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Design issues for a mission to exploit the gravitational lensing effect at 550 AU

Publication ,  Journal Article
West, JL
Published in: Acta Astronautica
January 1999

Reported herein are the first results of a NASA-sponsored study at the Jet Propulsion Laboratory (JPL), California Institute of Technology, exploring the scientific promise and technological viability of a mission to exploit the gravitational lensing effect of the Sun to obtain huge antenna gains for electromagnetic waves grazing the Sun's disk. With regard to scientific promise, these results, reported at about the halfway point of the study, substantiate the huge antenna gains offered by, as it will be called here, a Solar Gravitational Telescope (SGT) and point to the instrument's potential promise as a ``discovery machine'' but suggest considerable limitations to the telescope's usefulness as a general purpose astrophysical research tool. These limitations are seen to arise, primarily, from the geometry and scale of the ``virtual'' telescope which must be achieved and maintained to utilize the lensing effect and the turbulence effects of the Sun's plasma on the observed target's signal. With regard to technological viability, the preliminary results suggest a very aggressive use of unproven, as-yet-unflown new technology will be required to enable the desired science observations and mission durations approaching the short (3-10 year) NASA-targeted mission duration goal. Key needed new technologies are advanced propulsion, lightweight telescopes, membrane mirrors, inflatable/rigidizeable structures, and novel coronagraphic techniques. (C) 1999 Published by Elsevier Science Ltd. All rights reserved.

Published In

Acta Astronautica

DOI

ISSN

0094-5765

Publication Date

January 1999

Volume

44

Issue

2-4

Start / End Page

99 / 107

Related Subject Headings

  • Aerospace & Aeronautics
  • 0913 Mechanical Engineering
  • 0901 Aerospace Engineering
 

Citation

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ICMJE
MLA
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West, J. L. (1999). Design issues for a mission to exploit the gravitational lensing effect at 550 AU. Acta Astronautica, 44(2–4), 99–107. https://doi.org/10.1016/S0094-5765(99)00034-X
West, J. L. “Design issues for a mission to exploit the gravitational lensing effect at 550 AU.” Acta Astronautica 44, no. 2–4 (January 1999): 99–107. https://doi.org/10.1016/S0094-5765(99)00034-X.
West JL. Design issues for a mission to exploit the gravitational lensing effect at 550 AU. Acta Astronautica. 1999 Jan;44(2–4):99–107.
West, J. L. “Design issues for a mission to exploit the gravitational lensing effect at 550 AU.” Acta Astronautica, vol. 44, no. 2–4, Jan. 1999, pp. 99–107. Manual, doi:10.1016/S0094-5765(99)00034-X.
West JL. Design issues for a mission to exploit the gravitational lensing effect at 550 AU. Acta Astronautica. 1999 Jan;44(2–4):99–107.
Journal cover image

Published In

Acta Astronautica

DOI

ISSN

0094-5765

Publication Date

January 1999

Volume

44

Issue

2-4

Start / End Page

99 / 107

Related Subject Headings

  • Aerospace & Aeronautics
  • 0913 Mechanical Engineering
  • 0901 Aerospace Engineering