• Journal of Astronomy and Space Sciences
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• v.17 no.1
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• pp.67-76
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• 2000

Far-ultraviolet IMaging Spectrograph(FIMS) is the main payload of the first Korean scientific satellite, KAISTSTA-4, which will be launched in 2002. The optical system of FIMS consists of parabolic cylinder mirror, slit, ellipsoidal reflection grating, and MCP to get spatial information as well as spectral information. Allowed ranges of manufacturing and positioning error are derived for each optical components to achieve the astronomical goals. In the procedure, graphical simplification is dedicated to understand sensitivity table and to derive range and precision of manipulation for each optical component. The result shows that precision of ${\mu}m$ for linear and of 2' for angular manipulation fulfills optical requirements.

• Bulletin of the Korean Space Science Society
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• 2000.10a
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• pp.22-22
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• 2000

No Abstract, See Full Text

• The Bulletin of The Korean Astronomical Society
• /
• v.34 no.2
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• pp.77.2-77.2
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• 2009

• The Bulletin of The Korean Astronomical Society
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• v.30 no.1
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• pp.70.2-70.2
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• 2005

• The Bulletin of The Korean Astronomical Society
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• v.26 no.1
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• pp.41-41
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• 2001

• The Bulletin of The Korean Astronomical Society
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• v.27 no.2
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• pp.37-37
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• 2002

• The Bulletin of The Korean Astronomical Society
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• v.28 no.1
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• pp.28-28
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• 2003

• The Bulletin of The Korean Astronomical Society
• /
• v.26 no.2
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• pp.29.2-29.2
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• 2001

• The Bulletin of The Korean Astronomical Society
• /
• v.26 no.2
• /
• pp.55.2-55.2
• /
• 2001

• The Bulletin of The Korean Astronomical Society
• /
• v.26 no.2
• /
• pp.28-28
• /
• 2001