Publication Date:
2019-07-13
Description:
The paper presents the results of the first stage of a Mercury Orbiter Mission Concept Definition study originated by NASA, with emphasis on a proposed end-to-end mission scenario. The science rationale and the strawman payload are presented, along with the spacecraft design based on a novel use of conventional technology that eliminates the need for high-cost high-risk technology development. A mission scenario demonstrating the capability of conducting desired science investigations is addressed. It is shown that complete imaging coverage of the planet at 1-km or better resolution, and with at least three different phase angles, is possible. Focus is placed on launch period analysis, mission performance, and mission opportunities.
Keywords:
ASTRODYNAMICS
Type:
AAS PAPER 89-195
,
AAS/NASA Intl. Symposium on Orbital Mechanics and Mission Design; Apr 24, 1989 - Apr 27, 1989; Greenbelt, MD; United States
Format:
text
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