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Fission Surface Power Technology Development Update

机译:裂变表面功率技术开发更新

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摘要

Power is a critical consideration in planning exploration of the surfaces of the Moon, Mars, and places beyond. Nuclear power is an important option, especially for locations in the solar system where sunlight is limited or environmental conditions are challenging (e.g., extreme cold, dust storms). NASA and the Department of Energy are maintaining the option for fission surface power for the Moon and Mars by developing and demonstrating technology for a fission surface power system. The Fission Surface Power Systems project has focused on subscale component and subsystem demonstrations to address the feasibility of a low-risk, low-cost approach to space nuclear power for surface missions. Laboratory demonstrations of the liquid metal pump, reactor control drum drive, power conversion, heat rejection, and power management and distribution technologies have validated that the fundamental characteristics and performance of these components and subsystems are consistent with a Fission Surface Power preliminary reference concept. In addition, subscale versions of a non-nuclear reactor simulator, using electric resistance heating in place of the reactor fuel, have been built and operated with liquid metal sodium-potassium and helium/xenon gas heat transfer loops, demonstrating the viability of establishing system-level performance and characteristics of fission surface power technologies without requiring a nuclear reactor. While some component and subsystem testing will continue through 2011 and beyond, the results to date provide sufficient confidence to proceed with system level technology readiness demonstration. To demonstrate the system level readiness of fission surface power in an operationally relevant environment (the primary goal of the Fission Surface Power Systems project), a full scale, 1/4 power Technology Demonstration Unit (TDU) is under development. The TDU will consist of a non-nuclear reactor simulator, a sodium-potassium heat transfer loop, a power conversion unit with electrical controls, and a heat rejection system with a multi-panel radiator assembly. Testing is planned at the Glenn Research Center Vacuum Facility 6 starting in 2012, with vacuum and liquid-nitrogen cold walls to provide simulation of operationally relevant environments. A nominal two-year test campaign is planned including a Phase 1 reactor simulator and power conversion test followed by a Phase 2 integrated system test with radiator panel heat rejection. The testing is expected to demonstrate the readiness and availability of fission surface power as a viable power system option for NASA's exploration needs. In addition to surface power, technology development work within this project is also directly applicable to in-space fission power and propulsion systems.
机译:在计划探索月球,火星及其他地方的表面时,功率是至关重要的考虑因素。核电是一个重要的选择,特别是对于太阳光受限或环境条件艰巨(例如极冷,沙尘暴)的太阳系地区。美国宇航局和能源部通过开发和演示裂变表面动力系统技术,维持月球和火星裂变表面动力的选择权。裂变地面动力系统项目的重点是子规模组件和子系统的演示,以解决采用低风险,低成本方法进行地面任务的空间核动力方法的可行性。实验室对液态金属泵,反应堆控制鼓驱动器,功率转换,排热以及功率管理和分配技术的演示证明,这些组件和子系统的基本特征和性能与裂变表面功率初步参考概念一致。此外,已经建立了使用电阻加热代替反应堆燃料的无核反应堆模拟器的小规模版本,并与液态金属钠钾和氦/氙气传热回路一起运行,证明了建立系统的可行性不需要核反应堆的裂变表面功率技术的高水平性能和特征。尽管某些组件和子系统测试将持续到2011年及以后,但迄今为止的结果为继续进行系统级技术就绪演示提供了足够的信心。为了证明在操作相关的环境中(裂变表面动力系统项目的主要目标)裂变表面动力的系统级准备水平,正在开发一个全尺寸的1/4功率技术演示装置(TDU)。 TDU包括一个无核反应堆模拟器,一个钠钾传热回路,一个带电气控制的功率转换单元以及一个带有多面板散热器组件的散热系统。计划从2012年开始在Glenn研究中心6号真空装置进行测试,该装置的真空和液氮冷壁可提供与操作相关的环境的模拟。计划进行为期两年的名义测试活动,包括阶段1反应堆模拟器和功率转换测试,然后进行阶段2集成系统测试和散热器面板散热。预期该测试将证明裂变表面功率已经准备就绪,并且可以作为满足NASA勘探需求的可行动力系统选择。除了地面动力,该项目内的技术开发工作也直接适用于空间裂变动力和推进系统。

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