Farewell, Messenger

NASA’s Messenger mission is expected to end on April 30th at 3:30 PM EDT with a crash landing on Mercury.   Messenger has run out of fuel and NASA is using this phase of the mission to utilize the spacecraft’s low orbit to obtain very high-resolution images of Mercury’s surface. One of Messenger’s many remarkable discoveries was the confirmation that ice exists in the polar regions of Mercury, the planet closest to the Sun.

Messenger’s voyage to Mercury began on August 3, 2004. The trip to Mercury took almost seven years and Messenger finally achieved orbit on March 18, 2011. Why did the trip take so long? Even though Mercury is only, on average, 48 million miles from Earth, Messenger’s voyage to Mercury was 4.9 billion miles. The trajectory to Mercury involved one flyby of Earth, two flybys of Venus, and finally, three flybys of Mercury itself to insert Messenger into orbit. A video the Messenger’s journey to Mercury is below:

Messenger was the first spacecraft to reach Mercury since Mariner 10 did so in 1975. During this gap, tantalizing evidence emerged that ice might exist on the polar regions of Mercury. The Arecibo Radio Telescope (the same one Jodie Foster used in Contact and James Bond destroyed in Goldeneye) detected strong evidence that ice exists in the shadowed regions of polar craters on Mercury. That made the confirmation of ice deposits on Mercury one of the prime objectives of the Messenger mission. So how does ice exist on the closest planet to the Sun? The answer lies in two facts, the small axial tilt of Mercury and the lack of an atmosphere on Mercury.

The axial tilt of Mercury is 2.11 degrees compared to Earth’s axial tilt of 23.5 degrees. At the poles, this represents the highest angle above the horizon the Sun obtains at the Summer Solstice. The image below is Noon on June 21st at the North Pole on Earth complete with faux landscape courtesy of Starry Night.

North Pole Summer jpeg

Now lets take a look at the North Pole of Mercury when the Sun is at its highest.

Mercury Summer jpeg

Quite a difference, this is the same altitude the Sun has about 15 minuets after sunrise on Earth in the mid-latitudes. Think about how long the shadows are at that time. On Mercury, you have craters as deep as 1 km.  When the Sun stays low in the sky, and craters are that deep, there will be areas in those craters that will never see sunlight.

One might ask, with Mercury being so close to the Sun it must be hot enough to melt ice even if there is no sunlight in the craters. However, Mercury has practically no atmosphere, and with an atmosphere lacking, there is not any wind to transport heat from sunlight areas to dark areas on Mercury. The gravity on Mercury is only 38% that of Earth.   As a consequence, the escape velocity of Mercury is 4.3 km/s compared to Earth’s 11.2 km/s. Here, Mercury’s closeness to the Sun plays a key role. The hotter the temperature, the faster atoms and molecules are accelerated. On Mercury, atmospheric gases are accelerated faster than the escape velocity causing atmospheric loss. On Earth, cooler temperatures and a higher escape velocity enable Earth to retain its atmosphere. Hence, over the course of time, Mercury will lose any atmospheric gases it may have.

Mercury’s surface bears a resemblance to the Moon. The Moon also lacks an atmosphere and is unable to transfer heat from the daylight to the dark side. On Earth, the atmosphere distributes heat across the surface and as a result, there is only an order of difference of a few degrees between day and night. On the Moon, the same distance to the Sun as Earth, the temperature can range from 2500 F on the dayside to -2400 F on the dark side. On Mercury, the difference is more extreme. The range can be from 8000 F on the dayside to -2800 F on the dark side. A region in a crater that is permanently in shadow will never approach the sublimation point (meaning changing from ice to water vapor, the atmospheric pressure on Mercury is too low for liquid water to exist) of ice.

Credit: NASA/UCLA/Johns Hopkins University Applied Physics Laboratory/Carnegie Institution of Washington

Messenger’s detection of ice on Mercury is a classic case of matching a predicted result with observation. Messenger used a neutron spectrometer to measure the amount of neutrons emitted from the surface of Mercury. These neutrons are radiated as a result of high-energy cosmic rays striking the surface and ejecting them into space. Areas with ice absorb these neutrons, leading to a lower count in those regions. Scientists built a model predicting the neutron count, matched it up with observation, and voila, as the video below illustrates, a match was found.

This is a map of Mercury’s North Pole released by the Messenger mission in 2012.  The red regions are shadowed regions and the yellow indicate areas of ice.

Credits: NASA/Johns Hopkins University Applied Physics Laboratory/Carnegie Institution of Washington/National Astronomy and Ionosphere Center, Arecibo Observatory

In 2014, Messenger obtained visual confirmation of the existence of ice in the Kandinsky crater located near the North Pole of Mercury.  The image was taken by Messenger’s wide angle camera (WAC) with a 600 nanometer (orange) broadband filter.  Normally, this camera’s function was to image stars for calibration purposes, but it had the capability to capture ice in the craters of Mercury lying beneath the shadows using scattered sunlight. This capped off a 25 year hunt for proof of existence of ice on the closest planet to the Sun.

This image compares a view of the crater without the filter (left) and with the filter (right) that can detect detail in the dark recesses of the crater.

Credit: NASA/Johns Hopkins University Applied Physics Laboratory/Carnegie Institution of Washington

Even though Messenger is in its final days, it is still productive. As its orbit decays and the spacecraft gets closer and closer to the surface, this will enable Messenger to take some of the highest resolution images ever of a planetary surface. Messenger was selected by NASA for its mission in 1999. The total cost over those 16 years has been about $450 million. That is about the same as it cost to launch one shuttle mission. Or on more Earthly terms, the same amount Texas A&M will spend to renovate its football stadium.  Messenger has sent back over 10 terabytes (or 10,000 gigabytes) of data and over 200,000 images that will keep planetary scientists busy for years to come.  At least until 2024, when ESA’s BepiColumbo mission will reach Mercury.

Corning, Kodak, and Hubble

This being the 25th anniversary of the launch of the Hubble Space Telescope, it is an opportune time to take a look at the connections between Upstate New York and the Hubble. I will focus on two companies. Corning, whose technological innovations made the Hubble possible, and Kodak, whose efforts could have spared the NASA the grief of Hubble’s original design flaw.  The story begins in the 1930’s, as the proposed 200-inch Mt. Palomar Observatory mirror required a low expansion material to make the large mirror possible.

During the 1920’s, the largest telescope in the world was the 100-inch reflector at Mt. Wilson Observatory. It was in this decade that Edwin Hubble would make his historic observations at Mt. Wilson, which included the discovery of galaxies outside the Milky Way and the expansion of the universe. At the time, George Ellery Hale was in the planning stages of building the 200-inch telescope at Mt. Palomar. To understand the engineering problem at hand, the surface area of the Mt. Wilson mirror is:

A = πr2

Which is (3.14)(502 inches) = 7850 square inches or 54.5 square feet.

The surface size of the Mt. Palomar mirror would be:

(3.14)(1002 inches) = 31,400 square inches or 218 square feet.

Despite the fact the diameter of the mirror at Palomar would be only double that at Mt. Wilson, the surface area would be 4 times larger. The mirror at Mt. Wilson was made at the French Glass Works and weighed 9,000 pounds (the mirror at Mt. Wilson is green just like a wine bottle). The greater surface area of the Mt. Palomar mirror demanded a material that did not expand or contract as much to temperature changes. Unless an alternative material could be found, this expansion and contraction would distort the optics to the point of making the primary mirror useless.

Enter Pyrex

The invention of Pyrex at the Corning Glass Works was the result of an effort to make lantern glass suitable for railroad watchmen. Traditional glass lanterns would shatter when the heat of the flame combined with cold winter weather. By 1915, Pyrex was being produced for its most well known application-kitchenware. The low heat expansion quality of Pyrex made it an excellent material for cooking.

Image: Wiki Commons.

In 1932, George Hale was looking for a material to cast the 200-inch Palomar mirror. His first choice was fused quartz, but the efforts at General Electric to cast the mirror this way proved unsuccessful. After spending $600,000 ($10 million in 2015 dollars) on the failed quartz effort, Hale turned to the Corning Glass Works and its Pyrex product to give it a try for the Palomar mirror.

Besides kitchenware, you may be familiar with Pyrex from your high school chemistry lab. Pyrex is regular glass with borax oxide added to it. The combination produces borosilicate glass, which experiences low expansion when exposed to heat. This is what keeps Pyrex kitchenware and lab equipment from breaking when it is heated up rapidly. So, why is this important for a telescope mirror that does not experience the same type of heating when Pyrex is put in an oven or over a Bunsen burner?

The optical precision required for the Palomar mirror meant that the mirror could not deviate more than two-millionths of an inch from its prescribed shape. Needless to say, the slightest amount of thermal expansion would have grievous effects on the optical quality of the images produced by the mirror. With this in mind, the Corning went to work on producing the Palomar mirror blank with its Pyrex material.

It would take two tries for Corning to build the mirror to be used at Palomar. During the first attempt, pieces of the mold in the mirror broke off due to the heat used in the casting process. This flawed mirror is now on display at the Corning Museum of Glass (see video below). The second mirror was shipped via a highly publicized train ride cross-country to California in 1936. There, over 10,000 pounds of the glass was shaved off in an extensive grinding process to polish the mirror to its required shape to produce the high-quality images for the telescope. World War II delayed this work a few years, but eventually the mirror was installed in the telescope in 1948.

Mt. Palomar would remain the world’s largest telescope until 1993 when the Keck Observatory in Hawaii surpassed it. During its run as the world’s largest telescope, astronomers at Palomar would refine the measurement of the expansion of the universe and discover quasars among its many other discoveries.  At the same time, Corning’s experience with producing observatory mirror blanks would be called upon again to make another groundbreaking instrument of astronomy.

In 1946, Lyman Spitzer proposed an observatory be placed in orbit above the distorting effects of the Earth’s atmosphere. In 1962, at the dawn of the space age, the National Academy of Sciences recommended that Spitzer’s concept be adopted by NASA as a long-term goal of the space agency. In 1977, Congress approved funding for an orbiting space telescope. In 1978, Corning went to work to produce two mirror blanks for the Hubble.

The Hubble mirrors were not made from Pyrex. By the 1970’s, Corning developed Ultra Low Expansion (ULE) fused titanium glass. Rather than use borax oxide as Pyrex does, ULE is made with a blend of titanium and silica to give it a nearly zero expansion coefficient. Besides being used for telescope mirrors, ULE was also utilized for space shuttle windows, as it could resist expansion when frictional heat built up during re-entry into Earth’s atmosphere.  This ability to maintain its shape made ULE an excellent candidate for the space telescope mirror.

Even though the Hubble mirror is kept at constant 700 F, the mirror shape only deviates 1/800,000 of an inch. If the Hubble mirror were the diameter of the Earth, its highest “mountain” would only be six inches. The nearly expansionless ULE maintains this optical precision.  ULE is also very lightweight.  Despite being the same size as the 100-inch Mt. Wilson mirror, the Hubble mirror is only 20% the weight.

After the production of the two mirror blanks, one was shipped to the Perkin-Elmer Corporation, the other to Kodak-Eastman for polishing. The blank sent to Perkin-Elmer eventually was used for the Hubble.  It was at this stage the fateful flaw would be made in the Hubble mirror.

A Kodak Moment NASA Regrets Passing Up

NASA received two bids to polish the mirror blanks from Corning. The Kodak bid was for $105 million while Perkin-Elmer bid was for $70 million ($300 million and $200 million in 2015 dollars respectively). Naturally, the Perkin-Elmer bid was viewed as the most competitive but it contained some troubling aspects. The Kodak bid was to polish two mirrors with different testing techniques. The testing mechanism on each mirror would then be used on the other to determine which was the better mirror and as a quality control measure. Perkin-Elmer relied on a single method to polish the mirror. It then sub-contracted Kodak to polish the back-up mirror, albeit at NASA’s request.

Further complicating matters (wonderfully described in Robert Capers and Eric Lipton’s report) was the budgetary and time constraints the Perkin-Elmer employees were working under. Perkin-Elmer had deliberately low-balled their bid to win the contract with the expectation Congress would approve more funding as the project progressed. However, the early 1980’s experienced the greatest recession since World War II as unemployment climbed towards 10% and Congress was in no mood to allocate more funding to polish the mirror.

washers
Wiki Commons

In the proverbial cruel twist of fate, the famous flaw in the Hubble mirror was a result of the use of three washers (yes, the very same kind used in your kitchen faucet) by Perkin-Elmer technicians to shim the optical testing device referred to as a null corrector. A piece of worn paint caused a misalignment of a laser that calibrated the distance from the null corrector to the mirror.  The overworked and rushed Perkin-Elmer technicians failed to report the calibration error to meet the deadline to produce the mirror.  This was combined with overconfidence in the null corrector device as signs of a design flaw in the mirror were ignored by the Perkin-Elmer project management. In the end, the mirror was polished perfectly to the wrong prescription, as the null corrector was 1.3 mm closer to the mirror than it should have been. The flaw in the mirror itself was 2 micrometers or about 1/50th the width of a piece of paper.

Consequently, the $1.5 billion Hubble was launched into orbit 25 years ago today with spherical aberration in its mirror causing blurry images due to three washers worth about twenty cents.

And what happened to the Kodak mirror? It stayed here on Earth. Kodak was not able to use its cross testing method as it only made one mirror rather than two. However, Kodak had used more traditional, time-tested methods to grind its mirror and finished its work in 1980, well before the Perkin-Elmer mirror. When the Hubble mirror flaw was discovered shortly after launch, the Kodak mirror played a key role in the ensuing investigation. The final determination was that the Kodak mirror was ground to the right specifications and the corrective measures would not have been required had it been placed in the Hubble. Since Kodak was subcontracted by Perkin-Elmer, it was the latter who had the final say which mirror to use and quite naturally, Perkin-Elmer decided to use its own mirror. The flaw was corrected in 1993 by the STS-61 mission.  The shuttle mission replaced the original Wide Field and Planetary Camera (WFPC1) with another* (WFPC2) that contained optics to counteract the spherical aberration in the Hubble mirror images.  The difference before and after are below:

M100 before and after Hubble repair mission. Credit: NASA

For the other instruments on the Hubble, the Corrective Optics Space Telescope Axial Replacement (COSTAR) was installed.  This was a set of mirrors used to act as “glasses” to correct the spherical aberration for the Faint Object Camera & Spectrograph, along with the High Resolution Spectrograph.

The Kodak mirror (below) now resides at the Smithsonian Air & Space Museum.

Courtesy National Air and Space Museum

* Both the WFPC2 and COSTAR that corrected the mirror flaw in the Hubble were removed in 2009 by the final Hubble shuttle servicing mission. The WFPC2 and COSTAR were also donated to the Smithsonian Air and Space Museum.

Image on top of post is the Hubble mirror.  Photo:  NASA/ESA

Regional Astronomy Events This Week

A couple of intriguing astronomy events in New York state this week.

Thursday, April 16 – Professor Lynne Hillenbrand discusses young stars across the electromagnetic spectrum at the Cornell Astronomy Colloquia from 4-5 PM at the Space Sciences Building starting at 4 PM.

April 18th & 19th – The Northeast Astronomy Forum at Rockland Community College in Suffern, NY.

Apollo 11

Each semester during the Earth & Moon segment of my astronomy course, I like to show this video for the class of the Apollo 11 liftoff. It gives the students, most too young to have witnessed this, an opportunity to see how the event was covered at the time. Also, it ties in well with the concepts learned in the prior module involving Newton’s Laws of Force. Many of the concepts apply to launches today and this is a good opportunity to break down NASA jargon into comprehensible English.

Working the broadcast that day for CBS was Walter Cronkite and Wally Schirra, who was an astronaut on three space missions including Apollo 7.  The description of the video is as follows with the time being for the video rather than launch itself.

0:12 These are the 5 stage one F-1 engines each capable of producing 1.5 million pounds of thrust for a total of 7.5 million pounds of thrust. The Saturn V weight was 5 million pounds at launch. Newton’s third law states for every action, there is an equal and opposite reaction. The excess 2.5 million pounds of thrust is what lifted the Saturn V at launch. The engines were produced by Rocketdyne (dyne is Greek for power) which is now part of GenCorp Inc.  Now known as Aerojet Rocketdyne, the company has had some difficult times recently. The center engine is referred to as the inboard engine and the four outer engines as the outboard engines. The outer four gimbal and guide the rocket.

0:21 The voice you hear is Jack King, then the Kennedy Space Center Chief of Public Information.  King passed away in June of 2015.

0:30 The steam you see from the Saturn V is boil off from the cryogenically cooled liquid hydrogen and oxygen.  Hydrogen boils at – 4230 F.  That is only 360 F warmer than absolute zero.  Oxygen boils at -2970 F.  Venting the boiling liquid hydrogen and oxygen prevents the fuel tanks from being deformed.  The black markings on the Saturn V are quarter marks and are used to study the roll of the rocket during launch.

0:43 The fuel tanks are continually pressurized until right before launch as discussed above, liquid hydrogen and oxygen boil at very low temperatures and the boiled off fuel needs to be replenished.

1:53 Walter Cronkite mentions the water deluge on the launch pad. This system could release 45,000 gallons per minute as a sound suppression device to avoid acoustical damage to the Saturn V.  A nuclear weapon is the only human made device louder than a Saturn V.

2:21 Ignition of the F-1 engines starts 8.9 seconds before launch. This is the amount of time it takes to build up the required thrust for lift-off.

2:32 Lift-off! The Saturn V is angled 1.25 degrees away from the launch pad to avoid contact.  Close up videos of the launch (below) will reveal large chucks of ice vibrating off the rocket.  The Saturn V would have 1,200 pounds of ice on its sides created by the very cold liquid hydrogen and oxygen in the fuel tanks.

2:41 Jack King announces the tower is cleared. At this point, control of the flight is transferred from the Kennedy Space Center in Florida to the Johnson Space Center in Houston.

2:43 Neil Armstrong announces the beginning of the roll and pitch program to send the Saturn V over the Atlantic. This is the same direction the Earth rotates.  At the Cape, the Earth rotates at 914 mph (1471 km/hr).  That is the amount of velocity boost Apollo 11 receives from Earth’s rotation to help attain orbit and that is why all launches are eastward.  The closer to the equator, the faster the Earth’s rotational movement is. Launch facilities located near the equator such as ESA’s Guiana Space Center have a competitive advantage of being able to life more payload per amount of thrust.

2:48 Walter Cronkite mentions the building is shaking, a common occurrence during Apollo launches.  The press was stationed three miles from the launch pad. One (of many) reason the recent movie Apollo 18 was not realistic, lift-off would have set the entire Cape shaking. It would not be possible to launch a Saturn V there in secret.

3:31 As Apollo 11 approaches the speed of sound, the pressure differences from the shock waves lift water vapor away from the vehicle.

4:06 The region of maximum dynamic pressure, or Max Q, is when the combination of velocity and air pressure is greatest on the Saturn V. Although the velocity will continue to increase, the atmospheric density begins to drop off rapidly after this point. This can be seen by the widening thrust field from the rocket due to the rapid decline in atmospheric pressure.

5:12 Staging, the first stage is released and dropped into the Atlantic Ocean and the second stage ignites.  Apollo 11 is now in the stratosphere at an altitude of 42 miles.

5:16 The second stage has 5 J-2 engines. Like the F-1, these are also made by Rocketdyne. At this point in the flight, thrust is less important as the rocket is lighter and burn time takes precedent. The thrust of the J-2 is 230,000 pounds each but the burn time is about 7 minutes.

5:43 Skirt sep refers to the skirt between the first and second stage being separated.

5:58 Mike Collins reports visual is a go. He is referring to the command module launch shield being removed along with the escape vehicle. At this point, the astronauts now have a view out the window.

7:50 Here, many of my younger students express shock at the animation used in the coverage. A common device during the early years of the Space Age as there was not the miniaturization of cameras as there is today which allowed for on-board cameras famously seen on the shuttle launches.

8:45 Fitted between the third stage and the service module was the IBM computer for Saturn V. The computer ring was 3 feet high, 22 feet in diameter, and had 32 kb of memory-about half the size of a blank Word page.

IBM Saturn V Computer Ring – Courtesy: NASA

9:20 The water deluge on launch pad 39 to mitigate damage from the lift-off burn. After the Apollo program was complete, this launch pad was converted for use during the Shuttle program.  Today, launch pad 39 is leased out to SpaceX for its future space operations.

10:38 This was a very troubled time for American passenger railroads as alluded to by Walter Cronkite. Penn Central would file for bankruptcy less than a year later prompting Congress to form Amtrak in 1971.

Two hours and fifty minutes after launch, Apollo 11 began trans-lunar injection and was on its way to the Moon.

*Top image launch of Apollo 11, July 16, 1969.  Photo:  NASA.

Magnetic Reconnection, Part Deux

From the feedback I got from my last post I wanted to clarify a few things, mostly the Interplanetary Magnetic Field generated by the Sun. But first, the x,y,z axis scheme. Below is an image of a three dimensional axis:

The orbits of the planets reside in the x-y plane along with the Sun itself.  In astronomy, this is known as the plane of ecliptic. As the solar wind spreads out through the Solar System, it takes the IMF field lines with it. Because the Sun rotates just like the Earth, the solar wind, and thus, the IMF looks like the pattern you see from a water sprinkler when looking down on it towards x-y plane.

imf_big
Courtesy: NASA

However, the IMF is not flat along the x-y plane.  In addition to the sprinkler type formation seen above, it also has a wavy type feature as well.  This is represented in the image below:

Courtesy: NASA

The z-axis is up and down.  When the IMF slopes upward, it is said to have a positive Bz value as B is used in physics to represent a magnetic field.  The Earth’s magnetic field flows from the geographical South to North Pole and also has a positive Bz value.  When two magnetic fields are flowing in the same direction the probability of reconnection is low.  When the IMF is sloping downwards, it has a negative Bz value.  In this case, the probability of reconnection is high which brings along with it a high chance of auroral activity and magnetic storms.  This is why if you visit a space weather website to check out possible aurora, you’ll want to be on the lookout for a negative Bz value.