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Development and flight experience of the Voyager propulsion systemThe primary Voyager Project objective is to extend the exploration of the solar system to the neighborhood of Jupiter and Saturn with a spacecraft that can conduct scientific experiments at both planetary systems and pave the way for later missions to the outer planets. The development and in-flight performance of the Voyager propulsion system are described. Emphasis is placed on the unique features of this system and on the solution to several problems encountered in its development. Over the past 20-month flight, the propulsion systems on Voyager I and Voyager II have exhibited excellent performance without failures.
Document ID
19790055030
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Schatz, W. J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cannova, R. D.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cowley, R. T.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Evans, D. D.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
June 1, 1979
Subject Category
Spacecraft Propulsion And Power
Report/Patent Number
AIAA PAPER 79-1334
Report Number: AIAA PAPER 79-1334
Meeting Information
Meeting: AIAA, SAE, and ASME, Joint Propulsion Conference
Location: Las Vegas, NV
Start Date: June 18, 1979
End Date: June 20, 1979
Sponsors: AIAA, ASME, SAE
Accession Number
79A39043
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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