networking ground-based optical telescopes for space guard missions
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Networking ground-based optical telescopes for spaceguard missions
Hakim Luthfi Malasan
Bosscha Observatory & Astronomy Division, FMIPA, ITB
Earth in solar system,
NEO-NEA-ECA-PHA-...
Apollo 17 (7-19 DECEMBER 1972)
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New look at our solar system
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Asteroid Belt
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Asteroids with diameters > 250 km
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Asteroid Founder in Diameter (km)
1 Ceres Piazzi 1801 974
2 Pallas Olbers 1802 544
4 Vesta Olbers 1807 529
10 Hygiea de Gasparis 1849 407
31 Euphrosyne Ferguson 1854 370
704 Interamnia Cerulli 1910 350
511 Davida Dugan 1903 323
65 Cybele Tempel 1861 309
52 Europa Goldschmidt 1858 289
451 Patientia Charlois 1899 276
15 Eunomia de Gasparis 1851 272
3 Juno Harding 1804 267
16 Psyche de Gasparis 1852 250
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Near-Earth Asteroids (NEAs) • NEA diameters known: 13 with diameters > 250 km 811 with diameters > 1 km ~100,000 with diameters > 0.14 km • Meteor (shooting star): usually comet dust burning in Earth’s atmosphere. • Meteorite: reaches Earth’s surface, usually from asteroid belt. Mass: few kilogram to many tons. • 100-ton meteorite has impact energy of ~1 megaton TNT (~70 x Hiroshima). • On Earth: ~170 impact craters, diameters of ~10 to ~300 km: explosions up to 100,000 Gigaton TNT in the past. • Present chance for heavy impact: ~1 in 1 000 000 / yr. • Barringer meteorite: 50 000 years ago, 13 km/s, diameter ~50 m, mass ~300 000 ton, explosion of ~2.5 megaton TNT.
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Motivations
Two major events can be identified as the causes of such enlarged attention:
• The correlation between the impacts of minor bodies on our planet and global catastrophes;
• The evidence given to such type of cosmic events by the impact of the periodic comet Shoemaker-Levy 9 with the planet Jupiter in July 1994.
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IMPACTS
When d (asteroid) Crater d (Crater) E (TNT)
65 Myear BC 10 ± 4 km Chicxulub, Mexiico
180-300 km 108 MT
50 Kiloyear BC ~40 m Barringer, USA 1.2 km 2.5 MT
1490 meteorite fall 1-1.5 kg
Shani, China - >10,000 people †
1908 40 ± 10 m Tunguska, R [2000 km2] 10-15 MT
1947 Meteorite fall Sikhote Alin, R 1m -26 m
Hiroshima 15 kiloT
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Chicxulub, Yucatán, Mexico (D = ~265 km, t = 65 Myr)
Barringer Meteor Crater
Arizona, USA (D = 1.2 km, t = 50 000 yr)
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10-km NEO
resulted in total
extinction of about
half the living
species
of animals and
plants
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Terrestrial impact structures
• Nearly 200 have been established with a high degree of certainty
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Spaceguard,
spacewatch, Near-
earth objects
awareness program…
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Spacewatch project (Lunar and planetary laboratory, Univ. of Arizona)
• Discovery and followup of asteroids and comets
• First to use CCD for solar system astrometry
• Continuous operation since 1984
• Detection statistics have supported studies of:
– NEOs
– Centaurs
– Main belt
– TNOs
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Spaceguard Survey Progress
• Originally proposed by NASA panel in 1992 Additional support from US Congress in 1995
Adopted as NASA goal in 1998 (in collaboration with USAF)
• Objective: Discover and track 90% of the Near Earth Asteroids (NEAs) with diameter greater than 1 km within ten years (by 2008) Estimated number of NEAs larger than 1 km: approximately 900
Number discovered through end of 2000: approximately 430
Estimated completion date (to 90%): 2012
• Most NEAs discovered by MIT-Lincoln Lab LINEAR search system Two USAF 1-m telescopes with NASA operating funds
Discovery rate approximately 5 / month
• International program for follow-up and orbit determination
• Threatening NEAs (if any) should be identified decades before impact
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Technical characteristics..
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Instrumental requirements
• Discovery instruments D 1-m. At least two such instruments in each hemisphere, well separated in longitude, plus possible back-up instruments.
• The Field of view (FOV) of these instruments should be of several square degrees and paved with fast read-out CCDs.
• The discovery sites should have large storage capabilities in order to retain all frames taken during the sky survey. These images should, after a first processing for detecting new objects, be transferred to an ad hoc data center for further inspection and for documentation useful for non-NEO studies.
• The discovery centers should be sufficiently co-ordinated, in order not to duplicate efforts.
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• Follow-up instruments may be of any class, but at least two telescopes in the 2m range are needed for follow-up of faint objects, one in each hemisphere. Moreover, sufficient observing time should be allocated at larger instruments (in the 4m class) for follow-up of very faint objects, when the necessity arises.
• More professional centers should be involved in follow-up observations. The follow-up centers must be efficiently co-ordinated at a high level, including planning of observations, recovery strategies, sharing of schedules, joint campaigns.
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Bisei Spaceguard Center,
Bisei Town, Okayama Prefecture,
JAPAN
Large Optical Telescope
The large optical telescope, the primary
mirror of which has a diameter of 1 meter,
permits observation over a wide range of 3
degrees. A cooled charge-coupled device
(CCD) camera consisting of 10 highly
sensitive CCD elements arranged in a
mosaic pattern is installed at the focal point
of the telescope. A batch of digital image data
acquired by the camera is sent to computers
where it is analyzed. The telescope can
detect space debris of about 50 cm in
diameter near the GEO and GTO, and NEOs
of at least 1 km in diameter.
Focus mode Cassegrain-type focusing, F/3
Field of view 3 degrees
Max. tracking speed
More than 5 deg./sec (right ascension/declination)
Structure Folk-type equatorial
CCD camera Approx. 160-mm imaging diameter Uses ten of 2,000 x 4,000 pixel CCD cell
CCD temperature
Approx. 173K during observations
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Small Tracking Telescope
The two small telescope, which
have primary mirror of 50 cm
and 25 cm co-mounted on 50-
cm telescope, are principally
used to track and observe
space debris travelling at high
speed. For this season, each
telescope is mounted in a
structure designed to enable
the telescope tube to be
moved at a rate of 5 degrees
per second. As with the large
telescope, a cooled CCD
camera is used to acquire
image data which is analyzed
by computer in order
determine the orbit of the
space debris and NEOs.
50-cm Optical Telescope
25-cm Optical Telescope
Focus mode Cassegrain-type focusing, F/2
Baker Richey Chretian-type focusing, F/5
Field of view 2 degrees 5 degrees
Max. tracking speed More than 5 deg./sec (right ascension/declination)
ditto (Mount on 50-cm Optical Telescope)
Structure Folk-type equatorial ditto (Mount on 50-cm Optical Telescope)
CCD camera Approx. 50-mm imaging diameter Uses two of 2,000 x 4,000 pixel CCD cell
2,000 x 2,000 pixel CCD cell
CCD temperature Approx. 173K during observations
Approx. 243K during observations
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Computer System and LAN
The proposed computer system and
LAN for the Bisei Spaceguard Center
are shown at right. The large and small
telescopes are operated by computer
control. In addition, not only is it
possible to transmit observation data
from the facility to other stations, the
telescopes can also be controlled
externally.
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Observational and reduction techniques
Moving object detection program
Stacking method
Hough transform
…
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Can we participate in
the spaceguard
missions?
Observing network operation
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Northern hemisphere:
Italy, Japan, USA
Southern hemisphere:
Uruguay, Australia
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Small telescopes v.s.
Large telescope?
Networking observatories with “small”
telescopes
Astroeconomics model toward higher
productivity of (optical) data
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Astroeconomic model of network (Budding 1993) Cost-productivity for
group of telescopes
(characterized by D)
in remote/automated
fashion
1. Information flow
2. Key cost & organization
Advantages of small telescope: Efficiency
Adequacy Availability Flexibility
Serendipity
low capital
High capital
Relative knowledge rate WET
AAVSO
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Role of general-purpose small telescopes
(small telescope owner’s view)
• Projects which require large number of observations
• Projects which require all-sky or extended time coverage
• Projects which require extreme flexibility
• Stimulation for larger access ability to larger telescope
• Training, experiment & development of (new) instrument
• Education
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Proliferation of small telescopes at the Observatory and new public facility
Almost 40
telescopes with
20-28 cm are
available on
market and
owned by LAPAN,
BMKG, ITB and
other institutes
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Extending capability of small-
intermediate size telescopes for
networking
Support of pointing & tracking for proper CCD imagery & spectroscopy
Autoguider
New control system based on common S/W Remote
Embedded acquistion system
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Existing network of sites for small telescope (main
players: ITB, LAPAN, BMKG, supporters:
Kemenkominfo, Kemdiknas)
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Spaceguard integrated system
Leading institutions: LAPAN, BMKG, ITB
• A ground-based observational system, including all observation stations for discovery, follow up and physical studies
• A space-based observational system, devoted to physical characterization and discovery and tracking of peculiar objects
• A ground network, composed by the data collecting and analysis centers
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The Necessity of International Cooperation
The problem is thus international in scope; it is also international in solution.
The need for international cooperation is obvious, and rapid and efficient international communication
through a central agency is a requirement.
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That the hazard posed by NEO's is a problem for all
humankind hardly needs repeating.
The likelihood of a particular spot being the target of an
impact is independent of its geographic position, so that
we are all equally at risk.
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* IAU Minor Planet Center, hosted at SAO
* IAU Division III Working Group on
Small Bodies Nomenclature
* IAU EC Advisory Committee on
Hazards of Near-Earth Objects
* IAU web page <http://www.iau.org/public/nea/>
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The role of the International Astronomical Union (IAU)
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The IAU Executive Committee is invited to consider
Reviewing the role of the current IAU EC Advisory Committee (AC) on Hazards of Near Planetary Objects.
Creating a new IAU EC Working Group on Hazards of Near Earth Objects. Assigning one IAU (GA-)Symposium or GA-Special Session per three years to
Near Earth Objects hazards science, to be organized by the suggested new EC Working Group on Hazards of Near Earth Objects.
Calling upon its 67 IAU National Members to increase their support for astronomical observatories participating in surveys for detection, tracking and monitoring of Near Earth Objects down to D > 25 m (i.e., H < 26 mag). Such could perhaps be framed by the EC in a Resolution for the IAU XXVIII General Assembly in Beijing, August 2012.
Pro-active collaboration with other scientific unions and institutions with an interest in the risks of Natural Hazards and Disasters, particularly with the recently established International Council for Science (ICSU) programme on Integrated Research on Disaster Risk.
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IAU WEB PAGE on NEAs
The International Astronomical Union (IAU) reports the launch in March 2010 of its public web page on Near Earth Asteroids, entitled
"Near Earth Asteroids (NEAs) A Chronology of Milestones" <www.iau.org/public/nea/>
The page quotes facts related to Near Earth Asteroids for the period AD 1800 to AD 2200 from the available literature and web sites: discoveries, close encounters within 1 Lunar Distance (quoted from JPL), and related scientific meetings and reports.
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TERIMA KASIH
...since the Moon has always been the companion of the Earth,
the history of the former is only a paraphrase of the history of
the latter... [Its mirror on Earth] contains a disturbing factor.
There is no assurance that these meteoritic impacts have all
been restricted to the past. Indeed we have positive evidence
that [sizeable] meteorites and asteroids still abound in space
and occasionally come close to the Earth. The explosion that
formed the [lunar] crater Tycho...would, anywhere on Earth, be
a horrifying thing, almost inconceivable in its monstrosity. (Baldwin 1949)
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