Deployment history and design considerations for space reactor power systems

被引:105
作者
El-Genk, Mohamed S. [1 ,2 ]
机构
[1] Univ New Mexico, Inst Space & Nucl Power Studies, Dept Chem & Nucl Engn, Albuquerque, NM 87131 USA
[2] Univ New Mexico, Dept Mech Engn, Albuquerque, NM 87131 USA
关键词
BUK; RORSAT; TOPAZ; SNAP-10A; Space reactor power systems; Reentry; COPUOS; Safety; Reliability; NUCLEAR-POWER; ENERGY;
D O I
10.1016/j.actaastro.2008.12.016
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The history of the deployment of nuclear reactors in Earth orbits is reviewed with emphases on lessons learned and the operation and safety experiences. The former Soviet Union's "BUK" power systems, with SiGe thermoelectric conversion and fast neutron energy spectrum reactors, powered a total of 31 Radar Ocean Reconnaissance Satellites (RORSATs) from 1970 to 1988 in 260 km orbit. Two of the former Soviet Union's TOPAZ reactors, with in-core thermionic conversion and epithermal neutron energy spectrum, powered two Cosmos missions launched in 1987 in similar to 800km orbit. The US' SNAP-10A system, with SiGe energy conversion and a thermal neutron energy spectrum reactor, was launched in 1965 in 1300 kin orbit. The three reactor systems used liquid NaK-78 coolant, stainless steel Structure and highly enriched uranium fuel (90-96wt%) and operated at a reactor exit temperature of 833-973 K. The BUK reactors used U-Mo fuel rods, TOPAZ used UO2 fuel rods and four ZrH moderator disks, and the SNAP-10A used moderated U-ZrH fuel rods. These low power space reactor systems were designed for short missions (similar to 0.5 kW(e) and similar to 1 year for SNAP-10A, < 3.0 kW(e) and < 6 months for BUK, and similar to 5.5 kW(e) and up to 1 year for TOPAZ). The deactivated BUK reactors at the end of mission, which varied in duration from a few hours to similar to 4.5 months, were boosted into similar to 800km storage orbit with a decay life of more than 600 year. The ejection of the last 16 BUK reactor fuel cores caused significant contamination of Earth orbits with NaK droplets that varied in sizes from a few microns to 5cm. Power systems to enhance or enable future interplanetary exploration, in-situ resources utilization on Mars and the Moon, and civilian missions in 1000-3000km orbits would generate significantly more power of 10's to 100's kW(e) for 5-10 years, or even longer. A number of design options to enhance the operation reliability and safety of these high power space reactor power systems are presented and discussed. (C) 2009 Elsevier Ltd. All rights reserved.
引用
收藏
页码:833 / 849
页数:17
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