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Initial Cassini propulsion system in-flight characterization

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dc.contributor.author Barber, T. J. en_US
dc.contributor.author Crowley, R. T. en_US
dc.date.accessioned 2004-09-17T05:15:59Z
dc.date.available 2004-09-17T05:15:59Z
dc.date.issued 2002-07-07 en_US
dc.identifier.citation 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibition en_US
dc.identifier.citation Indianapolis, IN, USA en_US
dc.identifier.clearanceno 02-1168 en_US
dc.identifier.uri http://hdl.handle.net/2014/8606
dc.description.abstract The Cassini Propulsion Module Subsystem has performed excellently throughout the first four years of mission operations. The PMS is the most complex interplanetary propulsion subsystem ever flown, with separate monopropellant and bipropellant propulsion modules, each replete with many redundant components. en_US
dc.format.extent 4915660 bytes
dc.format.mimetype application/pdf
dc.language.iso en_US
dc.subject.other Cassini propulsion performance mission operations in-flight en_US
dc.title Initial Cassini propulsion system in-flight characterization en_US


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