Space Telescope fine guidance - A design for manufacturability

Astronomy and Astrophysics – Astronomy

Scientific paper

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Guidance (Motion), Onboard Equipment, Optical Tracking, Pointing Control Systems, Spaceborne Telescopes, Astrometry, Design Analysis, Mirrors, Optical Paths, Optical Scanners, Space Missions, Space Shuttles

Scientific paper

The NASA Space Telescope (ST) is a 2.4-m aperture, f/24 Ritchey-Chretien telescope coupled to five on-board astronomical scientific packages. The very accurate line-of-sight stability required by ST during operating periods of up to 24 hours is maintained by the Pointing Control System whose optical system, the Fine Guidance Subsystem (FGS), is described. The Pointing Control System includes three identical FGSs, any two of which provide line-of-sight stabilization by tracking guide stars while the third performs astrometry. The optical system for the ST FGS performs the field aberration correction within the FGS near a pupil plane measuring only 52.7 mm. The design is simple and easily corrected, and offers substantial advantages over the traditional approach in terms of manufacturability.

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