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Planetary missions using microspacecraft technologySome of the planetary missions using microspacecraft of mass on the order of 10 kg which are presently being considered at JPL are discussed. The primary benefits offered by this type of spacecraft is the small and relatively inexpensive launch vehicles and short program development schedules. A mission presently considered by the Asteroid Investigation with Microspacecraft (AIM) study is described with special attention given to the spacecraft configuration; the AIM mission will launch three spacecraft from a single Pegasus vehicle, achieving separate flybys for three near-earth asteroids. Attention is also given to the salient features of the Mars Rover Sample Return mission, the Venus Atmospheric Sounder, and the Comet Nucleus Mission, for which the application of microspacecraft technology is considered.
Document ID
19920074595
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Short, Kendra L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Jones, Ross M.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Salvo, Christopher G.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Mostert, Robert N.
(JPL Pasadena, CA, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Astronautics (General)
Report/Patent Number
IAF PAPER 92-0821
Report Number: IAF PAPER 92-0821
Accession Number
92A57219
Distribution Limits
Public
Copyright
Other

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