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The
Testimony of Dr. Lindley Johnson, Program Manager, Near Earth Objects
Observation Program, National Aeronautics and Space Administration
(NASA)
Given at a
Senate Science, Technology, and Space Hearing: Near Earth Objects (NEO)
Wednesday, April 7 2004 - 2:30 PM - SR -253
Thank you, Mr.
Chairman, for the opportunity to present to the subcommittee information
on the important subject of Near Earth Objects. At the request of
Congress, NASA conducts the Near Earth Object (NEO) Observation Program
to discover the larger sized asteroids (greater than 1 kilometer or 0.62
miles in size) and periodic comets that pass relatively close to the
Earth and may one day pose a collision hazard with our planet. Our NEO
program has been quite successful in finding these larger objects in the
first five years of the effort.
BACKGROUND
The Earth orbits
about the Sun in a cloud of planetary debris still left from the
formation of the Solar System. This debris ranges from micron-sized dust
particles, to meteoroids at sand grain to a few meters in size, and to
asteroids and comets that are tens of meters to several kilometers in
dimension. Collision with meter-sized meteoroids is almost a weekly
event for the Earth, but the surface is well protected from these common
events by its atmosphere, which will cause objects less than about 50
meters in size and of average density to disintegrate harmlessly before
reaching the ground. However, even the relatively active surface of the
Earth still bears scars of impacts from space, with 168 craters
worldwide - some up to 300 kilometers in size - having been identified
to date.
Though collisions
with larger bodies are much less frequent now than in the early stages
of planet formation in the Solar System, they do still occur. Very
significant events, capable of causing damage at the surface, will
happen on scales of a few hundred to a thousand years. But we do not
know when the next impact of an object of sufficient size to cause
widespread devastation at ground level may occur. At the current state
of knowledge, it is about as likely to happen next week as in a randomly
selected week a thousand years from now.
The Survey
In an effort to
gain better understanding of this hazard, NASA has been conducting a
search of space near the Earth's orbit to understand the population of
objects that could do significant damage to the planet should there be a
collision. Commonly referred to as the "Spaceguard Survey", NASA's
Office of Space Science conducts this research effort on "Near Earth
Objects (NEOs)" -- that is, asteroids and comets that come within an
astronomically close distance, <50 million kilometers of Earth. The
objective of this survey is to detect, within a 10-year period, at least
90% of the NEOs that are greater than 1 kilometer in size and to predict
their orbits into the future. The survey officially started in 1998 and
to date, over 700 objects of an estimated population of about 1100 have
been discovered, so the effort is believed to now be over 70% complete
and well on the way to meeting its objective by 2008.
A few words of
explanation on the parameters and limitations of the survey may be
appropriate. The threshold of 1 kilometer in size was accepted for this
survey because it is about the size asteroid that current research shows
would border on having a devastating worldwide effect should an impact
occur. Because of the orbital velocities involved, impact on Earth of an
asteroid of this size would instantly release energies calculated to be
equivalent to the detonation of almost a 100,000 megaton nuclear device,
i.e., more than all the world's nuclear arsenals detonated at the same
time. Not only would the continent or ocean where the impact occurs be
utterly devastated, but the effects of the super-heated fragments of
Earth's crust and water vapor thrown into the atmosphere and around the
world would adversely affect the global weather for months to years
after the event. Such an event could well disrupt human civilization
anywhere from decades to a century after an impact.
A goal of 90%
completeness was adopted as a compromise driven between the level of
resources that could be dedicated to this effort and the time period
practical to conduct the survey at this level of technical capability.
Currently, slightly over $4M per year is budgeted to the NEO Observation
Program within the Solar System Exploration Division's Supporting
Research and Analysis Program. This funds modest search efforts,
typically using refurbished, ground-based telescopes of about 1-meter
aperture and wide-field-of-view, coupled with digital imaging in order
to cover significant portions of the sky each month. Presently, five NEO
search projects are either wholly or largely funded with this level of
resource, along with significant support to central processing of
observations, orbit determination and analysis. These five search
projects are:
PROJECT NAME,
INSTITUTE, PRINCIPAL INVESTIGATOR
-
Lincoln Near Earth Asteroid Research (LINEAR), MIT /
Lincoln Laboratory, MA, Dr. Grant Stokes
-
Near Earth Asteroid Tracking (NEAT), Jet Propulsion
Laboratory, CA Dr.Ray Bambery
-
Lowell Observatory Near Earth Object Search (LONEOS),Lowell
Observatory, AZ, Dr. Edward Bowell
-
Catalina Sky Survey, LPL, University of Arizona Mr.
Steve Larson
-
Spacewatch LPL, University of Arizona, Dr. Robert
McMillan
Both the LINEAR
and NEAT projects operate using optical telescope facilities owned and
supported by research components of the U.S. Air Force. This represents
that service's entire contribution to the search effort, but utilization
and direction of these assets must be coordinated with the cognizant Air
Force Material Command offices. The Spacewatch Project also receives
some modest private funding.
Ten years was
considered a reasonable amount of time for this level of effort to bring
the overall large asteroid population known to 90% completeness. No
level of effort could ever be assured of achieving absolute 100%
completeness, because of the vast difficulty in searching all possible
orbit regimes and sources for generation of new NEOs. It should also be
understood that the NEO Observation Program is merely a science survey
and does not have the resources to provide a "leak-proof" warning
network for impact of any size natural object, large or small. Such a
comprehensive network would require an order of magnitude increase in
funding and could require the cooperative efforts of several government
departments and agencies.
PROGRESS OF THE
PROGRAM.
The NEO
Observation Program continues to make steady progress toward the goal of
finding at least 90% of the large NEO population. As of the end of March
2004, 513 of the 750 known NEOs (including 49 Earth-approaching comets)
determined to be larger than 1 kilometer in size have been found by the
program, of an estimated total population of about 1100. In addition,
the program found 1862 of 2032 known Near Earth Asteroids (NEAs) of
smaller sizes. The MIT/Lincoln Labs-led LINEAR project continues to be
the leading search team, having found 40 large NEOs in 2003 along with
196 smaller objects. Significant contributions continue to be made by
JPL's NEAT team (10 large and 58 smaller objects in the last year),
Lowell Observatory's LONEOS project (10 and 44), and the University of
Arizona's Spacewatch project (2 and 54). The Lunar and Planetary
Laboratory Catalina Sky Survey has gotten back on line in the last few
months of the year after an imager upgrade, obtaining 8 discoveries, 2
of them larger than 1 km.
The chart below
summarizes the progress to date on finding the NEAs greater than 1
kilometer in size. A noticeable increase in the discovery rate occurs
after the NEO Observation Program started in 1998.
Budget. The FY
2004 budget for this program is $4,062K, a 2.8% increase to the previous
year.
CURRENT SURVEY
OPERATIONS
Detection. The NEO
Observation Program wholly funds the operations of four search projects
and partially funds another. Routine operation of these assets is highly
automated, in order to maximize the sky coverage obtained each month.
Ground-based telescopes can only effectively operate at night during the
two to three weeks of the month opposite the full moon, due to the sky
brightness it causes, and when weather (cloud cover) permits accessible
clear sky. Telescope movement, pointing, and imaging operations are all
computer controlled via pre-scripted software routines to optimize sky
coverage and therefore maximize object detections.
The images taken
each night are then post-processed to detect moving objects relative to
the star background and obtain accurate measurements, called
"observations", of any detected object's motion relative to the star
background (a process called "astrometrics"). A group of these
observations, usually a set taken from three to five images of the same
patch of sky at slightly different times each night, is called a
"track". These show the relative motion of an object, which can then be
analyzed with other observations of the same object to determine its
orbit. These observation tracks are then formatted for bulk
telecommunications to the Minor Planet Center. On a productive night, a
search project may extract hundreds of observations on moving objects
from its imaging data, most of which will be on Main Belt Asteroids and
only a small fraction, perhaps one or two if lucky, will be determined
to be NEOs. The search teams also routinely find comets in their
collected images.
The Minor Planet
Center. All observations thought to be natural small bodies (asteroids,
comets and now Kuiper Belt Objects in the outer Solar System) are sent
to the Minor Planet Center (MPC), operated by the Smithsonian
Astrophysical Observatory at Cambridge, Massachusetts, under the
direction of Dr Brian Marsden. The MPC is internationally recognized and
officially chartered by the International Astronomical Union to confirm
the discovery of new objects in the Solar System and confer their
official designations. A modest amount of NASA funding is sent to the
MPC to support their work in confirming NEO detections.
The MPC receives
observations from around the world, with a significant percentage coming
from an informal international network of amateur asteroid hunters. The
orbital analyst at MPC attempts to correlate them with the positions of
tens of thousands of already known objects. Failing that, the MPC will
provisionally designate the observations as a possible new object,
determine an "initial" orbit for it, and place it on a list for objects
awaiting "confirmation". This list of provisional objects, along with
their predicted current positions, is available via the MPC web site for
the community of observers to use in attempts to obtain additional
"follow-up" observations to confirm the existence and orbit parameters
of a new object.
The observation
processing at the MPC is highly automated, as it must be with a staff of
only three to four analysts operating with a very limited budget.
However, initial orbit determination often requires some analyst's
massaging of the orbit fit to obtain the lowest residuals across what
may be observations with some inherent errors. Because individual search
sites can only do the roughest of orbit calculations based on their own
limited data, the MPC is, in most cases, the first place where it will
be known if a newly found object poses an impact hazard to the Earth.
Often a family of possible orbits is initially obtained which must be
narrowed with additional observations. For newly found NEOs, the MPC
solicits additional observations from the community via a web-based "NEO
Confirmation Page", and in the most critical cases, via phone calls to
known observers in whatever part of the world is most likely to have the
earliest accessibility to viewing the object.
Follow-up
Observations. Additional observations, either obtained by another
observer later the same night or on a subsequent night, even by the same
facility that first discovers an object, are essential to confirming the
objects existence and developing a more accurate orbit for the object.
For the most accurate orbit, it is best for the observations to be
obtained several days to a week or more after the initial set in order
to obtain a longer observed "arc" of the orbit and, therefore, a broader
fit of observation data. However, for NEOs, the time allowed to elapse
must be traded off between obtaining a broader arc and getting an orbit
established before the object is lost, either because the initial orbit
was too far in error, or, more likely, the object is so small that it
simply cannot be seen after only a few days of its closest approach to
Earth.
The informal
network of amateur astronomers does much of the follow-up observation
work today. However, the search for NEOs is beginning to enter an era
when the objects being detected are simply too faint to be seen by the
equipment affordable to most amateurs. Therefore, in the future, search
systems must ensure they have enough survey capacity available to do
their own follow-up on new objects in a timely manner.
High-accuracy
Orbit Determination. The best orbit determination requires enough
observations spread over a sufficient arc of the orbit to provide the
best resolution of motion for the object and reduce the influence of
subsets of data with may have some components of error. Again, getting
the best results can be somewhat of an art form, but the best orbital
modeling for this reside with the NEO Program Office established by NASA
at the Jet Propulsion Laboratory in Pasadena, California, and managed by
Dr. Donald Yeomans. This office also supports the orbit determination
and navigation for NASA's interplanetary missions to asteroids, comets,
and moons of other planets. Its NEO work is fully funded by NASA, and
the high-accuracy orbit determination capability is nicely complementary
to the MPC's observation processing and initial orbit determination
abilities.
The NEO Program
Office is able to use its orbital modeling capability to predict the
position of any known NEO up to 200 years into the future, taking into
account all the known gravitational influences and orbital perturbations
of the Sun, planets, and moons in the Solar System. This can be done
with a very high degree of precision for asteroids that have been
tracked for extended periods, particularly multiple orbits, or for which
high-precision observations have been taken by planetary radar.
High-precision radar observations can greatly reduce the position and
motion errors for the subset of objects that come close enough to the
Earth to allow its use.
High-precision
prediction of newly discovered NEO orbits allows them to be separated
into those whose orbits will not be a collision hazard to Earth for the
foreseeable future and those which are in orbits that pass close enough
to Earth's that they may someday pose a hazard. These "Potentially
Hazardous Asteroids (PHAs)" are about a 20% subset of all NEOs found. Of
course, known and unknown errors in the NEO's orbital parameters can
propagate out to significant uncertainty in the position when
predictions are done decades into the future. Therefore, periodic
observation of known objects, especially those known to be in
potentially hazardous orbits, must be done to update the last known
position and reduce the orbit errors.
Low
Probability, High Consequence Events on Short Timelines
A central premise
of the current survey effort is that in the relatively short 10-year
period, the search teams would be able to find almost all asteroids of
greater than 1 kilometer dimension that might pose a threat of impact -
many years to multiple decades before any such event. It could perhaps
even provide many centuries advanced notice, since this level of event
is thought to happen only once or twice in a million years.
Hypothetically, this would allow ample time to develop the techniques
and technologies that may be required to deflect or mitigate a predicted
disaster. But until the total population of these objects is known,
there is always a chance that an object bound for a nearer term impact
may be discovered, similar to the real-life scenario which unfolded when
Comet Shoemaker-Levy 9 was discovered in March 1993 inbound for a July
1994 impact on Jupiter.
The results of a
recent study by a Science Definition Team commissioned by NASA's Solar
System Exploration Division show that it is entirely appropriate that we
search for the larger NEOs first because, all factors considered, that
is where the greatest risk for an undetected asteroid on an impact
trajectory lies, principally due to the widespread devastation it would
cause. It is orders of magnitude above what smaller, sub-kilometer sized
impactors would produce. Completion of the current effort to find these
large objects will do much to reduce the uncertain risk of which we have
now become aware.
But more frequent
would be the discovery of a relatively small asteroid on a potential
impact trajectory with Earth, as this occurs more often. Since the
optical sensors used in the survey detect the brightness of the object
against the sky background, which can only be approximately related to
an asteroid's size based on assumed reflectivity of light, the search
systems are as capable of finding smaller asteroids at closer range as
larger objects much farther away. They are designed to detect 1
kilometer sized asteroids at least 50 million kilometers distant but can
also detect an asteroid a dozen meters in size within the Moon's
distance from Earth.
Operational
experience with the current systems shows that for every 1-kilometer or
greater sized asteroid found, there are three to four smaller sized
asteroids also discovered. But the true ratio of smaller asteroids, say
100-meter or larger objects to 1-kilometer or larger objects, is thought
to be closer to 100 to 1. Because of the limitations of the search
systems, the discovery of smaller asteroids is in a significantly
smaller volume about the Earth -- an object one tenth the size of
another must be about hundred times closer to be seen by the sensor,
assuming equal reflectivity of their surfaces. If the sensor can detect
a 1 kilometer sized asteroid at 50 million kilometers, it should
theoretically also see a 100-meter asteroid at 500,000 kilometers.
However, at
planetary relative orbital velocities, if the object is on collision
course with the Earth, it may cover even this distance in less than one
day. Thus the detection of a relatively small asteroid on a collision
trajectory with Earth could also come with a relatively short reaction
time. A 100 meter asteroid on direct collision with Earth could do
significant damage at the surface as this is estimated to result in an
approximately 50 megaton energy release at or perhaps slightly above the
surface. This would result in much loss of life if the impact were in a
populated area. It is therefore prudent that we begin to put in place
some contingency plans, such as an internal NASA notification plan we
are drafting, to deal with such a relatively unlikely but extremely
high-consequence event.
Again I thank you
for the opportunity to appear and would be happy to respond to any
questions.
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