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Microspacecraft technology for planetary science missionsA summary is presented of the technology that may enable a microspacecraft, whose mass is on the order of 10 kg, to perform smaller, faster, and more frequent planetary science missions. Some of JPL's activities in microspacecraft are discussed including the benefits of microspacecraft technology to a Mars Rover sample return mission and the conceptual design of a microspacecraft to examine near earth asteroids. Major technology items allowing the decrease in system mass include lightweight carbon-carbon and other composite structural materials and microsensors and instruments.
Document ID
19920029844
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Jones, Ross M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Salvo, Christopher G.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
October 1, 1991
Subject Category
Spacecraft Design, Testing And Performance
Report/Patent Number
IAF PAPER 91-051
Report Number: IAF PAPER 91-051
Accession Number
92A12468
Distribution Limits
Public
Copyright
Other

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