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Solar electric propulsion combined with earth gravity assist - A new potential for planetary explorationThe need to shorten mission time (travel time to target planet) in missions to the outer planets prompts a search for alternatives to one-way minimum-energy transfers while continuing to minimize on-power thrusts. Gravity assists via swing-bys of inner planets are examined, with emphasis on a projected Venus-earth gravity assist (VEGA) and a combined solar electric propulsion and earth gravity assist (SEEGA). Gravity assists are also examined as essential for missions with sample returns back to earth. Possible use of such techniques in the Shuttle Interim Upper Stage (IUS) program is considered. Various SEEGA and VEGA trajectories are discussed and charted, and time lost in the launch orbit to earth re-encounter time is weighed against time gained by faster speed toward the mission destination.
Document ID
19760060148
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Atkins, K. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sauer, C. G.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Flandro, G. A.
(Utah, University Salt Lake City, Utah, United States)
Date Acquired
August 8, 2013
Publication Date
August 1, 1976
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 76-807
Meeting Information
Meeting: Astrodynamics Conference
Location: San Diego, CA
Start Date: August 18, 1976
End Date: August 20, 1976
Sponsors: American Institute of Aeronautics and Astronautics and American Astronautical Society
Accession Number
76A43114
Funding Number(s)
CONTRACT_GRANT: NAS7-100
Distribution Limits
Public
Copyright
Other

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