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  9.1 OverviewConcern over the cosmic impact hazard motivated the U.S. Congress
    to request that NASA conduct a workshop to study ways to achieve
    a substantial acceleration in the discovery rate for near-Earth
    asteroids. This report outlines an international survey network
    of ground-based telescopes that could increase the monthly discovery
    rate of such asteroids from a few to as many as a thousand. Such
    a program would reduce the time-scale required for a nearly complete
    census of large Earth-crossing asteroids (ECAs) from several
    centuries (at the current discovery rate) to about t 25 years.
    We call this proposed survey program the Spaceguard Survey (borrowing
    the name from the similar project suggested by science-fiction
    author Arthur C. Clarke nearly 20 years ago in his novel Rendezvous
    with Rama). In addition, this workshop has considered the impact hazards
    associated with comets (both short-period and long-period) and
    with small asteroidal or cometary objects in the tens of meters
    to hundreds of meters size range. The object is not elimination
    of risk, which is impossible for natural hazards such as impacts,
    but reduction of risk. Emphasis, therefore, is placed upon the
    greater hazards, in an effort to define a cost-effective risk-reduction
    program. Below we summarize our conclusions with respect to these
    three groups of objects: ECAs, comets, and small (Tunguska-class)
    objects. 1) Large ECAs (diameter greater than 1 km,
    impact energy greater than a million megatons). These objects
    constitute the greatest hazard, with their potential for global
    environmental damage and mass mortality. About two thousand such
    objects are believed to exist in near-Earth space, of which fewer
    than 10 percent are now known. Between a quarter and a half of
    them will eventually impact the Earth, but the average interval
    between such impacts is long -- more than 100,000 years. While
    some of these objects may break up during entry, most will reach
    the surface, forming craters if they strike on the land. On average,
    one ECA in this size range passes between the Earth and the Moon
    every few decades. The proposed Spaceguard Survey deals effectively with this
    class of objects. Telescopes of 2-3 m aperture can detect them
    out to a distance of 200 million kilometers. Since their orbits
    bring them frequently within this distance of the Earth, a comprehensive
    survey will discover most of them within a decade and can achieve
    near completeness within 25 years. Specifically, the survey modeled
    here, covering 6000 square degrees of sky per month to magnitude
    V = 22, is calculated to achieve 91 percent completeness for
    potentially hazardous ECAs in 25 years. The most probable outcome
    of this survey will be to find that none of these objects will
    impact the Earth within the next century, although a few will
    need to be followed carefully to ensure that their orbits do
    not evolve into Earth-impact trajectories. In the unlikely case
    (chances less than 1 percent) that one of these ECAs poses a
    danger to the Earth over the next century or two, there will
    be a warning of at least several decades to take corrective action
    to deflect the object or otherwise mitigate the danger. 2. Comets. Comets with short periods (less than
    20 years) will be discovered and dealt with in the same manner
    as the ECAs described above; they constitute only about 1 percent
    of the ECA hazard in any case. However, comets with long periods
    (more than 20 years), many of which are entering the inner solar
    system for the first time, constitute the second most important
    impact hazard. While their numbers amount to only a few percent
    of the ECA impacts, they approach the Earth with greater speeds
    and hence higher energy in proportion to their mass. It is estimated
    that as many as 25 percent of the objects reaching the Earth
    with energies in excess of 100,000 megatons are long period comets.
    On average, one such comet passes between the Earth and Moon
    per century, and one strikes the Earth every million years. Since long-period comets do not (by definition) pass frequently
    near the Earth, it is not possible to obtain a census of such
    objects. Each must be detected on its initial approach to the
    inner solar system. Fortunately, comets are much brighter than
    asteroids of the same size, as a consequence of outgassing stimulated
    by solar heating. Comets in the size range of interest will generally
    be visible to the Spaceguard Survey telescopes by the time they
    reach the asteroid belt (500 million km distant), providing several
    months of warning before they approach the Earth. However, the
    short time-span available for observation will result in less
    well-determined orbits, and hence greater uncertainty as to whether
    a hit is likely; there is a greater potential for "false
    alarms" with comets than asteroids. Simulations carried
    out for this report indicate that only 35 percent of Earth-crossing
    long-period comets greater than 1 km in diameter will be detected
    with at least 3 months warning in a survey of 6000 sq degrees
    per month. By increasing the area of the survey to include the
    entire dark sky, as many as 77 percent could be detected.. Increasing
    telescope aperture to reach fainter magnitudes (V = 24) improves
    the discovery rate still further. Because of the continuing hazard
    from comets, which may appear at any time, the cometary component
    of the Spaceguard Survey should be continued even when the census
    of large ECAs is essentially complete. 3. Smaller Asteroids, Comets, and Meteoroids
    (diameters from about 100 m to 1 km; energies from 20 to a million
    megatons). These impacts are below the energy threshold for
    global environmental damage, and they therefore constitute a
    smaller hazard in spite of their more frequent occurrence. Unlike
    the large objects, they do not pose a danger to civilization.
    The nature of the damage they cause depends on the size, impact
    speed, and physical nature of the impacting object; only a fraction
    of the projectiles in this size range will reach the surface
    to produce a crater. However, detonation either at the surface
    or in the lower atmosphere is capable of severe local damage,
    generally on a greater scale than might be associated with a
    large nuclear weapon. Both the Tunguska (1908) and Meteor Crater
    impacts are small examples of this class. The average interval
    between such impacts for the whole Earth is a few centuries;
    between impacts in the inhabited parts of the planet is a few
    millennia; and between impacts in densely populated or urban
    areas is of the order of 100,000 years. More than one million
    Earth-crossing objects probably exist in this size range, with
    several passing between Earth and Moon each year. The Spaceguard Survey will discover as many hundreds of objects
    in this size range every month. By the end of the initial 25-year
    survey, it will be possible to track the orbits of as many as
    100,000, or about 10 percent of the total population. If the
    survey continues for a century, the total will rise to about
    40 percent. Since the interval between such impacts is greater
    than 100 years, it is moderately likely that the survey will
    detect the "next Tunguska" event with ample warning
    for corrective action. However, in contrast to the ECAs and even
    the long-period comets, this survey will not achieve a near-complete
    survey of Earth-crossing objects in the 100-m size range in less
    than a several centuries with current technology. If there is
    a societal interest in protecting against impacts of this size,
    presumably advanced technologies will be developed to deal with
    them.      
  9.2 Survey Network: Cost and ScheduleThe proposed Spaceguard Survey network consists of six telescopes
    of 2-3 meter aperture together with a central clearinghouse for
    coordination of the observing programs and computation of orbits.
    It also requires access to observing time on existing planetary
    radars and optical telescopes for follow-up. For purposes of
    this discussion, we assume that the Spaceguard Survey will be
    international in operations and funding, with the United States
    taking a leadership role through the Solar System Exploration
    Division of NASA.   The Spaceguard Survey TelescopesThe six survey telescopes required for the Spaceguard Survey
    are new instruments optimized for the discovery of faint asteroids
    and comets. While it is possible that one or more existing telescopes
    could be retrofit for this purpose, we expect that the most cost-effective
    approach is to design and construct telescopes specifically for
    this project. For purposes of this Report, we consider a nominal
    telescope design of 2.5 m aperture and 5.2 m focal length with
    a refractive prime-focus corrector providing a field-of-view
    of at least 2 degrees. The telescope will have altitude-azimuth
    mounting and be capable of pointing to an accuracy of a few arcsec
    and tracking to a precision of a fraction of an arcsec at rates
    up to 20 times sidereal. We assume that each telescope will be
    located at an existing observatory site of proven quality, so
    that no site surveys or new infrastructure development (roads,
    power, etc.) is required. The nominal aperture of 2.5 m is optimized
    for the ECA survey, but we note that larger telescope aperture
    (3 m or even more) would permit long-period comets to be detected
    at greater distances and thereby provide both greater completeness
    and months of additional warning. An instrument of very similar design has recently been proposed
    by Princeton University for a wide-angle supernova survey. Cost
    estimates for this telescope are summarized in Table 9.1, adapted
    from their current (1991) proposal to the National Science Foundation.
    We believe that the SPACEGUARD Survey Telescopes could similarly
    be built for about $6 million each, including observatory building,
    but not including the focal plane of several mosaiked CCD detectors
    or the supporting data processing and computation capability.
    For each telescope, we allocate $1 million for the focal plane
    and $1 million for computer hardware and software, for a total
    cost per installation of $8 million. If these six telescopes
    were purchased together, the capital costs would thus be about
    $48 million. For an estimate of operating costs, we assume that each telescope
    will require the following staffing: 2 astronomers, 2 administrative
    support personnel, 3 telescope operators, 1 each senior electronic
    and software engineers, and 2 maintenance and support technicians,
    for a total of 11 persons. Additional funds will be needed for
    transportation, power, sleeping accommodations for observers,
    and other routine costs associated with the operation of an observatory;
    the exact nature of these expenses depends on the location and
    management of the pre-existing site where the telescope is located.
    The total operations for each site should therefore run between
    $1.5 million and $2.0 million per year. In making this estimate
    we assume that each survey telescope is dedicated to the Spaceguard
    effort, and that it will be in use for about three weeks (100-150
    hours) of actual observing per month. If it is intended that
    the telescope be used for other unrelated purposes when the Moon
    is bright, we assume that the other users will pay their prorata
    share of operation costs. The Spaceguard Survey Operations Center should provide overall
    coordination of the international observing effort, including
    rapid communications among the survey telescopes and those involved
    in follow-up observations. The Spaceguard Survey Operations Center
    will also compute orbit ephemerides and provide an ongoing evaluation
    of the hazard posed by any object discovered by the Survey. Similar
    functions are performed today for the much smaller number of
    known asteroids by the Minor Planet Center in Cambridge, Massachusetts.
    Scaling from that operation, we estimate an initial cost of $2
    million for computers and related equipment, and an annual operating
    cost of $2 million. A third component of the Spaceguard Survey Program is follow-up,
    including radar and optical observations. As noted previously
    in this Report, it would be desirable to have one or more dedicated
    planetary radars and large-aperture optical telescopes (4-m class).
    However, we anticipate that a great deal of useful work could
    be done initially using existing planetary radars and optical
    facilities. Therefore, for purposes of this Report, we simply
    allocate a sum of $2 million per year for the support of radar
    and optical observing on these instruments.   Spaceguard Management and Cost-SharingThe total estimated capital costs for the Spaceguard Survey
    are $50 million, with operating costs of $8-$10 million per year.
    We anticipate that these costs would be shared among several
    nations with advanced technical capability, with the maximum
    expenditure for the U.S. (or any other nation) of less than half
    the total amount. For purposes of U.S. budgeting, we assume that
    NASA will pay the cost of two telescopes ($16 million) and the
    Operations Center ($2 million), and will support operating costs
    of $5 million per year. Management of the U.S. component of the Spaceguard Survey
    could be accomplished by NASA in one of two ways. (1) The telescopes
    could be constructed and operated by universities or other organizations
    with funding from NASA Headquarters through grants or contracts,
    as is done today with the NASA IRTF telescope on Mauna Kea (owned
    by NASA but managed by the University of Hawaii under a five-year
    contract) or the 0.9-m Spacewatch Telescope on Kitt Peak (owned
    and operated by the University of Arizona with partial grant
    support from NASA). (2) NASA could construct and operate the
    telescopes itself through one of its Centers (JPL or Ames, for
    example); the Centers might contract with universities or industry
    for operations but would retain a more direct management control.
    Similarly, the Spaceguard Survey Operations Center could be located
    at a NASA Center or could be supported by grants or contracts
    at a university or similar location, such as the present Minor
    Planet Center at the Harvard-Smithsonian Center for Astrophysics.
    In any case, international cooperation and coordination is essential,
    and an international focus is required from the beginning in
    planning and supporting this program.   Initial StepsThe construction of the new Spaceguard Survey telescopes will
    require approximately four years from the time funding is available.
    In the meantime, several steps are essential to ensure a smooth
    transition from the present small surveys to the new program.
    (1) An international coordination effort should be initiated
    by NASA, independent of but coordinated with the International
    Astronomical Union Working Group on Near Earth Objects, in order
    to plan for the orderly development of the Spaceguard Survey
    network. (2) The small cadre of current asteroid observers should
    be strengthened. Additional expenditures of about $1 million
    per year on existing teams would allow for expansion of personnel,
    purchase of badly needed new equipment, and greater sky coverage.
    Consequently, the discovery rate of ECAs should double to quadruple,
    thereby also increasing our confidence in modeling the population
    of such objects and planning the requirements for operation of
    the full-up survey. (3) In order to gain additional experience
    with the kind of automated CCD scanning techniques proposed for
    the Spaceguard Survey, efforts should be made as soon as possible
    to place in operation a telescope that utilizes these techniques;
    one such option is the proposed 1.8-m Spacewatch telescope at
    the University of Arizona. Efforts are also required in studying
    the use of CCD arrays and in developing appropriate software
    to support CCD scanning. (4) Continuing support should be provided
    for research on near-Earth asteroids and comets, including their
    dynamics and their physical properties. For purposes of this
    study, we assume an increase of $2 million/year beyond current
    NASA expenditures for these programs, to be maintained during
    the transition period.   Proposed Schedule for NASA FundingOn the assumption that the Spaceguard Program can begin in
    a modest way in FY 93 and will reach full funding about FY95,
    we suggest the following possible schedule for new NASA support
    of this effort 
 
 
      
        | TABLE 9.2: Proposed NASA Funding (in FY93 $M) |  
        | Fiscal Year | 93 | 94 | 95 | 96 | 97 | 98 | 99 | 00 |  
        | Transition | 02 | 02 | 02 | 02 | 02 | 02 | 01 | 00 |  
        | Capital Costs | 01 | 02 | 04 | 04 | 04 | 04 | 00 | 00 |  
        | Operations | 00 | 00 | 00 | 01 | 02 | 02 | 05 | 05 |  
        | Total | 03 | 04 | 06 | 07 | 08 | 08 | 06 | 05 |         
  9.3 ConclusionsThe Spaceguard Survey has been optimized for the discovery
    and tracking the larger ECAs, which constitute the greater part
    of the cosmic impact hazard. If any large ECAs threaten impact
    with the Earth, they could be discovered with ample lead-time
    to take corrective action. The Spaceguard system also will discover
    most incoming long-period comets, but the warning time may be
    only a few months. Finally, the great majority of the new objects
    discovered by the Spaceguard Survey will have diameters of less
    than 1 km; these should be picked up at a rate of about a thousand
    per month. It is therefore reasonably likely that even the "next
    Tunguska" projectile (20 megatons energy) will be found
    by the Spaceguard Survey if it is continued for a century or
    more. The Spaceguard Survey should be supported and operated on
    an international basis, with contributions from many nations.
    The total costs for this system are of the order of $50 million
    in capital equipment, primarily for the six survey telescopes,
    and $10-15 million per year in continuing operating support.
    However, these estimates will vary depending on the aperture
    and detailed design of each telescope, the nature of the international
    distribution of effort, and the management of the survey. In
    particular, larger telescopes would be appropriate if greater
    emphasis is to be given to the search for long period comets.
    Whatever the exact cost, however, the proposed system can provide,
    within one decade of its initial operation, a reduction in the
    risk of an unexpected large impact of about 50 percent at a relatively
    modest cost. Of course, additional and much greater expenditure
    would be required to deflect an incoming object if one should
    be discovered on an impact trajectory with the Earth, but in
    that unlikely event the cost and effort would surely be worth
    it. The first and essential step is that addressed by the Spaceguard
    Survey: to carry out a comprehensive survey of near-Earth space
    in order to assess the population of near-Earth asteroids and
    comets and to identify any potentially hazardous objects. 
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