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FPGA development for high altitude subsonic parachute testing

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dc.contributor.author Kowalski, James E.
dc.contributor.author Konefat, Edward H. en_US
dc.contributor.author Gromovt, Konstantin en_US
dc.date.accessioned 2005-10-11T19:42:01Z
dc.date.available 2005-10-11T19:42:01Z
dc.date.issued 2005-09
dc.identifier.citation Military and Aerospace Programmable Logic Device International Conference, Washington D. C., September 7-9, 2005 en
dc.identifier.clearanceno 05-2214
dc.identifier.uri http://hdl.handle.net/2014/37670
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 store data from multiple sensors at multiple rates during launch, ascent, deployment and descent phases of the subsonic parachute test. en
dc.description.sponsorship NASA en
dc.format.extent 657938 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 FPGA development for high altitude subsonic parachute testing en
dc.type Presentation en


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