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High altitude subsonic parachute field programmable gate array

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dc.contributor.author Kowalski, James E.
dc.contributor.author Gromov, Konstantin
dc.contributor.author Konefat, Edward H.
dc.date.accessioned 2005-11-11T23:10:36Z
dc.date.available 2005-11-11T23:10:36Z
dc.date.issued 2005-06
dc.identifier.citation Military and Aerospace Programmable Logic Device International Conference, Washington D. C., September 7-9, 2005 en
dc.identifier.clearanceno 05-1608
dc.identifier.uri http://hdl.handle.net/2014/38072
dc.description.abstract This paper describes a rapid, top down requirements-driven design of an FPGA used in an Earth qualification test program for a new Mars subsonic parachute. The FPGA is used to process and control storage of telemetry data from multiple sensors throughout; launch, ascent, deployment and descent phases of the subsonic parachute test. en
dc.description.sponsorship NASA en
dc.format.extent 662859 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US en
dc.publisher Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2005. en
dc.subject FPGA methodology en
dc.subject telemetry en
dc.title High altitude subsonic parachute field programmable gate array en
dc.type Presentation en


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