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New concepts for Mercury orbiter missionsThe next logical step in the exploration of Mercury is an orbiter mission. A conflict exists between those in the field of planetary sciences who desire a mission with a low circular orbit, and scientists in the fields and particles disciplines, who generally prefer a highly elliptical spacecraft orbit. The thermal environment imposed by the sun and planet render the low orbit intolerable for spacecraft using previous thermal control methods. A thermal control concept and a spacecraft mission concept have been developed which resolve these problems and promise a scientifically significant mission for the mid-1980s.
Document ID
19780036765
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
French, J. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Stuart, J. R.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Zeldin, B.
(California Institute of Technology, Jet Propulsion Laboratory, Pasadena Calif., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1978
Subject Category
Lunar And Planetary Exploration
Report/Patent Number
AIAA PAPER 78-79
Meeting Information
Meeting: Aerospace Sciences Meeting
Location: Huntsville, AL
Start Date: January 16, 1978
End Date: January 18, 1978
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
78A20674
Distribution Limits
Public
Copyright
Other

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