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Solar Polar Sail mission: report of a study to put a scientific spacecraft in a circular polar orbit about the sun

Goldstein, Bruce E. and Buffington, Andrew and Cummings, Alan C. and Fisher, Richard R. and Jackson, Bernard V. and Liewer, Paulett C. and Mewaldt, Richard A. and Neugebauer, Marcia (1998) Solar Polar Sail mission: report of a study to put a scientific spacecraft in a circular polar orbit about the sun. In: Missions to the Sun II. Proceedings of SPIE. No.3442. Society of Photo-optical Instrumentation Engineers (SPIE) , Bellingham, WA, pp. 65-76. ISBN 9780819428974. http://resolver.caltech.edu/CaltechAUTHORS:20181109-093937080

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Abstract

The Solar Polar Sail Mission uses solar-sail propulsion to place a spacecraft in a circular orbit 0.48 Au from the Sun with an inclination of 90 degrees. The spacecraft's orbit around the Sun is in 3:1 resonance with Earth phased such that the Earth-Sun-spacecraft angle range from 30 degrees to 150 degrees. The polar view will further our understanding of: (1) the global structure and evolution of the corona, (2) the initiation, evolution, and propagation of coronal mass ejections; (3) the acceleration of the solar wind; (4) the interactions of rotation, magnetic fields, and convection within the Sun; (5) the acceleration and propagation of energetic particles; and (6) the rate of angular momentum loss by the Sun. Candidate imaging instruments are a coronagraph, an all-sky imager for following mass ejections and interaction regions from the Sun to 1 AU, and a disk imager. A lightweight package of fields and particle instruments is included. A mission using a 158 m square sail with an effective areal density of 6 g/m^2 would cost approximately $250-300M (FY97) for all mission phases, including the launch vehicle. This mission depends on the successful development and demonstration of solar-sail propulsion.


Item Type:Book Section
Related URLs:
URLURL TypeDescription
https://doi.org/10.1117/12.330265DOIArticle
Additional Information:© 1998 Society of Photo-optical Instrumentation Engineers (SPIE). Engineering support was provided to the study by R. A. Wallace, J. Ayon, C. E. Garner, C. Sauer, C.-W. Yen, and the Advanced Projects Design Team (Team X) led by R. Bennett. A portion of this work was conducted at the Jet Propulsion Laboratory, California Institute of Technology, under contract with the National Aeronautics and Space Administration.
Group:Space Radiation Laboratory
Funders:
Funding AgencyGrant Number
NASA/JPL/CaltechUNSPECIFIED
Subject Keywords:solar sail, sail, solar wind, spacecraft, solar polar orbit, corona
Record Number:CaltechAUTHORS:20181109-093937080
Persistent URL:http://resolver.caltech.edu/CaltechAUTHORS:20181109-093937080
Official Citation:Bruce E. Goldstein, Andrew Buffington, Alan C. Cummings, Richard R. Fisher, Bernard V. Jackson, Paulett C. Liewer, Richard A. Mewaldt, Marcia Neugebauer, } "Solar Polar Sail mission: report of a study to put a scientific spacecraft in a circular polar orbit about the sun", Proc. SPIE 3442, Missions to the Sun II, (2 November 1998); doi: 10.1117/12.330265; https://doi.org/10.1117/12.330265
Usage Policy:No commercial reproduction, distribution, display or performance rights in this work are provided.
ID Code:90789
Collection:CaltechAUTHORS
Deposited By: Tony Diaz
Deposited On:13 Nov 2018 18:18
Last Modified:13 Nov 2018 18:18

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