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Looking at the architectureArchitectural and systems-engineering considerations and tradeoffs are primary design-drivers in Martian and lunar missions, entailing studies of such fundamental choices as the use of rapid trajectories in the course of which crews live in zero-g or slower trajectories in which crews are subjected to artificial gravity. The best use of transportation way-points, the integration of launch vehicles with spacecraft of various configurations, and the incorporation of such advanced concepts as solar sail propulsion, are additional considerations to be studied. The planning of lunar and Martian missions must always take into account the extent to which local resources can diminish earth-supplied logistics requirements.
Document ID
19890046549
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Bekey, Ivan
(NASA Office of Exploration Washington, DC, United States)
Date Acquired
August 14, 2013
Publication Date
April 1, 1989
Publication Information
Publication: Aerospace America
Volume: 27
ISSN: 0740-722X
Subject Category
Astronautics (General)
Report/Patent Number
ISSN: 0740-722X
Accession Number
89A33920
Distribution Limits
Public
Copyright
Other

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