Title: Canadian Very Large Optical Telescope Technical Studies Scott Roberts National Research Council Cana
1Canadian Very Large Optical Telescope Technical
StudiesScott RobertsNational Research Council
Canada, Herzberg Institute of Astrophysics(DAO)
http//www.hia.nrc.ca/pub/staff/cbt/XLT/Correspon
dence Email scott.roberts_at_nrc.ca Address
National Research Council Canada, 5071 West
Saanich Road, Victoria, B.C., Canada, V9E 2E7
Telephone 250-363-8314 Fax 250-363-0045
2Author list
Scott Robertsa, Christopher Morbeya, Dennis
Crabtreea, Ray Carlbergb, David Cramptona,Tim
Davidgea, Joeleff Fitzsimmonsa, Mike Gedigc,
David Hallidayc, James E. Hessera, Glen
Herriota, J. B. Okea, John Pazdera, Kei Szetoa,
Jean-Pierre Verana aHerzberg Institute of
Astrophysics, National Research Council
Canada bUniversity of Toronto cAMEC Dynamic
Structures Ltd.
3Outline
- Project organization
- Context for a Canadian LOT
- Optical configuration
- Observational modes
- Telescope structure and dome design
- Pupil segmentation schemes
- Gap, segment size effects on EE, PSF
- Candidate mirror substrate materials, SiC study
- Integrated model of telescope
4The future generation of large telescopes
Canadian Long Range Plan Coalition AMEC/NRC/CASCA
5Canadian large optical telescope project
- Project Scientist Ray Carlberg, University of
Toronto - Project Manager Dennis Crabtree, (HIA/NRC)
- Science Steering Committee (Ray Carlberg, Chair)
- Technical Studies
- Research Collaboration between HIA/NRC and AMEC
Dynamic Structures - Scott Roberts, Technical Lead (HIA/NRC)
- David Halliday Mike Gedig, Technical Leads
(AMEC) - Several University Groups
- Funded at 1M US/year as of April 2002
6Context for a Canadian large telescope
- The Canadian Long Range Plan (LRP) for Astronomy
calls for a 20 to 30 m telescope to be available
to astronomers early in the ALMA/NGST era
(2012). Faster deployment has a higher priority
than the largest possible telescope size. - Telescope should be superior to, or competitive
with a 6 m NGST at wavelengths less that 2
microns. - Image quality is the highest, but not sole,
priority. There is strong support for having the
widest possible field of view for natural seeing
observations. - Possible location at CFHT site on the Mauna Kea
summit ridge (ng-CFHT). - Design fits within Mauna Kea Master Plan
requirements. - Designed for Mauna Kea environmental conditions.
- Canadian community expects to partner, but would
prefer a second to none share of a large
telescope. - Baseline ? 0.36 to 2.3 microns, with extension
to longer wavelengths
7Optical Configuration and Observational Modes
8LOT optical configuration baseline
- RC Design
- Segmented primary mirror, 20 m diameter, F/1
- Secondary mirror 2.5 m diameter
- 18 m back focal length (F/15)
- First fold beneath mirror support cell
- Instruments on 2 Nasmyth Platforms (vertical)
- Maximum 20 field of view (1.7 m dia, 2.5 m
curv.).
9Observational modes
- Natural Seeing
- Maximum 20 field compatible with median MK
seeing - Degrades 50th ile MK seeing by no more than 15
- 10 Field with 1-metre refractive field
corrector and ADC - Degrades 25th ile MK seeing by no more than 10
- Low Order AO
- 6 field, low Strehl
- High Order AO
- 20 field, H Band Strehl 0.4
- Future upgrade path to MCAO
10Telescope Structure and Dome
11High performance, low profile structural design
- Large hydrostatic bearing wheels 12M diameter
- Monocoque primary support structure
- Short and direct load path for mass support
- Low profile azimuth platform
- Secondary support carried on main structure
- Elevation assy 880 tonnes, 1565 tonne moving mass
- Mirror cell 1st mode 13.4 Hz.
- Secondary support 1st 10.3 Hz.
12Structural design
- The load path from the telescope structure is
passed almost directly into the azimuth support
journal
- Main structure supports the mirror cell, bearing
wheels and the secondary support structure
13Primary mirror cell (monocoque)
Sectioned Monocoque Mirror cell
- Modeled Performance
- Maximum deflections due to gravity lt2mm
Mirror segment access
14Telescope critical dimensions
15Primary F/ versus dome size
Diameter 104M Height 70M
Diameter 72M Height 48M
Diameter 75M Height 55M
Diameter 51M Height 38M
Elevation axis 18M above grade
APPROXIMATE ENCLOSURE SIZE REQUIRED FOR A 20M
MIRROR WITH FOCAL LENGTHS OF F1 AND F1.5
APPROXIMATE ENCLOSURE SIZE REQUIRED FOR A 30M
MIRROR WITH FOCAL LENGTHS OF F1 AND F1.5
16Calotte dome
- See 4840-73, Wed. _at_ 210
- 2 stages, base and inclined
- Circular aperture
- Wind attenuation
- Structurally superior
- Balanced stages
- Even power dissipation
- Safety
- Dome closed by 2nd internal stage
17Pupil Segmentation Schemes, EE and PSF
18Pupil segmentation schemes
- Hexagonal Segmentation
- Best system solution?
- Complex pupil boundary
- Families of 6
- Many spares
- 1.2 m, 348 seg., 58 spares
- Radial Segmentation
- Smooth pupil boundary
- 8 m central segment
- Phasing
- Commissioning
- Families of 20/40
- Economy in fabrication?
- Few spares (180 seg, 9 spares)
19Mirror fabrication study
- Canada, France and CFHT have jointly funded a
study at Sagem to investigate technical, cost and
schedule issues related to various segmentation
schemes. - Key results of study will be
- Fabrication risks, figuring errors, edge effects
- Optical test method(s) and requirements
- Budget and fabrication schedule
8 m segments
348x1.2?
150x1.8?
84x2.5?
Radial (1801x8m)
20EEs 2 m hex segment, various gaps, no spider
?1.2 ?m
21EEs for various hex segment sizes, 10 mm gap,
spider
444x1m 12x6m
114x2m 6x8m
30x4m 1x20m
- Hexagonal 20 cm wide support spider
22PSFs for segmentations with secondary obscuration
23EEs for various segment size and constant 10 mm
gap
24Mirror Materials
25Primary mirror candidate materials
- SiC offers lower areal density, simpler support
systems, lower thermal mirror seeing effects
26Silicon carbide study
- Offers significant mechanical and thermal
advantages over Zerodur, ULE substrates - Isostatic Press, Machine, Light-weight, Sinter,
CVD SiC front surface, grind, polish, ion figure.
- Trade-off stiff, 3 point support vs. low areal
density whiffle tree support, 1 to 2 m - Currently expensive to produce
27Integrated Modeling
28Integrated model
- Matlab Model
- End-to-End
- Optimize system
- Link to external optics engines and atmospheric
models
29Summary
- Canadian designs for a Large Optical Telescope
are progressing - We would like to collaborate with other groups
on technical studies - See 4840-73, New approach to enclosure design
for large telescopes, D. Halliday, M. Gedig, W.
Brzezik, Y. Zhou, P. Evans, AMEC Dynamic
Structures Ltd., Wednesday _at_ 210