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Circulating transportation orbits between earth and MarsThis paper describes the basic characteristics of circulating (cyclical) orbit design as applied to round-trip transportation of crew and materials between earth and Mars in support of a sustained manned Mars Surface Base. The two main types of nonstopover circulating trajectories are the socalled VISIT orbits and the Up/Down Escalator orbits. Access to the large transportation facilities placed in these orbits is by way of taxi vehicles using hyperbolic rendezvous techniques during the successive encounters with earth and Mars. Specific examples of real trajectory data are presented in explanation of flight times, encounter frequency, hyperbolic velocities, closest approach distances, and Delta V maneuver requirements in both interplanetary and planetocentric space.
Document ID
19860063167
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Friedlander, A. L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Niehoff, J. C.
(Science Applications International Corp. Schaumburg, IL, United States)
Byrnes, D. V.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Longuski, J. M.
(California Institute of Technology Jet Propulsion Laboratory, Pasadana, United States)
Date Acquired
August 12, 2013
Publication Date
January 1, 1986
Subject Category
Astrodynamics
Report/Patent Number
AIAA PAPER 86-2009
Accession Number
86A47905
Funding Number(s)
CONTRACT_GRANT: JPL-957404
CONTRACT_GRANT: NAS7-918
CONTRACT_GRANT: NASW-3622
Distribution Limits
Public
Copyright
Other

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