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Data link relay designThe data link for the Ames baseline probe as applied to the MJU spacecraft specifically with an entry at Uranus is analyzed. A frequency analysis, a trajectory analysis, and a discussion of the effects on the spacecraft design by the data link are presented. The possibilities of a two-way link are considered.
Document ID
19750012323
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Parsons, P. (Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1974
Publication Information
Publication: Dynatrend, Inc. Proc. of Outer Planet Probe Technol. Workshop, Sect. 1 through 11
Subject Category
Communications And Radar
Accession Number
75N20395
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

IDRelationTitle19750012286Collected WorksProceedings of Outer Planet Probe Technology Workshop, Sections I Through IV
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