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Phase 1 Space Fission Propulsion System Design Considerations

机译:第1阶段空间裂变推进系统设计考虑因素

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Fission technology can enable rapid, affordable access to any point in the solar system. If fission propulsion systems are to be developed to their full potential; however, near-term customers must be identified and initial fission systems successfully developed, launched, and operated. Studies conducted in fiscal year 2001 (IISTP, 2001) show that fission electric propulsion (FEP) systems operating at 80 kWe or above could enhance or enable numerous robotic outer solar system missions of interest. At these power levels it is possible to develop safe, affordable systems that meet mission performance requirements. In selecting the system design to pursue, seven evaluation criteria were identified: safety, reliability, testability, specific mass, cost, schedule, and programmatic risk. A top-level comparison of three potential concepts was performed: an SP-100 based pumped liquid lithium system, a direct gas cooled system, and a heatpipe cooled system. For power levels up to at least 500 kWt (enabling electric power levels of 125-175 kWe, given 25-35% power conversion efficiency) the heatpipe system has advantages related to several criteria and is competitive with respect to all. Hardware-based research and development has further increased confidence in the heatpipe approach. Successful development and utilization of a "Phase 1" fission electric propulsion system will enable advanced Phase 2 and Phase 3 systems capable of providing rapid, affordable access to any point in the solar system.
机译:裂变技术可以快速,经济地访问太阳系中的任何一点。如果要开发裂变推进系统的全部潜力;但是,必须识别近期客户,并成功开发,启动和操作初始裂变系统。 2001年财政年度(IISTP,2001)进行的研究表明,在80 kWe或以上操作的裂变电动推进(FEP)系统可以增强或使众多的机器人外部太阳系特使。在这些功率水平,可以开发满足任务性能要求的安全,实惠的系统。在选择追求系统设计时,确定了七个评估标准:安全,可靠性,可测试性,特定质量,成本,日程表和程序风险。进行了三个潜在概念的顶级比较:基于SP-100的泵送液锂系统,直接气体冷却系统和热管冷却系统。对于高达至少500 kWt的功率水平(使电力水平为125-175 kWe,给予25-35%的功率转换效率),热管系统具有与若干标准相关的优势,并且对所有标准具有竞争力。基于硬件的研发在热管方法方面进一步增加了置信度。成功的开发和利用“第1阶段”裂变电动推进系统将实现高级阶段2和相位3系统,能够提供对太阳系中的任何点的快速,价格合理的访问。

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