An article for AGU’s EOS (Transactions of the American
Geophysical Union)
New Horizons: NASA’s Pluto-Kuiper Belt Mission
Alan Stern
Southwest Research Institute
Department of Space Studies
1050 Walnut Street, No. 426
Boulder, CO 80302
[303]546-9670
[303]546-9687 (fax)
Andy Cheng
Johns Hopkins Applied
Physics Laboratory
Johns Hopkins Road
Laurel, MD 20723
[240]228-5415
[240]228-6670 (fax)
Revised: 25 February 2002
Introduction
The trans-Neptunian region, containing the binary
planet Pluto-Charon and the myriad planetary embryos of the Kuiper Belt, is a
scientific and intellectual frontier. In
recent years, the Pluto-Charon system itself has become recognized as a key
element for understanding the origin of the outer solar system. So too, it has
become apparent that Pluto-Charon is a scientific wonderland offering insights
into exotic dynamics, the nature of primitive organic material, complex volatile
transport processes, hydrodynamic atmospheric escape, as well as rich surface
and atmospheric chemistry. Pluto’s size, density, albedo, surface composition,
and atmosphere also make it a unique (and likely more primitive) comparator to
Neptune’s, large and complex icy satellite Triton. Further, the
discovery of the Kuiper Belt (KB), within which Pluto-Charon orbits, has fueled
a revolution in our understanding of the origin, architecture, and richness of the
deep outer solar system. Together, Pluto-Charon and the Kuiper Belt provide an
exciting frontier for first-time planetary reconnaissance, with rich
possibilities for illuminating the origin of the outer solar system, the nature
of binary worlds, the interior and surface evolution of small bodies, and the
physics of cryogenic atmospheres.
In this article we describe the Pluto-Kuiper Belt
mission recently selected for development by NASA. This mission, called New
Horizons, involves a team consisting of the Southwest Research Institute
(SwRI), the Johns-Hopkins Applied Physics Laboratory (APL), Ball Aerospace,
NASA/Goddard Space Flight Center (NASA/GSFC), Stanford University, and
scientists from over a dozen other U.S. universities, NASA centers, and research
institutions, including the Jet Propulsion Laboratory (JPL). The goals of the New
Horizons mission are to reconnoiter the Pluto-Charon and the Kuiper Belt;
exploration of the Jupiter system is also planned, as is a limited cruise
science program. In total, the mission will include up to five science flybys
(including Jupiter). These topics are of broad interest to planetary science
and geophysics.
The selection of the New Horizons team
culminated a yearlong NASA process to compete the PKB mission. This process,
announced in December 2000 began with the January 2001 release of a NASA Office
of Space Science Announcement of Opportunity (AO) calling for complete mission
proposals due in April 2001. It continued with peer review leading to a
down-select announced by NASA in June 2001 of two mission study team finalists
from the suite of submitted proposals. These two teams then conducted detailed,
NASA-funded Phase A studies of the PKB mission requirements and implementation
techniques. After Phase A study submission by the two finalist teams in
September 2001, and site visits and detailed peer review of the Phase A study
reports in October 2001, NASA selected of New Horizons as the winning PKB
mission team in November, 2001.
The entire PKB selection process, which was
recommended by NASA’s Solar System Exploration Subcommittee (SSES) and Space
Science Applications Advisory Committee (SSAAC) advisory committees,
represented the first time that an outer planets mission was competitively
selected. The end result of this process was a mission with substantially
greater scientific return but lower cost than the sole-sourced Pluto Kuiper
Express (PKE) mission that NASA was forced to cancel in 2000 owing to
unacceptable projected cost increases.
Pluto-Charon. Because the Pluto-Charon
system is the only planet-satellite system in our solar system that has not
been explored by spacecraft, the state of knowledge about this system is
necessarily more primitive than at any other planet. Despite this, however,
many basic facts are established. These include the radius, mass, and density
of Pluto (each known to better than 10%) and the radius of Charon (known to
7%), and the mass and density of Charon (known to about 25%). Importantly,
Charon is almost precisely half the size of Pluto. Because the system
barycenter is known to be outside Pluto (between the two bodies), the pair
constitute a true double planet— something unique in our knowledge of the solar
system.
Pluto-Charon orbit the Sun
in an elliptical, inclined, 248-year orbit. This orbit is in 3:2 mean motion
resonance with Neptune, which may indicate Pluto (along with Neptune) migrated
outward several AU in the distant past. Perihelion was reached in 1989; the
system is now receding from the Sun. The planet and satellite share a polar
obliquity of 122 deg. Pluto-Charon have reached complete spin-spin-orbit
synchronicity; the pair are the only fully tidally evolved planet-satellite
pair in the solar system. Models based on Pluto’s density, which is very near 2
gm cm-3, indicates its bulk composition is dominated by hydrated
rock, but contains up to 35% water ice. Light organics and other materials are
predicted to be abundant minor constituents.
Pluto’s surface is the most
highly reflective of the planets, with a globally averaged normal albedo of
55%. The surface color is red, much like Triton. Reflectance spectroscopy has
identified N2, CO, CH4, and H2O frosts on the
surface, with N2 being the dominant constituent. Other light
organics resulting from ice radiolysis and other processes are widely expected
to be present. Photometric measurements have revealed a complex lightcurve with
an amplitude of almost 30%, higher than
any other planet in the solar system. The surface has been mapped crudely (500
km resolution) by HST; the maps reveal polar caps and other high-contrast
surface units. Thermal measurements indicate steep surface temperature
contrasts, with bright areas being near 40 K, and dark units being near 60 K.
Pluto’s atmosphere was
discovered by stellar occultation techniques. Its base surface pressure is at
least 3 and perhaps as great as 0.150 millibars; the upper atmosphere has a
temperature of 106 K owing to a near-surface inversion, but the details of this
thermal structure are indeterminate. Hazes and/or discrete clouds may be
present in the atmosphere. Model calculations predict an N2 dominated
atmosphere, with traces of CH4, CO, and a complex suite of
photolysis products. Owing to Pluto’s high orbital eccentricity and its high
axial tilt, strong thermal forcing results. As a result of coupled
ice/atmosphere sublimation thermal balance, strong seasonal pressure cycles
have been predicted, including possible seasonal atmospheric collapse around
2020. Escape rate calculations indicate that Pluto’s atmosphere is likely to be
in hydrodynamic escape, unlike any other planet (but like the early Earth and
Mars).
Charon’s average surface
albedo (35%) is much darker than Pluto’s; its surface color is gray (neutrally
reflecting), and it has only a low amplitude (8%) lightcurve. Its surface
composition appears to be dominated by water ice, but new absorption features
in the mid-infrared have been detected in recent years, indicating the presence
of other, as yet unidentified, surface constituents (possibly including ammonia
or ammonia-hydrates). There has been no definitive detection of an atmosphere.
The origin of the
Pluto-Charon binary is thought caused by a giant impact, much like the
Earth-Moon system. The evidence for this hypothesis is based on the system’s
high specific angular momentum, its high axial obliquity, and the large mass
ratio of the binary. Pluto itself is thought to have been grown in heliocentric
orbit during the epoch of planetary growth in the Kuiper Belt, some 4 Gyr ago.
As such, and owing to its size, it is expected to represent a key sample of the
bulk composition of planetesimals in the trans-Neptunian region.
The Kuiper Belt. The existence of the Kuiper
Belt was first predicted by mid-20th century astronomers such as
Kenneth Edgeworth and Gerard Kuiper. These and other astronomers of the 1930s,
1940s, and 1950s postulated that a debris belt of material left over from
planetary formation might orbit the Sun beyond Neptune. However, the telescope
and photographic technology of the mid-20th century was too
primitive to give astronomers much hope of finding small bodies at these great
distances.. By the late 1980s cometary astronomers, however, found strong
evidence in the inclination distribution of the Jupiter family comets that they
are coming from a disk-like reservoir just beyond Neptune’s orbit. As a result,
a number of searches were begun in the late 1980s for the belt of material that
Kuiper predicted. The first Kuiper Belt Object (KBO) was subsequently
discovered in 1992. This object, designated 1992QB1, is more than
1000 times fainter than Pluto, and probably about 10 to 15 times smaller in
radius.
Over 500 KBOs have now been
discovered, with estimated diameters ranging from 50 to 1200 km. It is expected
that the KBO size distribution includes still smaller objects (comets) and
larger objects (perhaps even up to Pluto’s size).
Based on the amount of sky
left to be searched and the number of faint, distant objects being found in
faint CCD images, it is estimated that over 100,000 KBOs with diameters >50
km may orbit in a disk- or belt-like structure that stretches from 30 to at
least 55 Astronomical Units (AU) from the Sun. This large population means that
the Kuiper Belt is an even greater collection of objects than the asteroid belt
between Mars and Jupiter (the main asteroid belt has only about 1000 objects as
large as 50 km).
Based on analogy to cometary
nuclei and recently-obtained millimeter wave detections, the surfaces of Kuiper
Belt Objects are expected to be very dark, typically reflecting only 3% to 10%
of the light that falls on them. It has been found the KBOs have a wide range
of surface colors, varying from almost gray to very red, but it is not clear
whether this is due to genetic differences among KBOs or evolutionary affects
(e.g., space weathering, collisional resurfacing). There is some evidence for
water ice and more exotic ices on KBOs. It is also not known if KBOs fall into
compositional groups as the asteroid do, though some observing groups have
claimed evidence to this effect. It is believed KBOs consist primarily of
mixtures of water ice and rock, with some amount of organic and other complex
compounds as well. Most KBOs rotate on their axes in a few hours, but some take
days to rotate. In 2001 the first KBO satellites were discovered.
Collisional processes are
known to play a key role in the Kuiper Belt. One significant result of
collisional modeling is that KBOs smaller than ~50 km in diameter cannot have
survived the collisional bombardment over time and therefore must be younger
than the age of the solar system. As a result it is now widely accepted that
the Jupiter Family comets, which have their source region in the Kuiper Belt,
are chips off KBOs created in comparatively recent times by collisions in the
Kuiper Belt.
Computer simulations
indicate that the KBOs formed along with Pluto early in the history of the
solar system. The total mass of the present-day Kuiper Belt is low, in the
range of 0.5 to 1 Earth mass. This is known to be too low to have been able to
form the KBOs in the age of the solar system. It is therefore surmised that the
primordial Kuiper Belt was many (e.g., 50) times its present day mass. This
mass estimate indicates that the primordial solar nebula extended uninterrupted
beyond Neptune’s distance (30 AU), at least to the present-day edge of the main
Kuiper Belt (55 AU). It is not clear if the relative dearth of large KBOs seen
beyond 55 AU is due to a real edge in the Kuiper Belt near this distance, a
decrease in the size and/or albedo of large KBOs, or simply a gap which may
stretch only a few tens of AU with a larger, even more massive belt lying
beyond.
Based on the sizes and
orbits of KBOs, it appears that the Kuiper Belt was well on its way to growing
one or more large planets, perhaps even something the size of the Earth, or
even Neptune, when the growth process was interrupted. It is believed that the
formation of Neptune is what disturbed the region gravitationally and
interrupted this growth. One
consequence of this disturbance is that Neptune’s gravitational influence
caused collisions between objects in the young Kuiper Belt to become very
violent. As a result, much of the mass in the Kuiper Belt was eroded into dust
and subsequently blown away into interstellar space. Similar processes have
been observed to be taking place in what appear to be Kuiper Belts around many
stars in the galaxy, such as Vega and Fomalhaut. This strong connection between
the Kuiper Belt and other solar systems adds impetus to the desire to explore
the Kuiper belt and KBOs further.
The first exploration of the Pluto-Charon system and
the Kuiper Belt promises to be a scientific watershed. It will provide valuable
insights into the origin of the outer solar system and the ancient outer solar
nebula, the origin and evolution of planet–satellite systems presumably formed
by giant impacts, and the comparative geology, geochemistry, tidal evolution,
atmospheres, and volatile transport mechanics of icy worlds.
The New Horizons mission begins with the
launch of a Discovery-class interplanetary spacecraft in January 2006 onto a
trajectory that reaches Pluto-Charon via a March, 2007 Jupiter Gravity Assist
(JGA). Pluto-Charon can be reached as early as 2015 or 2016, depending on the
launch vehicle selected by NASA. Multiple KBOs will be encountered in the five
succeeding years after the Pluto-Charon encounter.
The New Horizons spacecraft design mass is
416 kg, including propellant for a 290 m/s propulsion budget. The spacecraft
subsystems are based on APL’s Discovery/CONTOUR spacecraft. CONTOUR is
scheduled for launch in July 2002. CONTOUR itself, a multiple comet flyby
spacecraft, is based in part on APL’s TIMED earth orbiter mission (launched in
2001). Use of CONTOUR design heritage reduced schedule and cost risk, allowing
a substantial, 22% dry mass margin, a healthy 20% power margin at Pluto
encounter, and a significant, multi-year margin against the NASA AO’s 2020
Pluto-Charon arrival date limit.
This spacecraft will carry four
complementary reconnaissance instruments. The payload consists of the PERSI
Vis/IR/UV remote sensing package, the REX radio/radiometry experiment, the PAM
plasma suite and the LORRI long-focal-length imager. Notably, New Horizons
accommodates an infrared imaging spectrometer, which Voyager did not have, and
which is essential to characterize the composition and the physical state
(including temperature) of the ices on the surface. In addition, New
Horizons will achieve a best imaging resolution at Pluto that is several
times superior to the best achieved by Voyager at Triton, allowing, for
example, better discrimination among possible geologic processes. The
disk-average surface temperatures of the daysides and the nightsides of Pluto
and Charon will be determined by measurement of the microwave brightness
temperatures by REX; surface temperature mapping across each body will be
achieved by measurement of temperature-sensitive spectral features of ices by
LEISA. Table 21provides additional detail regarding the payload and its sensor
suite.
As the next mission to Jupiter,
New Horizons
will
conduct an intensive, 4-month campaign of Jupiter system observations in early
2007. Closest approach will occur in March 2007 at a distance of 45±5 Rj
(as set by the Pluto aim point); this is over three times closer than Cassini’s
Jupiter flyby in 2000-2001. This encounter affords irresistible opportunities
for studies such as long time base imaging studies of atmospheric and auroral
dynamics, new observations of the Galilean and irregular satellites of Jupiter,
and in situ exploration of the jovian magnetosphere.
During the cruise from Jupiter to Pluto, New
Horizons may be able to reach a Kuiper belt escapee (a so-called Centaur
object), but this depends upon groundbased searches finding a suitable target
along the mission trajectory.
The Pluto-Charon encounter begins 6 months prior to
closest approach. For a period of 75 days on either side of closest approach, New
Horizons images will exceed the best the Hubble Space telescope can achieve
at Pluto-Charon. This allows advance planning to optimize the close approach
sequence, and a substantial timebase of disk-resolved images to study
time-variable phenomena such as volatile transport and meteorology.
Table 1. New
Horizons payload overview.
Instrument |
Type |
Sensor Characteristics |
Builders |
PERSI |
Remote sensing suite |
MVIC (panchromatic and four-color CCD imager,
0.4-1.0 microns, 20 microradians/pixel), LEISA
(near infrared imaging spectrometer, wedged filter, 1.25-2.5 l/Dl = 600 for 2.1-2.25 microns and 300 otherwise,
62 microradians/pixel), and ALICE (UV imaging spectrometer, 500-1850 Ĺ,
spectral resolution 3 Ĺ, 5 milliradians/pixel) |
Ball, SwRI, NASA/GSFC |
REX |
Uplink radio science, passive radiometry |
Signal/noise power spectral density 55 db-Hz;
ultrastable oscillator stability 1x10-13 in 1 second samples.
Disk-averaged radiometry to ±0.1 K. |
Stanford U., JHU/APL |
PAM |
Plasma and high energy particle spectrometers |
SWAP (solar wind plasmas up to 6.5 keV, toroidal
electrostatic analyzer and retarding potential analyzer), and PEPSSI (ions
1-5000 keV and electrons 20-700 keV, time-of-flight by energy to separate
pickup ions) |
SwRI, JHU/APL |
LORRI |
High resolution imager |
Panchromatic, narrow angle CCD imager, 0.30-0.95
microns, 5 microradians/pixel |
JHU/APL |
Long focal length approach
imagery will include 40 km-class mapping of the so-called farside hemispheres of Pluto and Charon 3.2 days out (one half the
rotation period of Pluto-Charon). This obviates the well-known farside mapping
dilemma imposed by Pluto’s slow (6.4 d) rotation for a single-spacecraft flyby
mission.
The spacecraft-planet relative
flyby speed of the Pluto-Charon encounter will be 11 km/sec. Near closest
approach, New Horizons will obtain maps of both Pluto and Charon with
km-scale resolution; at closest approach, images at scales as high as 25
m/pixel may be achieved (depending on the final flyby distance selected). In addition, the Group 1
objectives call for mapping the surface composition and distributions of major
volatile species, for which New Horizons will obtain: (i) four-color
global (dayside) maps at 1.6 km resolution, (ii) diagnostic, hyper-spectral
near-infrared maps at 7 km/pixel resolution globally (dayside) and at 0.6
km/pixel for selected areas. Characterization of the neutral atmosphere and its
escape rate will be accomplished by a battery of investigations including: (i)
diagnostic ultraviolet airglow and solar occultation spectra to determine the
mole fractions of N2, CH4, CO and Ar to 1% in total
mixing ratio and to determine the temperature structure in the upper
atmosphere, (ii) radio occultations at both Pluto and Charon, measuring the density/temperature
structure of Pluto’s neutral atmosphere to the surface, (iii) in situ
determination of the atmospheric escape rate by measuring Pluto pickup ions,
and (iv) H Lyα mapping of the Pluto-Charon system in order to determine
the rate of Roche-lobe flow of atmosphere from Pluto to Charon.
Numerous other scientific
objectives will also be carried out during the encounter, as shown in Table 2. New Horizons will achieve the same
objectives at the sample of Kuiper Belt Objects it reconnoiters as it will at
Pluto-Charon.
Table 2. New Horizons Pluto-Charon and KBO
measurement objectives.
Group 1: Required by the NASA
PKB AO |
Characterize the global geology
and morphology of Pluto and Charon |
Map surface composition of
Pluto and Charon |
Characterize the neutral
atmosphere of Pluto and its escape rate |
Group 2:
Highly Desired by NASA PKB AO |
Characterize the time
variability of Pluto's surface and atmosphere |
Image Pluto and Charon in
stereo |
Map the terminators of Pluto
and Charon with high resolution |
Map the surface composition of
selected areas of Pluto and Charon at high resolution |
Characterize Pluto's ionosphere
and solar wind interaction |
Search for neutral species
including H, H2, HCN, and CxHy, and other hydrocarbons and
nitriles in Pluto's upper atmosphere |
Search for an atmosphere around
Charon |
Determine bolometric Bond
albedos for Pluto and Charon |
Map the surface temperatures of
Pluto and Charon |
Group 3:
Cited as Desirable in the NASA PKB AO |
Characterize the energetic
particle environment of Pluto and Charon |
Refine bulk parameters (radii,
masses, densities) and orbits of Pluto and Charon |
Search for additional
satellites and rings |
Concluding
Remarks
The New Horizons mission team is excited to
initiate the development of the PKB mission for NASA. Congress funded the PKB
effort sufficiently to complete the detailed design effort and to initiate
certain long lead-time procurements in FY2002. Further development of the
mission will require sustained funding in FY2003 and beyond. If NASA is funded
to complete New Horizons and launch it, the result should be the long
awaited reconnaissance of the planetary system’s third domain and final
frontier— Pluto-Charon and the Kuiper Belt.
The New Horizons project intends this
reconnaissance to benefit the entire community and the U.S. public. Efforts to
accomplish this broad-based return include an active, well-funded Education and
Public Outreach (EPO) program, a rapid (days timescale) data dissemination
policy, and an $11M funding block within New Horizons for NASA-selected
participating scientist and data analysis efforts by members of the U.S.
national planetary science community.
The first exploration of the last known planet in
the solar system is an exciting possibility, with strong prospects for
providing the public with a renewed sense of drama and excitement in planetary
exploration. Equally importantly, in achieving its geophysical, geochemical,
geological, and atmospheric science objectives, the Pluto-Kuiper Belt mission
will open the study the origin and evolution of binary worlds and Kuiper Belt
Objects, and in doing so, address some of the most compelling questions in all
of planetary science.
Alan Stern is the Principal
Investigator of the New Horizons mission. Andy Cheng is the Project Scientist
for New Horizons. Additional information on New Horizons can be found at http://pluto.jhuapl.edu and www.boulder.swri.edu/pkb.
Figure 1. Upper panel: The New Horizons spacecraft and key components. The high-gain Communications antenna is 2.5 m in diameter. Lower panel: Heliocentric trajectory schematic.