The Large Binocular Telescope Project
J. M. Hill, Steward Observatory
Large Binocular Telescope Project
Technical Memo
UA-95-01
February 23, 1995
presented at January 1995 AAS meeting as poster 10.06
http://medusa.as.arizona.edu/lbtwww/tech/ua9501.htm

Figure 1: Conceptual rotating enclosure for the LBT.
Contents:
Abstract
LBT Summary
LBT Project Status
Optical Design Drivers
Baseline Focal Stations
Telescope Structure
Telescope Enclosure
Abstract
The Large Binocular Telescope (LBT) Project has evolved from concepts
first proposed in 1985. The present partners involved in the design
and construction of this 2 x 8.4 meter binocular telescope are the
University of Arizona, Italy represented by the Osservatorio
Astronomico di Arcetri and the Research Corporation based in Tucson.
These three partners have committed sufficient funds to build the
enclosure and the telescope populated with a single 8.4 meter optical
train --- approximately 40 million dollars (1989). Based on this
commitment, design and construction activities are now moving
forward. Additional partners are being sought. The next mirror to be
cast at the Steward Observatory Mirror Lab in early 1996 will be
the first borosilicate honeycomb primary for LBT. The baseline
optical configuration of LBT includes wide field Cassegrain
secondaries with optical foci above the primaries to provide a
corrected one degree field at F/4. The infrared F/15 secondaries are
a Gregorian design to allow maximum flexibility for adaptive optics.
The F/15 secondaries are undersized to provide a low thermal
background focal plane which is unvignetted over a 4 arcminute
diameter field-of-view. The interferometric focus combining the light
from the two 8.4 meter primaries will reimage two folded Gregorian
focal planes to a central location. The telescope elevation structure
accommodates swing arms which allow rapid interchange of the various
secondary and tertiary mirrors. Maximum stiffness and minimal thermal
disturbance continue to be important drivers for the detailed design
of the telescope. The telescope structure accommodates installation
of a vacuum bell jar for aluminizing the primary mirrors in-situ on
the telescope. The detailed design of the telescope structure will be
completed in 1995 by ADS Italia (Lecco) and European Industrial
Engineering (Mestre). The final enclosure design is now in progress
at M3 Engineering (Tucson) and ADS Italia. Construction activities on
the Emerald Peak (Mt. Graham) site should begin in the spring of 1995.
LBT Summary
- optical configuration ------------- binocular 8.4 meter apertures
- equivalent aperture ------------ 11.8 meters (2 * 55 m 2)
- 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 (25%)
- Italy --- Osservatorio Astrofisico di Arcetri (25%)
- Research Corporation (12.5%)
- Ohio State University (4%)
- mounting type ------------ dual ring platform (altitude -- azimuth)
- moving mass ------------ 420 metric tons
- site ------------ Mt. Graham, Arizona (Emerald Peak, 3190 m)
LBT Project Status
- Telescope Design
The detailed mechanical design of the telescope is
being done by the Italian engineering firms ADS (Lecco) and EIE
(Venice). As of December 1994, the detailed design work is about 40%
complete. Already over 100 MB of Autocad drawings have been
generated. The design of the control system is being done by Steward
Observatory.
- Enclosure Design
The detailed architectural design of the enclosure is
being done by a consortium of companies headed by M3 Engineering &
Technology Corp. (Tucson). Major construction (concrete) should
begin during the 1996 construction season.
- Site Work
The LBT will be part of the Mt. Graham International
Observatory near Safford, Arizona. The construction of the
observatory with three telescopes was approved by Congress in November
1988. The site for the LBT Project approved by the Forest Service in
1993 is shown in the drawing below together with the locations of the
Lennon (1.8 m F/1.0 optical) and Hertz (10 m sub-millimeter)
telescopes which are now operational. Trees on the site (Emerald Peak)
were cut in December 1993. Geology testing was done in January 1994
to select the precise pier location. Leveling of the site and
completion of the access road were delayed by a lawsuit filed against
the Forest Service in July 1994. We are now awaiting a ruling on an
appeal by the 9th Circuit Court in San Francisco.
- Telescope Fabrication
Once the design drawings of the telescope are completed
in the Summer of 1995, the project will solicit bids world-wide to
select the companies to fabricate and assemble the telescope.
- Mirror Fabrication
The Steward Observatory Mirror Lab has now cast two 6.5 m
honeycomb mirrors. The first of these F/1.25 parabolic mirrors is now
being ground and polished. The fabrication and assembly of the mold
for the first LBT 8.4 m F/1.14 mirror is now underway. The actual
casting of this mirror should occur in early 1996. The polishing of
this mirror should be completed by 1998.
- Funding
The existing partners Arizona, Italy and Research
Corporation have committed sufficient funds, $40M, to permit
construction of the complete telescope and enclosure with only a
single set of optics. The project is proceding with construction on
that basis. Additional partners are being sought to complete the
$60M (1989) budget and permit the second primary mirror and
instrumentation to be added.
- First Light
Current schedules for the telescope, mirror and enclosure
suggest that first light will occur in Fall 1999.
Optical Design Drivers
- Large total collecting area for sensitivity on faint objects.
- Excellent image quality through passive, active and adaptive
control of seeing and other aberrations.
- Low background from a clean thermal infrared design.
- Versatile instrumentation and rapid changes in configuration to
take maximum advantage of specific observing conditions.
- High ultimate spatial resolution by providing a relatively long
baseline with the stability and field-of-view provided by a common mounting.
- Low construction and operations costs.
Baseline Focal Stations
- trapped Cassegrain, optical, dual F/4.0
- Gregorian, infrared, dual F/15
- phased combined, reimaged F/15, center
- bent or pseudo-Nasmyth, F/15
Figure 2
Figure 2: This figure shows what LBT has come to call ``Beam Combiner Design
3''. Collimator and camera lenses are used to reimage a pair of bent
8.4 m F/15 Gregorian focal planes to the combined focus. The
reimaging lenses have not been optimized so the design should be
considered illustrative of the concept.
Telescope Structure
- Telescope Structure: model A 3, platform design
- Support Spacing: 2 ``C'' rings on 10 meter centers
- Pier Diameter: 14 meters for azimuth track
- Telescope Height: ~ 25 meters at elevation axis
(30 m above bedrock)
- Support of Telescope: hydrostatic pads
- Drive Mechanism: gear and pinion
- Telescope and Drive Stiffness Goal: locked rotor frequency > Hz
- Vibration Specification: < 0.025 µm amplitude above 8 Hz
- Encoders: strip type
- Telescope Moment of Inertia: approximately 1*107 Kg m 2 (both axes)
- Telescope Mass: approximately 420 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
Telescope Enclosure
- Co-Rotating Rectangular Enclosure
- Double Sliding Portal Shutters
- Building Height: 48 meters at roofline
- Maximum Operating Wind Speed: 80 km/hr
- Survival Wind Speed (closed): 225 km/hr
- Primary Mirror Aluminizing: on-board the telescope
- Handling System: overhead crane (2 x 40 tons)
- Ventilation: large area --- passive
- Snow Removal: circulation of heated air
View Figure 3 here
View Figure 4 here
View Figure 5 here
View Figure 6 here
View Figure 7 here