Optics for the Columbus Project Telescope
J. M. Hill
Steward Observatory, University of Arizona
Columbus Project Technical Memo
UA-92-01
June 8, 1992
presented at the Columbus, Ohio AAS meeting
http://medusa.as.arizona.edu/lbtwww/tech/ua9201.htm
Abstract
The Columbus Project telescope is a 2 x 8.4 meter binocular
instrument being built by the University of Arizona and the
Osservatorio Astrofisico di Arcetri. Dual 8.4 meter borosilicate
honeycomb primary mirrors provide an equivalent collecting area of
11.8 meters. With a focal ratio of F/1.14, these primaries will
permit a very compact and stiff telescope structure. The combined
focus provides an interferometric baseline of 22.8 meters on a common
mount. The phased focus provides a coherent field-of-view up to 6
arcminutes in diameter at F/33. In addition to a central focus for
interferometry, the telescope will be instrumented with dual
Cassegrain focal stations at F/5 and F/15. The F/5 foci will be
optimized for wide field work in the optical and near-infrared. The
1.96 m diameter secondaries provide a naked Cassegrain focus at F/5.2.
A three-element refractive corrector provides a 50 arcminute
field-of-view at F/5.4. This wide field will be used for multiobject
spectroscopy as well as wide field imaging and long-slit spectroscopy.
The F/15 foci will be optimized for work at mid- and thermal infrared
wavelengths with approximately a 10 arcminute field-of-view. The
infrared foci will be used for imaging and spectroscopy over a wide
wavelength range. The 0.74 m diameter secondaries will have chopping
and rapid guiding capabilities. Adaptive optics will also play a key
role in the telescope operation. Tertiary flats will provide bent
Cassegrain focal stations. Secondaries which are not in use will be
stored in the center of the telescope structure allowing for rapid
interchange during the night. The error budget for the optics and the
telescope will attempt to match the wavefront provided by an r0 =
45 cm atmosphere.
Columbus Project --- Optics for the Second Voyage
- optical configuration ------- binocular 8.4 meter apertures
- equivalent aperture --------- 11.8 meters
- collecting area --------- 2 * 55 m 2 (3500 C8's)
- interferometric baseline --------- 22.8 meters
- resolution (
/ D) in the visible --------- 5 milliarcsec
- primary mirrors --------- 8.4 meter F/1.14 borosilicate honeycomb
- world's most powerful common mount telescope
- consortium partners:
- University of Arizona
- Italy --- Osservatorio Astrofisico di Arcetri
- Research Corporation
- mounting type --------- dual ring platform (altitude -- azimuth)
- moving mass --------- 400 metric tons
- site --------- Mt. Graham, Arizona (near Emerald Peak, 3140 m)
Primary Mirrors
- Number of Primary Mirrors: 2
- Primary Spacing: 14.408 meters center-to-center
- Primary Glass Diameter: 8.417 meters
- Primary Clear Aperture: 8.408 meters
- Primary Focal Ratio: F/1.142
- Central Hole Diameter: 1.0 meter
- Primary Figure: parabolic
- Primary Construction
- cast borosilicate honeycomb
- 28 mm faceplate thickness
- edge thickness 894 mm, plano-concave
- Primary Mirror Mass: approximately 14.5 metric tons each
Focal Stations
- Cassegrain, optical, dual F/5.4
- Cassegrain, infrared, dual F/15
- phased combined, F/33 (moving, 4 mirrors)
- bent Cassegrain, dual front, F/5 or F/15
- phased coud è, F/33 (gravity fixed, 6 mirrors, optional)
- bent Cassegrain, dual rear (optional)
- versatile array feed (optional)
- prime (optional)

Figure 1: Telescope Optical Layout for Wide Field Dual Cassegrain at F/5.2.
A three element refractive corrector provides a 50 arcminute field of view.
Two 8.4 meter mirrors provide an interferometric baseline of 22.8 meters.
Secondary Complement
- optical Cassegrain, F/5.17 (naked)
- interchange: trolley
- mirror diameter: 1.96 m
- field-of-view: 50 arcminutes (corrected)
- baffle diameter: 2.55 m
- infrared Cassegrain, F/15
- interchange: flip-top
- mirror diameter: 0.738 m (1% undersized)
- field-of-view: ~10 arcminutes (vignetted)
- combined beam, F/33 (possibly adaptive)
- interchange: flip-top
- mirror diameter: 0.828 m
- field-of-view: 6 arcminutes (unvignetted)
- interferometric baseline 22.816 m
Other Optics
- tertiary flats (2)
- interchange: trolley, articulated
- minor axis diameter: 75 cm (or 94 cm)
- location: 2.5 m above primary vertex
- beam combiners (2)
- interchange: fixed
- minor axis diameter: 63 cm
- wide field correctors
- small field correctors

Figure 2: Three Element Refractive Corrector for Wide Field Cassegrain.
This corrector was designed by Domenico Bonaccini at the Osservatorio
Astrofisico di Arcetri. It contains three all spherical fused silica
elements. 80% of the energy is concentrated with 0.25 arcsecond in
the inner 40 arcminutes of the field. This degrades to 0.86 arcsecond
over the full 50 arcminute diameter field. This could be improved by
adding one aspheric surface. The corrector works over a wavelength
range of 0.33 to 1.1 microns. The corrector may be used with or
without a pair of counter-rotating prisms to correct atmospheric
dispersion. The focal plane has a 5 meter radius of curvature.
Instrument Mounting Clearances
- Maximum Instrument Diameter: 3.0 meters
- Diameter of Instruments longer than 2.3 meters: 2.4 meters
- Maximum Instrument Length: 3.5 meters below the focal plane
- Bent Cassegrain Instruments: ~2 meters diameter, ~ 2.5 meters long
- Clearance for Coudè Optical Beam: 1 meter at zenith angle less than 60 degrees
Error Budget
The error budget for the total telescope is 0.225 arcsec FWHM which
corresponds to an r0 = 45 cm atmosphere at 0.5 microns. This has
been divided as follows:
- Tracking and Drives = 0.070 arcsec FWHM
- Optical Alignment and Focus = 0.084 arcsec FWHM
- Optical Design = 0.070 arcsec FWHM
- Optical Surfaces = 0.175 arcsec FWHM
- Telescope Seeing (5% ) = 0.056 arcsec FWHM
Telescope Structure and Enclosure
- Telescope Structure: model A', platform design
- Support Spacing: 2 ``C'' rings on 10 meter centers
- Pier Diameter: 13 meters for azimuth track
- Telescope Height: 20 - 25 meters at elevation axis
- Building Height: 35 - 40 meters at roofline
- Support of Telescope: hydrostatic pads
- Drive Mechanism: gear and pinion
- Telescope and Drive Stiffness Goal: locked rotor frequency >8 Hz
- Vibration Specification: < 0.025 µ m amplitude above 8 Hz
- Encoders: strip type
- Telescope Moment of Inertia: approximately 1*10 7 Kg m 2 (both axes)
- Telescope Mass: approximately 380 metric tons
- Maximum Angular Speed: 1.5 degrees/second
- Maximum Angular Acceleration: 0.3 degrees/second 2
- Error Budget: telescope and optics to match r0 = 45 cm atmosphere
- Implied Image Size from Telescope = 0.22 arcsecond FWHM
- Short Term Tracking Specification: 0.03 arcsecond rms (5 seconds)
- Whole Sky Pointing Specification: 0.3 arcsecond rms
- Wind Speed for Pointing and Tracking Specs: 24 km/hr
- Maximum Operating Wind Speed: 80 km/hr
- Survival Wind Speed (closed): 225 km/hr
- Primary Mirror Aluminizing: on-board the telescope

Figure 3: Design of the Two-Shooter Telescope Structure. This drawing
was done by the engineering firm ADS Italia. The dual ring elevation
support allows a structural resonant frequency of 9--10 Hz.

Figure 4: Design of the Two-Shooter Telescope Enclosure. This drawing
was done by the engineering firm ADS Italia. The enclosure is a corotating
box with two portal shutters. Openings in the front, sides and rear allow
good ventilation to assure thermal equilibrium. A large elevator on the
ground provides access to the observing chamber for instruments and other
heavy equipment. Functions which produce heat are isolated in the lowest level
of the rotating section.