flux Materials Testing Reactor BR2 with the Aid of Fluence Dosimetry and Comparison with Other Methods

Author(s):  
C De Raedt ◽  
E Malambu ◽  
S Bodart ◽  
M Wéber ◽  
M Willekens
2021 ◽  
Vol 2021 ◽  
pp. 1-15
Author(s):  
Y. Xia ◽  
J. Li ◽  
R. Zhai ◽  
J. Wang ◽  
B. Lin ◽  
...  

Fission power is a promising technology, and it has been proposed for several future space uses. It is being considered for high-power missions whose goal is to explore the solar system and even beyond. Space fission power has made great progress when NASA’s 1 kWe Kilowatt Reactor Using Stirling TechnologY (KRUSTY) prototype completed a full power scale nuclear test in 2018. Its success stimulated a new round of research competition among the major space countries. This article reviews the development of the Kilopower reactor and the KRUSTY system design. It summarizes the current missions that fission reactors are being considered as a power and/or propulsion source. These projects include visiting Jupiter and Saturn systems, Chiron, and Kuiper belt object; Neptune exploration missions; and lunar and Mars surface base missions. These studies suggest that the Fission Electric Propulsion (FEP)/Fission Power System (FPS) is better than the Radioisotope Electric Propulsion (REP)/Radioisotope Power System (RPS) in the aspect of cost for missions with a power level that reaches ~1 kWe, and when the power levels reaches ~8 kWe, it has the advantage of lower mass. For a mission that travels further than ~Saturn, REP with plutonium may not be cost acceptable, leaving FEP the only choice. Surface missions prefer the use of FPS because it satisfies the power level of 10’s kWe, and FPS vastly widens the choice of possible landing location. According to the current situation, we are expecting a flagship-level fission-powered space exploration mission in the next 1-2 decades.


2009 ◽  
pp. 546-546-10
Author(s):  
CM De Raedt ◽  
LF Sannen ◽  
PJ Vanmechelen ◽  
BM Oliver

1989 ◽  
Vol 8 (3-4) ◽  
pp. 201-227 ◽  
Author(s):  
G. P. Lawrence ◽  
G. L. Varsamis ◽  
T. S. Bhatia ◽  
B. Blind ◽  
F. W. Guy ◽  
...  

1987 ◽  
pp. 381-393 ◽  
Author(s):  
J. Bakker ◽  
A. Baritello ◽  
J. Bordo ◽  
J. F. W. Markgraf ◽  
H. P. Leeflang ◽  
...  

Neutron News ◽  
1997 ◽  
Vol 8 (3) ◽  
pp. 28-28
Author(s):  
J.-M. Baugnet
Keyword(s):  

Author(s):  
Usha Pal ◽  
V. Jagannathan

Loading of seedless fertile rods has been used as the central principle to maximize fertile to fissile conversion in the two thorium breeder reactor concepts, viz. ATBR and FTBR [1, 2]. At fresh state the seedless thoria rods will produce practically no fission power, or nearly thousand times less fission rate compared to the seed fuel rods. Hence it is conceived that the fuel assembly would be constituted by assembling the fresh seed rods with one fuel cycle irradiated fertile thoria rods. Even in this state there is a wide disparity between the fissile content of these rods. By judicious choice of the rod dimensions and their relative locations, a degree of balance in the fission rate is achieved in the fresh state of seeded rods. Remarkably as the burnup proceeds the initially seedless fertile rods have a continuous growth of fissile content up to an asymptotic value for a given spectrum and the fissile content in seeded rods monotonically decreases. If the discharge burnup is sufficiently large by design, it is seen that the power share of the initially seedless fertile rods can even exceed that of the seed fuel rods. The physics principles of achieving this characteristic are presented in this paper.


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