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A data acquisition and storage system for the ion auxiliary propulsion system cyclic thruster testA nine-track tape drive interfaced to a standard personal computer was used to transport data from a remote test site to the NASA Lewis mainframe computer for analysis. The Cyclic Ground Test of the Ion Auxiliary Propulsion System (IAPS), which successfully achieved its goal of 2557 cycles and 7057 hr of thrusting beam on time generated several megabytes of test data over many months of continuous testing. A flight-like controller and power supply were used to control the thruster and acquire data. Thruster data was converted to RS232 format and transmitted to a personal computer, which stored the raw digital data on the nine-track tape. The tape format was such that with minor modifications, mainframe flight data analysis software could be used to analyze the Cyclic Ground Test data. The personal computer also converted the digital data to engineering units and displayed real time thruster parameters. Hardcopy data was printed at a rate dependent on thruster operating conditions. The tape drive provided a convenient means to transport the data to the mainframe for analysis, and avoided a development effort for new data analysis software for the Cyclic test. This paper describes the data system, interfacing and software requirements.
Document ID
19890008053
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Hamley, John A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1989
Subject Category
Computer Systems
Report/Patent Number
NASA-TM-101469
E-4583
NAS 1.15:101469
Report Number: NASA-TM-101469
Report Number: E-4583
Report Number: NAS 1.15:101469
Accession Number
89N17424
Funding Number(s)
PROJECT: RTOP 506-48-91
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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