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Ballistic comet exploration mission optionsTrajectory options and mission opportunities of cometary rendezvous missions begining in 1990 are explored. The study is constrained to the capabilities of the Mariner Mark II multi-mission spacecraft, Shuttle launch and Centaur G-prime boost. The mission would be targeted at collecting an atomized sample, near the comet perihelion, and returning the sample for analysis. Mission trajectories, launch dates, payload masses and flight durations are provided for 13 comets. All missions would take from 4-8 yr and deliver a 600-2000 kg payload. A survey of mission opportunities involving Jupiter gravity assists is also presented.
Document ID
19840061717
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Yen, C.-W. L.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena CA, United States)
Date Acquired
August 12, 2013
Publication Date
August 1, 1984
Subject Category
Astronautics (General)
Report/Patent Number
AIAA PAPER 84-2028
Report Number: AIAA PAPER 84-2028
Accession Number
84A44504
Distribution Limits
Public
Copyright
Other

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