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    기술보고서 게시판 내용
    타이틀 Advanced Stirling Convertor Dynamic Test Approach and Results
    저자 Meer, David W.;; Hill, Dennis;; Ursic, Joseph J.
    Keyword ACCELEROMETERS;; DYNAMIC TESTS;; FLIGHT TESTS;; LAUNCHING;; PISTONS;; QUALITY CONTROL;; REFUELING;; SPACE MISSIONS;; STIRLING CYCLE;; VIBRATION;; VIBRATION TESTS
    URL http://hdl.handle.net/2060/20100017258
    보고서번호 NASA/CR-2010-216237
    발행년도 2010
    출처 NTRS (NASA Technical Report Server)
    ABSTRACT The U.S. Department of Energy (DOE), Lockheed Martin Corporation (LM), and NASA Glenn Research Center (GRC) have been developing the Advanced Stirling Radioisotope Generator (ASRG) for use as a power system for space science missions. As part of the extended operation testing of this power system, the Advanced Stirling Convertors (ASC) at NASA GRC undergo a vibration test sequence intended to simulate the vibration history that an ASC would experience when used in an ASRG for a space mission. This sequence includes testing at workmanship and flight acceptance levels interspersed with periods of extended operation to simulate prefueling and post fueling. The final step in the test sequence utilizes additional testing at flight acceptance levels to simulate launch. To better replicate the acceleration profile seen by an ASC incorporated into an ASRG, the input spectra used in testing the convertors was modified based on dynamic testing of the ASRG Engineering Unit (ASRG EU) at LM. This paper outlines the overall test approach, summarizes the test results from the ASRG EU, describes the incorporation of those results into the test approach, and presents the results of applying the test approach to the ASC-1 &#353 and &#354 convertors. The test results include data from several accelerometers mounted on the convertors as well as the piston position and output power variables.

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