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Systems design study of the Pioneer Venus spacecraft. Volume 1: Technical analyses and tradeoffs, sections 8-12 (part 4 of 4)The probe bus and orbiter subsystems are defined, and tradeoffs analyzed. Subsystems discussed include: communications, electric power, data handling, attitude determination and control, propulsion, thermal control, structure and mechanisms, NASA/ESRO orbiter interface, mission operation, and flight support.
Document ID
19740024194
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Date Acquired
September 3, 2013
Publication Date
July 29, 1973
Subject Category
Space Vehicles
Report/Patent Number
NASA-CR-137507
TRW-2291-6008-RU-00
Accession Number
74N32307
Funding Number(s)
CONTRACT_GRANT: NAS2-7249
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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