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Chemical launch system options for microspacecraftThe paper presents launch vehicle and upper-stage options for application to lunar and interplanetary microspacecraft missions. Particular attention is given to the capabilities of Piggyback, small launch vehicles, and large launch vehicles. It is noted that Piggyback options on the Shuttle and expendable launch vehicles enable near-term earth-orbital missions and the potential for lunar and planetary missions if an electric-propulsion upper-stage is developed. Launch systems like the Space Shuttle could be used to launch large members of microspacecraft in 'constellation deployment' and 'shotgun' class missions to a variety of solar-system targets such as the sun, asteroids, comets, the moon, Mars, and Saturn.
Document ID
19900024904
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Sargent, Mark G.
(California Institute of Technology Jet Propulsion Laboratory, Pasadena, United States)
Date Acquired
August 14, 2013
Publication Date
October 1, 1989
Publication Information
Publication: British Interplanetary Society, Journal
Volume: 42
ISSN: 0007-084X
Subject Category
Astronautics (General)
Accession Number
90A11959
Distribution Limits
Public
Copyright
Other

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