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Solar system 'fast mission' trajectories using aerogravity assistInitial analyses of the aerogravity assist (AGA) delivery technique to solar system targets (and beyond) has been encouraging. Mission opportunities are introduced that do not exist with typical gravity assist trajectories and current launch capabilities. The technique has the most payoff for high-energy missions such as outer planet orbiters and flybys. The goal of this technique is to reduce the flight duration significantly and to eliminate propulsion for orbit insertion. The paper will discuss detailed analyses and parametric studies that consider launch opportunities for missions to the sun, Saturn, Uranus, Neptune, and Pluto using AGA at Venus and Mars.
Document ID
19920049562
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Randolph, James E.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mcronald, Angus D.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
April 1, 1992
Publication Information
Publication: Journal of Spacecraft and Rockets
Volume: 29
ISSN: 0022-4650
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 91-0531
Accession Number
92A32186
Distribution Limits
Public
Copyright
Other

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