タイトル | Reactor Simulator Testing Overview |
本文(外部サイト) | http://hdl.handle.net/2060/20130011206 |
著者(英) | Schoenfeld, Michael P. |
著者所属(英) | NASA Marshall Space Flight Center |
発行日 | 2013-02-25 |
言語 | eng |
内容記述 | OBJECTIVE: Integrated testing of the TDU components TESTING SUMMARY: a) Verify the operation of the core simulator, the instrumentation and control system, and the ground support gas and vacuum test equipment. b) Thermal test heat regeneration design aspect of a cold trap purification filter. c) Pump performance test at pump voltages up to 150 V (targeted mass flow rate of 1.75 kg/s was not obtained in the RxSim at the originally constrained voltage of 120 V). TESTING HIGHLIGHTS: a) Gas and vacuum ground support test equipment performed effectively for NaK fill, loop pressurization, and NaK drain operations. b) Instrumentation and control system effectively controlled loop temperature and flow rates or pump voltage to targeted settings. c) Cold trap design was able to obtain the targeted cold temperature of 480 K. An outlet temperature of 636 K was obtained which was lower than the predicted 750 K but 156 K higher than the cold temperature indicating the design provided some heat regeneration. d) ALIP produce a maximum flow rate of 1.53 kg/s at 800 K when operated at 150 V and 53 Hz. |
NASA分類 | Nuclear Physics |
レポートNO | M13-2447 |
権利 | No Copyright |
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