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Exploration of PlutoTwo NASA-sponsored cost-constrained mission implementations for the exploration of Pluto are described. One is the Pluto Fast Flyby (PFF) mission, which utilizes an 83 kg spacecraft to be launched in 1998 aboard a Titan IV (Solid Rocket Motor Upgrade)/Centaur) for an about 7-year-long direct trajectory to Pluto, which will carry an integrated CCD-imaging/UV spectrometer, with a possible integrated IR spectrometer. The other is the Pluto-350 spacecraft, weighing about 316 kg, which will carry a broader instrument set, greater redundancy, and which will require greater than 11 year flight time. Pluto-350 will be launched in 2001 aboard a Delta or Atlas, toward earth and Jupiter swingbys to provide the energy to reach Pluto.
Document ID
19920073233
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Staehle, Robert L.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Abraham, Douglas S.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Carraway, John B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Esposito, Paul J.
(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)
Terrile, Richard J.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Wallace, Richard A.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Weinstein, Stacy S.
(JPL Pasadena, CA, United States)
Hansen, Elaine
(Colorado, University Boulder, United States)
Date Acquired
August 15, 2013
Publication Date
August 1, 1992
Subject Category
Lunar And Planetary Exploration
Report/Patent Number
IAF PAPER 92-0558
Report Number: IAF PAPER 92-0558
Accession Number
92A55857
Distribution Limits
Public
Copyright
Other

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