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Coma and tail trajectory design for the CRAF missionThe design of the trajectory for the proposed Comet Rendezvous Asteroid Flyby (CRAF) mission to study comet coma and tail development is examined. A two part trajectory is planned for the CRAF mission to study comet Kopff. It is proposed that, during the 213 day perihelion phase of the trajectory, CRAF should perform multiple petallike flybys at 50-5000 km from the comet's nucleus. Nine days after the perihelion, the spacecraft would transition into the comet tail in the antisun direction to a maximum distance of 50,000 km. The objectives of these two phases of exploration are discussed.
Document ID
19900056481
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Ionasescu, Rodica
(JPL Pasadena, CA, United States)
Date Acquired
August 14, 2013
Publication Date
January 1, 1989
Subject Category
Astrodynamics
Report/Patent Number
AAS PAPER 89-208
Meeting Information
Meeting: AAS/NASA Intl. Symposium on Orbital Mechanics and Mission Design
Location: Greenbelt, MD
Country: United States
Start Date: April 24, 1989
End Date: April 27, 1989
Accession Number
90A43536
Distribution Limits
Public
Copyright
Other

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