
After Apollo interest in further scientific examination of the Moon seemed to rachet down almost to "nil". But as various nations have succeeded in establishing viable space programs, the Moon once again has been targeted for renewed exploration during the first decade of the 21st century.
The views presented so far highlight
the two dominant characteristics of the lunar surface: 1) the mare/highlands
dichotomy, and 2) the abundance of circular features, nearly all being impact
craters and basins but some of probable volcanic (caldera) origin. This next
scene emphasizes both characteristics by showing an exaggerated false-color
image of the front side of the Moon, taken by the multispectral vidicon onboard
the Galileo spacecraft (described later in this Section). The highlands, with
their higher reflectances, appear in shades of red and orange and the lower
reflectance maria are in blues and greens. After Apollo, the Moon was not specifically
revisited for 22 years, until an unmanned spacecraft, Clementine (funded by
the Department of Defense), orbited it to conduct mapping studies between February
19 and April 21, 1994, using UV/Visible, Near IR, and High Resolution Cameras,
Lidar (a radar altimeter), and a radar-like unit that transmits in the S-band
radio frequency (2.293 GHz, or 13.19 cm wavelength).
Look first at a topographic
map of the front and far sides of the Moon, in which stereo data provided elevation
differences from high resolution photographs and radar altimetry data, acquired
by the Clementine spacecraft as it orbited the lunar surface. In the Far Side view, note the low topography around the South Pole. 
As explained in the next paragraph, image data at various wavelengths can be used to map compositional differences in much the same manner as with multiband data obtained by Landsat and other terrestrial spacecraft. Below is an image of the 40 km wide crater Aristarchus that is found in the southeastern part of Oceanus Procellarum. The composite image is constructed from three ratio images (input bands in units of micrometers [µm]): 0.750/0.415 = red; 0.750/1.00 = green; 0.415/0.750 = blue. The dark gray surface is mare basalt; the reddish unit is ejecta from Aristarchus; the light blue is probably anorthositic rock (common in the highlands) exposed in the crater interior:

Among specialized products were more detailed maps of lunar topography (elevations) and global maps of the distribution of several chemical elements, such as iron (Fe) and titanium (Ti), determined by analyzing reflectance variations at 0.75 m m and 0.95 m m, where these elements absorb irradiation. Most of the iron is actually in the form of FeO (reduced iron). The Clementine results when plotted as FeO are thus:

While iron is widespread, its maximum concentrations are in a broad region on the nearside, roughly coincident with the vast lava outpourings into Oceanus Procellarum and several other mare basins.
Clementine made a controversial discovery, which, if proved correct, has major implications for humans returning to the Moon. Its S-band radio unit detected abnormal reflections from the rim of a
huge crater (basin) around the lunar South Pole, in areas permanently sheltered from the Sun's rays, as seen in this Clementine image:
These reflections could be due either to water ice or to some abnormal
surface roughness condition. If indeed ice is present in significant quantity, then this precious material (which supplies water needed for life and
also oxygen, when broken down by electrolysis) might allow future astronauts to establish a
manned base on the Moon. Transport of sufficient water and oxygen for long stays
is presently beyond the space program's technical capability. Because the South Pole region is a candidate for an eventual lunar base, radar units from Earth have returned high resolution images of the polar terrain, without so far having confirmed the presence of ice. Here is an image made at 13.2 cm wavelength, from the Arecibo radar dish in Puerto Rico (no ice was identified at the 20 m resolution of this system).
The observation of possible ice, and other intriguing
results of Clementine's compositional mapping, has led to a follow-on mission.
For the first time in 25 years, NASA has returned to the Moon with a small,
but versatile orbiting satellite, called Lunar Prospector. The entire mission
including data analysis is another effort by NASA to achieve high scientific
returns at relatively low cost (for LP, $65 million). Launched on January 6,
1998, by an Agena rocket, Prospector now is operating in a 100-km high circumlunar
polar orbit, from which it can map the entire Moon over a 3-year lifetime in
more detail than Clementine provided. Here is an artist's sketch of the spacecraft:
The spacecraft, just 1.4 m (4.5 ft)
high and 1.2 m (4 ft) in diameter, weighing 300 kg (660 lbs), receives its power
from solar cells that surround its exterior. An S-band radio sensor designed
to measure lunar gravity employing a Doppler effect procedure, sits on top of
a conical communications antenna (top). At the end of the 8-ft boom or mast
extending to the front left, a Magnetometer/Electron Reflectometer will conduct
improved measurements of the Moon's magnetic and particle fields. At the end
of the left rear mast is the Gamma Ray Spectrometer, which can detect these
elements: U, Th, K, Fe, Ti, O, Si, Al, Mg, and Ca. On the right boom are the
Alpha Particle Spectrometer that will measure radon gas to assess lunar radioactivity
as a clue to volcanic and other current events, and the Neutron Spectrometer
that will determine the presence of hydrogen and can detect water ice (its confirmation
from Clementine results is a major goal). A plot of the varying thermal neutron
flux, as determined by the Neutron Spectrometer, show a wide area of low neutron
counts (resulting from high neutron capture) associated with the maria on the
frontside and near the North Pole and higher counts in the highlands. Compare the distribution of Fe as determined by Lunar Prospector (below) with the same coverage by Clementine shown above: Information on the distribution of radioactivity on the lunar surface was one goal of Lunar Prospector. This map shows that the element thorium is highest on the front side of the Moon, mainly in the highlands south of Mare Imbrium. The correspondence with the Imbrium Basin suggests that the basaltic lavas that filled it were enriched in Th. Note that corresponding highland surfaces on the farside are lower. The first results on Lunar Prospector's detection of ice
were released during an exciting press conference, held on March 5, 1998. Around
both poles, the neutron spectrometer has indeed detected neutrons, released
from hydrogen by natural cosmic ray bombardment of water ice in craters that have permanently sheltered shadow zones. The drop in neutrons emanating from the Moon is clearly maximal around the poles as seen in this plot.
The initial estimate of the amount, to be determined
more accurately with later observations, is 30 to 300 million metric tons (recent thinking has raised the upper limit to perhaps as high as 3 billion tons). If melted,
this larger number would fill a "lake" 10 square kilometers in area
(3.1 x 3.1 km) to a depth of 10 meters. Surprisingly, the North Pole region
contains about 50% more ice than its southern counterpart. The source of the
water ice is probably residues from cometary bodies that impacted the polar
regions, forming craters but allowing much of the comet mass to survive embedded
in the target. The implications are encouraging for future exploration of the
Moon, to the extent that we can establish and occupy a manned base facility
over extended time because of the availability of vital water (for consumption
and as a source of hydrogen, suitable as a fuel). Landing in polar
regions is technically more difficult but doable. The dream of a permanent observation
post on our satellite is now much more feasible. More details on Lunar Prospector
are given at the National
Space Science Data Center Web site and the Mission Management Home Page
at NASA Ames Research Center. As NASA
accrues and releases data and maps, we will place them in the Web version of
this Tutorial and in later CD-ROM versions. An important mission to the Moon is ESA's SMART-1 spacecraft. Launched September 27, 2003 as Europe's first venture in exploring beyond Earth, the spacecraft, using a novelion (Xenon gas) propulsion system, proceeded slowly to the Moon and then arrived in November of 2004.





SMART-1 is Europe's first lunar mission and has provided some significant advances to many issues currently active in lunar science, such as our understanding of lunar origin and evolution. The mission also contributes a step in developing an international program of lunar exploration. The spacecraft was launched on 27 September 2003 on an Ariane 5, as an auxiliary passenger to Geostationary Transfer Orbit (GTO), performed a 14-month long cruise using the tiny thrust of electric propulsion alone, reached lunar capture in November 2004, and lunar science orbit in March 2005. SMART-1 carries seven hardware experiments (performing 10 investigations, including three remote sensing instruments, used during the cruise, the mission's nominal six months and one year extension in lunar science orbit). The remote sensing instruments will contribute to key planetary scientific questions related to theories of lunar origin and evolution, the global and local crustal composition, the search for cold traps at the lunar poles and the mapping of potential lunar resources.
This low cost satellite orbited the Moon for nearly two years gathering information about surface composition. Its instruments are:
AMIE: A miniaturised color camera with a resolution of 40 meters for lunar surface imaging.
SIR: A near-infrared spectrometer for lunar mineralogy studies.
D-CIXS: A compact X-ray spectrometer to perform fluorescence spectroscopy and map the Moon's surface elemental composition. It also performed observations of celestial X-ray sources while en route to the Moon.
XSM: An X-ray monitor to support D-CIXS with measurements of solar X-ray emission for calibration. It also observed solar flares while en route to the Moon.
Here are two images made by AIME of the lunar surface.

Below are an AIME view of the central peak of Crater Zucchius and ejecta around Mare Orientale:


Here is a SIR mineral map of a cratered area on the Moon:

The D-CIXS detects X-ray fluorescence of minerals that are being excited by X-rays from the Sun. This is a map of Calcium distribution within a small area of the Moon around Mare Crisium:

SMART-1 spent a lot of time looking at the polar regions, partly to search for evidence of possible water ice. In so doing, it provided information on the Aitken impact basin, some 2500 km in diameter, reputedly the largest such structure in the Solar System. Here is a map of the South Polar region showing this structure:

SMART-1 ended its mission by being deliberately impacted onto the lunar surface on September 3, 2006.
The Chinese and Japanese have sent probes to the Moon in 2007 and 2008 respectively.This is an artist's view of the China's Chang'e-1 spacecraft, which was launched on October 24, 2007:

The first image from Chang'e-1 is shown here:

This panel shows the types of products coming from Chang'e-1:

The contrast in this Chang'e-1 image of the craters at the lunar South Pole is interesting:

Chang'e-1 was sent to the lunar surface (crashed) on March 1, 2009.
Japan's spacecraft, Kaguya (Selene), is primarily an imager but it does have 13 separate instruments. Here is how it looks:

These are typical images of the lunar surface as captured by Kaguya:


Here are Kaguya images of the rim and the central peak of the crater Tycho:


This is Tycho's image of Mare Muscovensis on the lunar far side:

Unlike the earlier U.S. orbiting imagers, Kaguya can produce quasi-color images:

An interesting Kaguya image shows the disturbed soil around the site where the Apollo 15 LM took off more than three decades earlier:

One of Kayuga's task was to search for water, especially in the polar regions. Its instruments dedicated to that search came up with no positive evidence of water. At face value, that may seem discouraging but perhaps the sensors were inadequate for that purpose. The question remains moot.
Kayuga ended its mission on June 10, 2009 by crashing onto the lunar surface. The crash was observed from Earth. This is a sequence seen through the Anglo-Australian telescope:

The impending crash itself was monitored by Kayuga as its approached the surface. Here are two of several images sent back just before contact:


India launched its first outer space probe towards the Moon on October 22, 2008. Named Chandrayaan-1, the spacecraft has multiple instruments from several nations. NASA's contribution are the MiniSAR and M3 (Moon Mineralogy Mapper, which will gather data in both the Visible and IR parts of the spectrum). Data from Chandrayaan (shown below) started to be received by mid-November:


NASA's JPL has an instrument onboard Chandrayaan-1, called the Moon Mineralogy Mapper (m3). One of the first products released to the public is this image in which iron minerals are shaded green:

In September of 2009, NASA and several scientific groups made headlines with the announcement that water has been detected over most of the lunar surface. The amounts are miniscule by earth standards. The soil spread over any area comparable to a football field in size hold a cumulative amount of water sufficient to fill an ordinary drinking glass. But the discovery is important since it indicates that water does occur in non-polar latitudes. This illustration, based on Chandrayaan-1 data, indicates typical distribution:


Following President Bush's policy statement on its long term goals, NASA is also committed to re-explore the Moon. Two missions slated for launch together in mid-2009 are LCROSS (Lunar Crater Observing and Sensing Satellite), which will try to validate the evidence for water ice at the poles ultimately by crashing a probe onto the surface, and LRO, the Lunar Reconnaissance Orbiter.
The two satellites were successfully launched by an Atlas 5 rocket on June 18, 2009 and will enter orbit with perilune at 35 and 50 km respectively. The LRO spacecraft is pictured below. These are its onboard instruments:

The Cosmic Ray Telescope for the Effects of Radiation (CRaTER) will characterize the lunar radiation environment and determine its potential biological impacts. CRaTER will also test models of radiation effects and shielding, which may enable the development of protective technologies.
The Diviner Lunar Radiometer (DLRE) will provide orbital thermal mapping measurements, giving detailed information about surface and subsurface temperatures (identifying cold traps and potential ice deposits), as well as landing hazards such as rough terrain or rocks.
The Lyman Alpha Mapping Project (LAMP) will map the entire lunar surface in the far ultraviolet. LAMP will search for surface ice and frost in the polar regions and provide images of permanently shadowed regions illuminated only by starlight.
The Lunar Exploration Neutron Detector (LEND) will create high resolution hydrogen distribution maps and provide information about the lunar radiation environment. LEND can be used to search for evidence of water ice on the Moon's surface, and will provide space radiation environment measurements useful for future human exploration.
The Lunar Orbiter Laser Altimeter (LOLA) will measure landing site slopes, lunar surface roughness, and generate a high resolution 3D map of the Moon. LOLA will also identify the Moon's permanently illuminated and permanently shadowed areas by analyzing Lunar surface elevations.
The Lunar Reconnaissance Orbiter Camera (LROC) will retrieve high resolution black and white images of the lunar surface, capturing images of the lunar poles with resolutions down to 1m, and will image the lunar surface in color and ultraviolet. These images will provide knowledge of polar illumination conditions, identify potential resources & hazards, and enable safe landing site selection.
The Mini-RF technology demonstration's primary goal will be to search for subsurface water ice deposits. In addition, Mini-RF will take high-resolution imagery of permanently-shadowed regions.
The first LRO image was released on July 2, 2009. It shows a scene 1800 meters across in cratered terrain within Mare Nubium: This image shows part of the crater Hahn; below it is a series of secondary craters formed from ejecta from a distant large impact crater: The montage below shows five of the Apollo landing sites; arrows point to the base equipment from which the LMs were launched.: So, how good is the image resolution obtained by LRO? In this next image, again of the Apollo 14 landing site, some of the tracks made by the walking astronauts are visible as dark streaks: LRO carries Mini-RF, a SAR-type radar instrument whose main task is to search for ice, especially in the polar regions. Here is a radar strip of terrain near the South Pole. LCROSS is treated as a separate mission. After establishing orbit, sensors (visible and spectrographic) on LCROSS are programmed to examine craters in the polar regions
seeking more detailed evidence that any of these contain water. The final event, at 4:35 AM PDT on October 9, 2009 is a one-time-only "shoot the moon", in which the Centaur rocket upper stage was made to crash onto the south polar surface at a small crater, Cabeus A, that looks promising as containing ice. The LCROSS remained nearby in orbit to observe the collision and the ejecta spray or plume produced by the first impact
Following that, this shepherding spacecraft was deliberately crashed onto the same Cabeus A. Here is an artist's sketch of LCROSS as the impacting projectile is
released:





Expectations were high that the collision and resulting plume would be "spectacular". Professional and amateur observatories on Earth were trained on the polar region. No one in fact saw much of anything. LCROSS itself picked up a brief flash but no obvious plume. (The writer explains this as a consequence of the dark material in any such plume lacking notable contrast against the dark surface of the crater itself.) The spectrograph did pick up a strong signal but this will take awhile to be analyzed.
In the next three images, we show first the target crater, then a sequence of four images made by LCROSS just after Centaur impact, and finally an image which shows the Centaur impact as a bright flash:



Some two weeks after launch, an image of the faint plume was processed and released to the public. To make it visible, the scene had to be strongly contrast-stretched, making the lighter tones almost white. Here it is:

The lunar probes shown above are all providing new data that will help in planning for eventual manned Moon missions. The question now being asked: Is such a resumption of exploration by humans affordable in the current world economy?
As mentioned earlier in this Section, NASA and other space agencies have started planning a manned return to the Moon under the mandate given by Pres. George W. Bush (which, unfortunately, could be scaled back or scratched by his successors). A new, more versatile Space Transportation System will be needed, and calls for proposals are now out. The first landings will probably be more like the Apollo ones but in time it is hoped to establish a permanent (or at least long term) lunar base where astronauts can subsist and explore for extended stays. Four things are essential in making a safe, flexible base: 1) a means of replenishing oxygen; 2) water; 3) source(s) of power; and 4) suitable shielding from extralunar radiation.
Oxygen, in principle, is extractable from the lunar silicate minerals but a reliable, practical means of obtaining this is yet to be worked out (in May 2005, NASA issued a Call for Proposals for innovative solutions). Water can, in part, be recycled from sources (such as astronaut urine) brought with the explorers. But, if substantial water is found near the polar regions, extraction should not be too difficult - thus the base would likely be located at high latitudes. Power requirements can be met with nuclear generators and/or with efficient solar arrays. Shielding may prove difficult since the base units (presumably separate from the landing craft) need to be of light materials. Still, growing experience should aid in selecting radiation-absorbing outer components of the base.
There is another strong argument for selecting polar regions for the base besides the water potential. Placing astronomical observatories at either or both poles would allow almost ideal observing conditions (for some applications better than the present Hubble Space Telescope since systems and components would be state-of-the-art). Nearly all of both celestial hemispheres would be accessible, whereas locating an observatory at lower latitudes would have some light interference from earthshine. But exploration would be curtailed somewhat by dependence on a polar station.
A recent National Academy of Sciences report offers another cogent argument for resumption of Moon visits: The observatory that would eventually be built would be of immense value in astronomical studies and in continual monitoring of the Sun. But, even more valuable to earth-dwellers, 21st Century technology operating through telescopes would produce copious data on the Earth itself. While geostationary satellites can do some of that, the fact that any part of the non-polar Earth is bathed in sunlight every 24 hours makes "observation on demand" feasible. The value of the Moon as a platform was demonstrated during Apollo 16 when astronaut John Young pointed a geocoronagraph towards Earth, getting this image that shows a shroud of low density excited hydrogen around much of the planet:

Establishment of a Moon base will be a giant step in mankind's renewal of outer space exploration. Among its benefits, it could serve as the launching site for a trip to Mars. On September 18, 2005 NASA made its first public announcement of how its approach to how the Moon landings (and probably Mars later) will be made. There is a striking similarity to the Apollo approach in that landing craft will be on a large multistage rocket, with the main thrust section falling back to Earth after putting the manned vehicle on its journey. This vehicle and a companion for sending material to build a lunar base shown here, with other existing vehicles side by side for comparison:

A closer look at the rocket that would carry a crew of into lunar orbit is pictured here. At its tip is the Crew Exploration Vehicle (CEV).
This panel diagram shows the sequence of events or stages now envisioned in the current plan for renewed lunar exploration:

As the lunar trip gets underway, the Departure Vehicle (jettisoned after burn) and Lander group have mated with the Crew Exploration Vehicle (CEV) capsule, as shown here:

The Service module remains unmanned during the days spent on the lunar surface. The lunar landing craft, housing all 4 astronauts (but, eventually, able to support 6 astronauts), as envisioned on the Moon's surface, is displayed here:

The landing units descend to the surface, much like during the Apollo program, with the larger unit consisting of a braking rocket and fuel. After the lunar stay is ended, the upper crew unit fires its rocket to put it into orbit and eventual docking with the service unit.

The schedule calls for the CEV system, without the Lander units, to be ready to fly by or shortly after 2010. It will replace the phased-out Space Shuttle program and will be NASA's means of servicing the International Space Station. This will provide extended experience in CEV use up to the first Moon landings.
Ambitious and exciting as this master plan appears to be, there are many obstacles that could delay or even cancel its execution. The earliest readiness date for a landing is set at 2018. A crew of 4 will descend on the CEV and stay for (at least) a week. Over time, the stay will be longer as the astronauts build a lunar base capable of sustaining the mission for weeks to months. This will provide the needed experience for prolonged missions that would take place on Mars at a later time. When the crew returns to Earth in the detached capsule, it will have the capability of landing either on land or at sea. If no serious damage occurs, the CEV can be used up to 10 flights.

An estimated cost for the first landings is $104 billion dollars. This is likely to be exceeded, since as a rule, such estimates are nearly always low. Additional monies must be appropriated if the undetaking is to happen. Budgetary deficits (exacerbated in 2005 by the Katrina disaster and subsequently by Iraq) can affect the schedule. Some monies will become available for the program after the Space Shuttle program is retired in 2010. But, NASA, and even its critics, together recognize that a Moon exploration resumption followed by Mars exploration (which would gain from the lunar experiences) may be vital to keeping the American space program healthy enough to press forward, rather than wither and diminish by loss of dedicated personnel.
Imaginative futurists being a common breed today, one could predict that no sooner did NASA announce plans for a Moon Base, the Internet would start accruing many "artist's conceptions" of the layout of such an endeavor. Here are two:


Two active websites offer more discussion of such a base: 1) Colonization of the Moon, and 2) Solar Voyager.
19-23: List or mentally note what you think were the principal findings of the Apollo program? ANSWER
The list you created - and that in the answer - certainly does not tell the whole story. Here are some key items that complement the listing:
1. Probably the top achievement, by consensus, is this: that human intellect and commitment combined to make the technical feat of astronauts reaching and landing on the Moon - and RETURNING safely - six times stand out as perhaps the greatest accomplishment of mankind to date.
2. Close behind is the singular success in the face of dire adversity of bringing back the Apollo 13 astronauts to Earth after the near fatal catastrophe that almost doomed them to a dire ending in outer space.
3. The many orbiting and lander missions leading up to Apollo 11 proved the value of unmanned flights designed to gather critical data as part of an overall exploration program.
4. The question of the Moon's origin has been settled by analysis of lunar samples, which disclosed a strong kinship with Earth such that the Moon had to be derived from its terrestrial parent - most likely from a huge impact event (see below).
5. Impact and volcanism, which dominate the lunar surface, are adjudicated to be among the most fundamental of planetary processes.
Another of these top achievements is/are model(s) of the lunar interior. We cite this diagram that is one of the early popular versions (Dr. Anthony Ringwood, of Australia) of the Moon's structure. By now, you should have learned enough to explain the meaning of each major layer in the outer part of the Moon (note: the quartzo-feldspathic layer at the top proxies for the felsitic rocks typified by sample 12013). A similar but more recent model assumes the outer half of the Moon melted - forming the so-called "magma ocean" - early in its history and then underwent differentiation to produce the present general layering: We begin that review of the Moon's history or evolution by showing first a chart that summarizes what was known prior to Apollo: These salient points were determined both from Earth-based telescope observations and from lunar orbiters and landers. The presence of a lunar soil or regolith was confirmed by the Surveyors. The next chart encapsulates the main information on the time-marked evolution of the Moon arrived at from all sources utilizing both Apollo human observations and lunar sample analyses by Principal Investigators and other scientists: The ages cited in the above chart are determined from relative cratering frequencies, calibrated by radiometric dating of the Apollo samples. In this model, a feldspar-rich moonwide crust forms from the magma ocean. Two periods of intense bombardments by asteroids, mini-planets, and comets produce major basins which tossed materials from the highlands crust as first and then also mare surface over most of the lunar surface. These formed eventually consolidated deposits of large to small blocks and fragments making up interleaved "ejecta blankets" from 100s of meters to several kilometers thick. Off-loading and other processes mobilized subsurface rock (largely basaltic [high Fe, Mg, Ca and low Si] in composition) that melted and invaded the surface filling the maria and the interiors of larger craters. Cratering began early in lunar history, reached a maximum around 4 billion years ago, and has tapered off since. This next chart describes the changes and conditions associated with the Moon's outer reaches at the outset of the main period of basaltic lava extrusion: The ideas expressed in these charts can be presented in a different way, as shown in this timeline chart (again, courtesy of H.H. [Jack] Schmitt): This diagram has a deceptively inconspicuous word, "cataclysm", which calls attention to a major defining event in lunar history. First proposed in the early 1970s by Dr. Gerald Wasserburg of Cal Tech, the Lunar Cataclysm (also called the "Late Heavy Bombardment [LHB]), occurred during a hundred million year span centered around a 3.9 billion year age. Wasserburg found that glasses in lunar breccias had prevailing radiometric ages (Argon-40/Argon-39) in that time frame. These glasses are best interpreted as resulting from impact processes. He, and later workers, attributed the impacts that caused large basins such as Imbrium, Serenitatis, and Crisium, together with many of the smaller craters, to swarms of asteroids striking the lunar surface. (Later work on lunar meteorites [found mainly in the ice surfaces of the Antarctic], which represent sampling over the entire lunar terrains, have confirmed this clustering of ages around 3.9 b.y.) The bulk of the asteroids are believed derived from the Asteroid Belt between Mars and Jupiter; these asteroids are postulated to have been perturbed out of their prevailing orbits by a "resonance" process related to Jovian gravitational influence.
The Moon has obviously changed its appearance over time. This set of three paintings depict (left to right) 1) the surface following the major bombardment up to the present, 2) the surface after the Imbrium lavas were emplaced, and 3) the early lunar surface before lavas entered the impact basins. Jack Schmitt has a most interesting Internet site in which he uses various illustrations to show the progressive development of the Moon from its earliest history through the late stages of basaltic emplacement around 3 billion years ago. The site, accessed here, is in .pdf format, which requires Acrobat Reader. His figures on lunar evolution take into account much of the research done in the last 30 years, so it is worth a try to move through this site. To entice you to work through his sequence, we put up here the last (and most complicated) of his model diagrams which has added mare basalt emplacement from a period ending 2 billion years ago. By going through his Lecture 8, you will see the evolutionary steps taken to get to this stage (after which the major changes are associated with small to large impacts). The origin (formation) of the Moon has always been a prime topic for conjecture and scientific insight among selenologists. Four main schemes for lunar origin existed before the Apollo program brought back lunar samples. One view had the Moon form from leftover debris as the Earth itself built up by aggregation. A second idea holds that debris which makes the Moon was tossed off the Earth in the latter's early days when our planet was spinning (rotating) much faster. A third proposal claims the Moon is a captured small planet once more distant from Earth.
The fourth ascribed its formation to material wrenched from the Earth's outer crust by a massive impact leaving the Pacific Ocean Basin as a scar equivalent to a huge crater (a model that would need revision and probable discounting after the ideas of plate tectonics and continental migrations took hold). None of these hypotheses adequately explains the observed balance between the combined angular momenta of the Moon and Earth which theory indicates remains constant since the two bodies became linked. Despite its greater rotation speed in the first few hundred million years of Earth's existence, this still is not enough to foster co-accretion. Nor is the speed sufficient to fission off the debris. But, that spin was too fast to allow capture of a passing body.
By the 1970s, with the Apollo data now in hand, impact had gained favor as an integral part of lunar formation. Several impact models has since been proposed. This diagram neatly summarizes this idea and the key features of subsequent lunar evolution:
All lunar genesis models are constricted by the two Apollo observations that the entire Moon is deficient in iron (Fe can be high in some mare basalts, but is very low in its interior, with no, or a small, iron core) and by the low percentages of the volatile elements sodium and potassium. That the Moon was derived from an impact of giant magnitude on the early Earth is supported by the strong similarity in oxygen isotope compositions in the two planetary bodies. The first model was developed by scientists associated with Harvard University. But, their head-on collision model has since come up with energy and compositional problems. The most recent variation on the general impact model is illustrated by the succession of steps shown in this diagram which is the result of a computer simulation of a huge impact into the protoEarth but oriented at that moment so as to glance against or sideswipe the outer layers of an Earth whose crust had not yet fully developed. Look at this computer simulation of such an event: The model and some variants, collaboratively developed by scientists at the Southwest Research Institute (William Ward and Robin Canup; others) and the University of Arizona (A.G.W. Cameron, Jay Melosh, William Hartmann; others), considers the impact to have occurred late in the formational history of the Earth, but probably prior to the differentiation that formed an early terrestrial crust. At this time, a part, perhaps much, of the outer Earth may have been molten. A Mars-sized asteroid or small planet (about 10% of the present terrestrial mass) struck the Earth at a glancing angle. Although the Earth survived total disruption, much of the outer shell on one side was tossed into space, but held to the Earth by its larger gravity. The fragments in the ejecta plume are affected by rotational forces from Earth and within 24 hours have organized into a near circular orbit. In time these fragments (whose composition mirrors that of the primitive Earth's outer shell(s)) began to collide until the Moon was built up to its present size, large enough for it to have melted and reshaped into a sphere, developing an anorthositic crust. The Earth, still forming, healed its "wound", resumed its organization during subsequent remelting into a near-sphere, and went on to fully differentiate into the crust, mantle, and core that has survived to the present day. The advantages of the swiping impact model are these: 1) a proper relation between Earth-Moon angular momentum comes out of the calculations; 2) the high heat of such an event boils off all water and some of the volatile elements sodium and potassium; 3) the similarity of refractory element composition between Earth and its satellite is explained; 4) only the outer mantle and any early crust are involved; 5) temperatures in a glancing event would have been higher (up to 18000° K); 6) a larger fraction of the Earth target would be ejected into orbit; 7) differences in composition could be due to incorporation of some of the impactor body, which likely varied somewhat from Earth. The resulting Moon may have been much closer to Earth, perhaps as near as 29000 km (18000 miles). This first Moon would have appeared to occupy much more of the sky than today. It is now known that the Moon is receding at a rate of about 2.4 cm/year (around an inch), to its present average distance from Earth's center of 384000 km (240000 miles). Extrapolating back in time for 4.5 billion years yields this early proximity value (which, however, may exceed the Roche Limit - the closest distance two large planetary bodies can be without one at least being disrupted). To close this subsection, there are literally thousands of informative and often exotic images of the Moon, taken by various remote sensors. Perhaps none can better convey the human emotions of having triumphantly landed astronauts on the Moon than this heart-throbbing photo taken by Michael Collins from the CSM of the about-to-dock LM containing Neil Armstrong and Edwin "Buzz" Aldrin, with Mother Earth looking so distant in the background, yet as history shows returned to successfully by these intrepid Apollo 11 explorers and ten others who set foot on the Moon's surface (watched over by five comrades in orbit) in subsequent missions:
Two very readable popular accounts of lunar exploration are The Moon Book by Bevan M. French, 1977, Penquin Books, and Lunar Science: A Post Apollo View by S. Ross Taylor, 1975, Pergamon Press. Reluctantly, we must take leave of our local satellite to begin an impressive
journey through the Solar System. We start with the two innermost planetsMercury
and Venus. 








Primary Author: Nicholas M.
Short, Sr.