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Encke flyby science packageCometary exploration objectives are considered, giving attention to reasons for the selection of Encke as a target for early exploration missions. An Encke environmental model is discussed together with the scientific requirements of an exploratory mission, instrument selection criteria, and the science payload. The instruments to be used include a television camera, an IR radiometer, a UV spectrometer, a mass spectrometer, a Sisyphus dust detector, devices for the measurement of the EM field, and instruments for the determination of plasma characteristics. It is pointed out that solar electric propulsion affords the only practical, currently available means of reaching Encke with the desired encounter velocity below 7.5 km/sec.
Document ID
19740027949
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Newburn, R. L.
(California Institute of Technology, Jet Propulsion Laboratory, Space Sciences Div., Pasadena Calif., United States)
Weddell, J. B.
(Rockwell International Corp. Space Div., Downey, Calif., United States)
Date Acquired
August 7, 2013
Publication Date
October 1, 1973
Subject Category
Space Sciences
Report/Patent Number
AIAA PAPER 73-1125
Report Number: AIAA PAPER 73-1125
Meeting Information
Meeting: Electric Propulsion Conference
Location: Lake Tahoe, NV
Start Date: October 31, 1973
End Date: November 2, 1973
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
74A10699
Funding Number(s)
CONTRACT_GRANT: NAS7-100
CONTRACT_GRANT: NAS8-27360
Distribution Limits
Public
Copyright
Other

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