Shuttle/Shuttle Concept Restart: Fwd: 15 Years Since STS-99

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From: "Gary Johnson" <gjohnson144@comcast.net>
Date: February 16, 2015 at 11:12:57 AM CST
To: "Gary Johnson" <gjohnson144@comcast.net>
Subject: FW: 15 Years Since STS-99

AmericaSpace
For a nation that explores
February 14th, 2015
Mapping Planet Earth: 15 Years Since STS-99 (Part 1)
By Ben Evans

Computer-generated image of Endeavour performing radar observations with instruments in her payload bay and affixed to the deployable Outboard Antenna on STS-99. Image Credit: NASA
At the dawn of the year 2000, more precise radar maps existed of Venus—thanks to NASA's Magellan imaging spacecraft—than of our own Home Planet. Although areas of Earth had been digitally mapped at resolutions of 100 feet (30 meters), the vast majority of the world lacked such reliable data, primarily due to cloud cover in equatorial regions, which precluded imaging by optical satellites or aircraft. "Humans always want to know about their environment," said German astronaut Gerhard Thiele, "and for the first time we will generate a coherent data set; a picture of the Earth." Fifteen years ago, this week, Thiele and his five STS-99 crewmates launched aboard Endeavour on the ambitious $220 million Shuttle Radar Topography Mission (SRTM), tasked with utilizing an innovative technique to assemble the most comprehensive maps of our world to date. Although it has since been enhanced by more modern technologies, SRTM had generated 750,000 confirmed users of its data sets by mid-2011 and its resources have been accessed by people in 221 countries.
Right from the start, SRTM was an affair which transcended nations. Spearheaded by NASA and the Department of Defense's National Imaging and Mapping Agency (NIMA), and supported by the German and Italian space agencies, it would operate from a high-inclination orbit of 57 degrees and employ hardware which had previously seen use on the first and second Space Radar Laboratory (SRL) missions in April and September 1994. The six-member crew—Commander Kevin Kregel, Pilot Dom Gorie, and Mission Specialists Thiele, Janet Kavandi, Janice Voss, and Japan's Mamoru Mohri—were assigned to STS-99 in October 1998, with an original target launch date in mid-September of the following year. "During the mission, the crew will use specialized radar equipment and other electronics to map 80 percent of the Earth's land mass, extending from the southern tip of Greenland to the northern edge of the Antarctic Circle," NASA revealed, with a swath from 60 degrees North to 56 degrees South latitude. "Data targets will be spaced approximately every 90 feet (27.4 meters) and the resulting image should be accurate to within 30 feet (9 meters) of the height of the terrain."
During their 11 days in space, the crew would perform in excess of 1,000 "data-takes," operating in two 12-hour shifts, using 29,980 pounds (13,600 kg) of radar instruments both inside and outside Endeavour's cavernous payload bay. The two main SRTM instruments, affixed to a Spacelab pallet, were NASA's third-generation Shuttle Imaging Radar (SIR-C) and the joint German/Italian X-band Synthetic Aperture Radar (X-SAR), both of which flew on the two SRL missions. These instruments would transmit microwaves at C- and X-band wavelengths toward the surface and gather the reflected echoes on two separate receivers. SIR-C offered multi-frequency, multi-polarization imagery and represented the first space-borne radar with the ability to transmit and receive horizontally and vertically polarized waves at both the L- and C-band wavelengths.
STS-99 Commander Kevin Kregel (left) and Pilot Dom Gorie are pictured during training in May 1999. Photo Credit: NASA
Measuring 39 feet (12 meters) long and 13 feet (4 meters) wide, SIR-C was the most massive piece of flight hardware ever built at the Jet Propulsion Laboratory (JPL) in Pasadena, Calif. It was a Synthetic Aperture Radar (SAR) and filled almost half of Endeavour's payload bay for STS-99. Originally assembled from spares left over from NASA's 1978 Seasat mission, SIR-C was affixed to its own truss support structure, which, in turn, was mounted onto a Spacelab pallet, providing a "side-looking" viewing angle, some 47 degrees from the nadir. As a result, during data-gathering operations, the shuttle was required to reorient itself to precisely direct SIR-C at its ground targets. Its radar beam was formed from hundreds of transmitters, embedded within the surface of the antenna. By properly adjusting the energy from these transmitted, the beam could be electronically "steered" and, when combined with shuttle maneuvers, offered the scope to acquire images from various directions. However, SIR-C was not the only radar in the payload bay for SRTM. Running like a strip along the uppermost edge of SIR-C was "X-SAR," a 39-foot (12-meter) x 1.3-foot (40 cm) synthetic-aperture device, built by a partnership of organizations, including the German Dornier and Italian Alenia Spazio companies, together with the German and Italian space agencies, which offered a single-polarization radar, operating in the X-band. It was designed to be mechanically aligned with the L-band and C-band beams of SIR-C.
With the SIR-C/X-SAR combo serving as one of SRTM's two receivers (dubbed the "Main Antenna"), the second receiver (known as the "Outboard Antenna") was mounted at the end of a 200-foot-long (60-meter) mast, which extended "sideways" into space over the shuttle's payload bay wall. Radar "echoes" from the instruments were captured, amplified, and their data recorded on digital tapes for post-flight analysis. It was also expected to be possible to downlink data from one of the radar frequencies in real time to ground-based researchers, through NASA's Tracking and Data Relay Satellite (TDRS) constellation.
Interferometry as a radar-mapping technique was not entirely new ground for the shuttle, since it was first demonstrated at the end of the SRL-2 mission. However, since that mission only carried the SIR-C/X-SAR payload and was not equipped with a mast-mounted outboard antenna, the SRL-2 crew had to fly over the same patch of ground track and acquire two radar images over separate orbital passes. In effect, it was only possible to achieve "multiple-pass interferometry," rather than acquiring the data in a single orbital pass. Moreover, the shuttle's altitude and the relative instability of its attitude meant that it could only collect useful interferometry data with the L-band capability of SIR-C. Nevertheless, the seed of an idea was planted for a fixed-baseline, single-pass interferometer, and on 8 July 1996 a formal Memorandum of Understanding (MOU) between NASA and the Department of Defense to develop SRTM had crystallized into a proposal for a future shuttle payload.
Emblazoned with the surnames of six astronauts from three sovereign nations, the STS-99 crew patch highlights the radar-mapping focus of the mission. Image Credit: NASA
The payload carried the elements of the first fully-equipped, single-pass interferometer ever carried aboard the shuttle, capable of taking two simultaneous images of Earth from slightly different locations and at different frequencies, to be combined into high-resolution, three-dimensional topographical maps for a wide range of civilian, military, and scientific purposes. The presence of the outboard antenna on SRTM allowed this interferometric data to be gathered with greater efficiency at C- and X-band frequencies. Since it would be possible to acquire both images in the same orbital pass, the potential data return was expected to be significantly higher. In the words of STS-99 Commander Kevin Kregel, operating two antennas in this manner, was akin to acquiring two radar images, 200 feet (60 meters) apart, "and that gives us the capability to get the 3D image."
The outboard antenna and its 200-foot (60-meter) mast were to be deployed from a 9.5-foot (2.9-meter) canister, which was also mounted onto the Spacelab pallet, next to the main antenna, and would represent the real novelty of SRTM. Its design was based upon the same technology used for the truss members destined for the International Space Station (ISS), and it was fabricated by AEC-ABLE Engineering of Goleta, Calif., which also built a mast to support the Tethered Satellite System (TSS) on two earlier shuttle missions in July 1992 and February 1996. It consisted of carbon-fiber-reinforced plastic, stainless steel, alpha titanium, and an iron-nickel alloy, known as "Invar." Officially designated the "ABLE Deployable Articulated Mast" (ADAM), when fully extended the 640-pound (290-kg) device represented the longest rigid structure ever deployed from the shuttle.
During its launch and re-entry phases, the mast was folded up in a manner not dissimilar to a giant accordion in its canister. Once described by Gerhard Thiele as nothing short of a "miracle," the mast was deployed in space by means of a rotating nut, which grasped the edges and corners and pushed them outward into a succession of 87 almost-perfect "cubes." It was designed to deploy successfully without twisting, which allowed it to house electrical wiring, fiber-optic cables, and gas thruster lines along its entire length to connect the outboard antenna with the instruments in the payload bay. AEC-ABLE also guaranteed that the mast would remain stable to within 0.8 inches (2 cm) of total tip displacement, which was considered essential if the radar-mapping standards demanded of SRTM were to be met. At the mast's tip was the outboard antenna itself, which had been assembled from spares left over from the two SRL missions, and included C-band and X-band passive receiver panels to collect radar echoes from the SIR-C/X-SAR transmissions.
In spite of the exciting nature of its scientific potential, STS-99 was a long time coming. When its six-strong crew were announced by NASA in October 1998, they confidently anticipated launching in September of the following year, on an 11-day flight. By the middle of July 1999, the SRTM hardware had been loaded into Endeavour's payload bay in the Orbiter Processing Facility (OPF) at the Kennedy Space Center (KSC), ready for the rollover to the Vehicle Assembly Building (VAB) in August for stacking onto her External Tank (ET) and Solid Rocket Boosters (SRBs). Unfortunately, STS-99 and several other shuttle missions met with significant delay in the summer and winter of 1999, following extensive wiring defects which impacted the entire fleet of orbiters. In order to inspect Endeavour's wiring, the SRTM hardware had to be removed from the payload bay, and the STS-99 launch was postponed until at least early October. A bent freon line on SRTM, later repaired with a brace, added to the problems, but by early December the wiring inspections were completed, and on the 13th the shuttle stack was rolled out to Pad 39A, tracking an opening launch attempt in mid-January 2000.
Had the mast for the Outboard Antenna failed to deploy or fold correctly, Janet Kavandi would have led a contingency EVA to manually drive it. Photo Credit: NASA
This date soon became untenable, following lengthy delays to the previous shuttle mission, STS-103, which eventually flew over Christmas 1999. A new launch target of 31 January was established and countdown operations ran smoothly, and the crew suited up and were strapped into their seats aboard Endeavour. Unfortunately, they were thwarted by doubtful weather conditions, including low clouds and rain at KSC, and by a potential problem with an on-board Master Events Controller (MEC). The latter was housed in avionics boxes within the shuttle's main engine compartment, and the countdown clock was held at the T-20-minute mark, then scrubbed for 24 hours when engineers could not replicate the exact cause of the problem. At length, the Mission Management Team (MMT) opted to play it safe and replace the MEC. Although removal and replacement was fairly straightforward, the function of the MEC was entwined with a number of pyrotechnic operations, which firstly required the safing of pyrotechnics, then the removal and replacement procedure itself, and then the reinstallation and reactivation of the pyrotechnics.
This pushed back the STS-99 launch until no earlier than 9 February. This was also moved 48 hours to the right, due to the countdown demonstration test on the 10th of a Titan IV booster at nearby Cape Canaveral Air Force Station, which required Eastern Range tracking support. Eventually, on the 11th, despite minor technical issues associated with cabin leak checks, a hydraulic recirculation pump, and a liquid hydrogen manifold tank heater, Endeavour passed smoothly through the final stages of the countdown and rocketed into orbit at 12:43 p.m. EST.
Within hours of entering space, the crew divided into its two teams, with the "blue shift" of Gorie, Voss, and Mohri setting up a network of laptop computers, then heading to bed for an abbreviated, six-hour sleep period. Meanwhile, the "red shift" of Kregel, Kavandi, and Thiele began activating the activation of the SRTM payload, its instruments, and deploying its outboard antenna. Since both Kavandi (EV1) and Thiele (EV2) had been specifically trained to perform a contingency spacewalk to manually unfurl or retrieve the mast in the event of problems, it made sense for Kregel to assign them to the same shift, as well as to the shift which began the deployment process.
Had problems arisen with the mast during this critical phase, Kavandi and Thiele would have embarked on an EVA to decouple its motors and manually drive it open or closed with a power wrench. The trio initiated the extension of the mast at 6:27 p.m. EST, and all 87 cube-shaped bays had been successfully deployed from their canister within 17 minutes, reaching a maximum length of 200 feet (60 metres) from Endeavour's port side. The astronauts maneuvered Endeavour into the correct mapping attitude, with the orbiter's tail facing into the direction of travel, and under Kregel's direction executed a series of thruster firings to test the ability of dampers to absorb the force of maneuvers and keep both the main and outboard antennas correctly aligned with their targets. By the time Kregel, Kavandi, and Thiele retired to sleep at about 10:45 p.m. EST, about 10 hours after launch, they had triumphantly executed STS-99's most complex task. The radar mission was underway.

Copyright © 2015 AmericaSpace - All Rights Reserved

AmericaSpace
For a nation that explores
February 15th, 2015
Mapping Planet Earth: 15 Years Since STS-99 (Part 2)
By Ben Evans

The Outboard Antenna of the Shuttle Radar Topography Mission (SRTM) extends 200 feet (60 meters) into space atop a mast extended from Endeavour's payload bay. Photo Credit: NASA
Fifteen years ago, this week, the six-member crew of STS-99—Commander Kevin Kregel, Pilot Dom Gorie, and Mission Specialists Janet Kavandi, Janice Voss, Germany's Gerhard Thiele, and Japan's Mamoru Mohri—embarked on the $220 million Shuttle Radar Topography Mission (SRTM) to assemble the most comprehensive maps of Earth to date. As described in yesterday's AmericaSpace history article, SRTM utilized radar "interferometry," with a pair of antennas positioned 200 feet (60 meters) apart, one in the payload bay and the other at the end of a deployable mast, and its successful deployment on the first day of the 11-day mission gave Thiele cause for great relief. In time, SRTM would generate 750,000 confirmed users of its data by mid-2011, and its resources have been accessed by people in no less than 221 discrete countries.
With the STS-99 crew split into two 12-hour shifts—"red" and "blue"—it was the responsibility of the red team, consisting of Kregel, Kavandi, and Thiele, to oversee the actual deployment of the mast. "Everything has to go like clockwork and the red shift will deploy the mast, calibrate the radar, verify that both antennas … look at the same point on Earth," Thiele explained before the flight. "We will calibrate it with the help of the ground, of course, and then at the end of our shift, the mission will be rolling." If the mast-based Outboard Antenna did not deploy correctly, the mission would be significantly impaired; "not so much that we could not live with a shorter [radar] baseline," admitted Thiele, "but the key thing here is safety." The mast needed to be firmly locked in place in order to compensate for shuttle motions, and it could not be firmly locked into place if it was improperly deployed. The criticality of the work to be done by Thiele and his red shift crewmates in the first few hours after Shuttle Endeavour reached space was acute.
However, it soon became evident that the mast's damping system, which acted as a shock absorber, was not behaving as expected. Mission Control opted to leave the dampers in their "locked" position, since calculations indicated that the mast was at no risk in this configuration and it would not pose any threat in terms of science capability. By the morning of 12 February, less than 18 hours into the STS-99 mission, the SRTM radars had begun their first "swath" over southern Asia and by the end of their first full day in orbit had mapped a total of 1.7 million square miles (4.5 million square km), which was roughly equivalent to an area half the size of the contiguous United States. X-band imagery of White Sands, N.M., was met with delight from investigators at its level of detail and quality.
The multi-national crew of STS-99 included Japan's Mamoru Mohri (seated left) and Germany's Gerhard Thiele (seated right). Standing (from left) are Janice Voss, Kevin Kregel, Dom Gorie, and Janet Kavandi. Photo Credit: NASA
The breadth of their radar mapping covered all of Earth's southern areas, save Antarctica, and all northern areas to the south of the southern tip of Greenland, southern Alaska, and central Russia. During his second shift, Kregel performed a series of thruster pules to measure the movement of the mast and noted that the tip moved, as predicted, by a matter of less than 11 inches (28 cm). Later, on 13 February, the crew also performed their first so-called "flycast maneuver," which was designed to reduce strain on the mast and maintain the most optimum conditions for radar mapping. It was named in honour of the casting technique adopted by a fly fisherman and sought to limit the loads on the mast during frequent shuttle attitude-control maneuvers.
"Once a day, because we're at a fairly low altitude, we have to adjust our orbital altitude," explained Dom Gorie before launch. "We do that with a couple of reaction control jets in the aft end of the shuttle. If we were to do that without thinking of the ramifications on the mast, we would pulse on the back end of the orbiter with the reaction control jets and the mast would deflect backwards, because of its mass and inertia. Once we stop the burn, if we let it go, the mast would swing back and forth. What we have designed is a maneuver that will minimize the deflections on the mast and minimize the loads at the tip. If we did this without the flycast maneuver, we would have a 3-foot (90-cm) deflection at the mast tip and we would approach the mast limit loads at the base. So we pulse for just a short time, one-sixth of the natural frequency of the mast, and the mast will deflect 'back' slightly. Right when it starts springing backwards, we will pulse again and, in essence, 'catch' it in its deflected state. We are then burning the reaction control jets for the duration of the burn that it takes to adjust our altitude. When we stop the burn, the mast wants to start swinging back, and, if left alone, it would start flycasting again; it would start twanging back and forth, just like that fly fisherman's rod. As it reaches back to its neutral position, we do one more pulse at one-sixth the frequency of the mast for that duration and catch it in its neutral position. That way we take those 3 feet (90 cm) of deflection that we would expect without a flycast maneuver and we halve it to 1.5 feet (45 cm) and the mast loads at the tip are halved as well. What we've done is designed a maneuver that achieves our end parameters, but greatly reduces the risk of damage to the mast."
During each of the flycast maneuvers performed during the mission, Endeavour was oriented into a nose-first attitude, with the mast extending away into space, after which the Reaction Control System (RCS) thrusters were pulsed to deflect the mast backwards and then rebound it forward. When it reached "vertical," a stronger thruster was applied to arrest its motion and increase the orbiter's velocity, thereby keeping Endeavour in the most optimum altitude for radar mapping.
The mast, bearing the Outboard Antenna, extends over the port-side wall of Endeavour's payload bay. Photo Credit: NASA
Overall, SRTM operations ran with exceptional smoothness, with flight controllers' attention drawn only to a minor propellant consumption issue associated with the nitrogen gas thruster at the end of the mast. The thruster was designed to keep the mast from "righting" itself in response to Earth's gravity and thereby remove the need for additional thruster firings to keep the antenna in its data-collection position. Although propellant was flowing to the thruster, it appeared that little or no thrust was being produced, in spite of the crew periodically cycling its valve open and closed. In the meantime, Kregel and Gorie were required to use orbiter firings to maintain the fine position, which increased propellant expenditure by about 0.07 to 0.15 percent per hour.
However, efforts to conserve propellant were explored over the following days, including a relaxation of the requirement to maintain the mast's attitude, which was already showing its stability to be far better than predicted. Other measures included changing the manner in which waste water was dumped overboard and limiting the use of non-critical equipment. On the 17th, Gorie cycled the nitrogen line and Voss reported seeing the dislocation of a small, white object, which was presumably a small piece of ice and flight controllers subsequently noticed that the thruster began to generate some thrust. Later that day, propellant conservation measures paid off and the crew was advised that it would be granted a ninth full day of science, as originally intended in the mission plan. "That's great news," exulted Gorie. "They're getting some fantastic data on this mission!"
Fantastic, indeed, for SRTM was uncovering the Home Planet as never seen before. By the evening of 13 February, more than 17.7 million square miles (45.8 million square km), about equal to 38 percent of Earth's total land masses, had been mapped in unprecedented detail. "We're starting to see the first 'quick-look' results from the X-band and C-band antennas and the details are fantastic," said SRTM Project Scientist Michael Kobrick of the Jet Propulsion Laboratory (JPL) in Pasadena, Calif. "Even in this lower resolution … we can see many topographic features that were completely invisible in the best maps we have today." Kobrick later noted that Endeavour's crew were mapping approximately 38,000 square miles (100,000 square kilometers) every minute, more than tripling the world's supply of digital terrain elevation data. By the fifth day of the flight, 15 February, more than half of the targeted land surface had been mapped and around 20 percent had been mapped twice, covering regions the size of Africa, North America, and Australia combined. Dozens of sites were mapped two and three times and images of Brazil, South Africa, and New Zealand's South Island were considered so spectacular in their topographical detail that enthusiastic scientists gushed that the data would be used for decades to come. Although "quick-look" data was available to researchers, the bulk of the SRTM results were stored on about 270 high-density tapes, which contained approximately the same amount of information as 13,500 CDs.
SRTM radar image of the volcano Cotopaxi in Ecuador. Image Credit: NASA/NIMA
As STS-99 wore on, additional flycast maneuvers continued to fine-tune Endeavour's orientation. The sixth such manoeuvre of the mission was executed early on 18 February and lasted slightly longer than previous burns, in order to conserve propellant by eliminating another flycast planned for the 20th. By this stage, one week into the 11-day flight, over 83 percent of the pre-launch scientific targets had been mapped on at least one occasion, with over 50 percent surveyed two or more times. NASA explained that the rate of mapping coverage allowed SRTM to cover the equivalent of the state of Alaska in just 15 minutes and Rhode Island in less than two seconds. Images of the San Andreas Fault and the Rose Bowl area of southern California, together with the Kamchatka Peninsula in Russia's Far East and the Hawaiian island of Oahu were judged as so significant that they could lead to new insights into wildfires, lava flows, tsunamis, and localised flooding. An additional nine hours of mapping time, and, later, on 20 February, an extra 10 minutes, was granted to the crew for their radar observations. Although a seemingly small addition to the timeline, those extra 10 minutes allowed SRTM to radar-map Flinders Island on the northeast corner of Tasmania, which completed the mission's coverage of Australia and its neighbouring islands in their entirety. It also brought up the total mapping coverage to 99.96 percent of the pre-launch targeted sites. Elsewhere aboard the shuttle, the EarthKAM digital camera acquired more than 2,700 images of the Home Planet on behalf of student investigators from 75 middle schools around the world.
As they worked, the sight of Earth in all its glory in their windows provided an ever-present source of inspiration for the crew. "I can't see how anyone who's spent any time in space would say it would be boring," said Kregel before the flight. "I can spend two weeks easily, just looking out the window. We're going to be kept pretty busy. We've got to do maneuvers every 45 minutes to maintain the accuracy that's required. We have to change out the tapes. We're there to back up when ground commanding is not available, to go ahead and start taking the data." For Janice Voss, who served as "Payload Lead" for the blue shift, it was "beyond my comprehension" that space flight could ever become mundane. "If you ever have a little bit of extra time and … need to change your perspective," she said, "you would just look out the window and freshen your mind up for a few seconds and come back to what you're doing."
With the additional hours of radar time, Endeavour's mapping period ended at 6:54 a.m. EST on 21 February 2000, about 24 hours ahead of the scheduled return to Earth. The SRTM instruments and the STS-99 crew had imaged almost all of their targeted areas, save small portions of the United States, which were already well characterised in terms of topography. The scientists who oversaw the mission were united in their praise. "A magnificent accomplishment" was Program Scientist Earnest Paylor's judgement, with Tom Hennig of the Department of Defense's National Imaging and Mapping Agency (NIMA) adding that its success was "absolutely wonderful."
Gerhard Thiele observes a point on Earth during STS-99. Photo Credit: NASA
After 222 hours and 23 minutes of uninterrupted radar-data collection, the planned 18-minute process of retracting the 200-foot (60-meter) mast began at 8:17 a.m. EST on 21 February. The procedure ran crisply, until the mast had been retracted to just an inch (2.5 cm) shy of the canister … then stopped. One of the three latches on the canister's lid had failed to engage properly, although Kregel radioed that from his perspective the protruding segment of mast posed no obstruction and he saw no difficulty in safely closing Endeavour's payload bay doors at the end of the mission. Nor did he consider it necessary to awaken Kavandi and Thiele for a contingency EVA which did not seem necessary. Mission Control agreed. "Appreciate your concerns for your crew members," replied Capcom Steve Robinson from Houston. "Our current plans do not include them heading out the door, so I think you can leave them as is."
Suspicion on the cause of the problem centred on the possibility that the mast had endured cold temperatures whilst fully deployed and that this had reduced its flexibility. At first, the astronauts waited for higher temperatures to warm up any stiffened components inside the canister, then drove open the latches and turned on the retraction motors in the hope that the mast would retract and the latches would re-engage. They did not. "We saw perhaps just a tiny movement at initial power-up, but then nothing else," reported Kregel, glumly, "and, of course, you saw the currents were pretty high." Even switching the retraction motors to their maximum torque only served to move the mast by an additional quarter-inch (0.6 cm), then stalled. Finally, after three failed attempts, the mast was successfully folded into its canister.
That almost 10 full days, or 223 hours, of mapping time was acquired was quite remarkable. Original plans called for 10 days and 10 hours (a total of 250 hours) of mapping operations, with the shutdown of the radar instruments and the retraction of the mast on the day before landing. However, in late January 2000 NASA managers had opted to halt operations about 24 hours earlier, giving the SRTM teams only nine days for science. The reason was linked to nervousness about how well the mast would retract at the end of the mission and to preserve the option for a contingency spacewalk. If Janet Kavandi and Gerhard Thiele were required to perform an EVA to manually crank the mast closed, they would need the additional time to prepare their space suits, pre-breathe pure oxygen, and perform the spacewalk itself.
Janet Kavandi, Dom Gorie, and Mamoru Mohri are pictured on Endeavour's middeck during the 11-day STS-99 mission. Photo Credit: NASA
Leaving the retraction until the final day before landing offered no time in the flight plan to handle unforeseen problems. Also, since the radar consumed so much energy during the mission (about 900 kilowatt-hours, or enough to power an average home on Earth for two months), an EVA would not have been possible after a full 250 hours of mapping. "This is a device we've never deployed before," explained STS-99 Lead Flight Director Paul Dye. "It's the longest space structure anybody's ever put out and we would like to be able to get it back. If we had a problem on the stow day, we'd have had no opportunity to try to fix that problem with an EVA or other means. We had stretched the mission as long as we possibly could." Dye compared taking 24 hours off the mapping time as the difference between "a glass that's 10 percent empty or 90 percent full." With the extension of mapping activities by the additional nine hours, then an additional 10 minutes on top of that, most of SRTM's originally baselined radar time was met.
When judging the success of SRTM, the numbers spoke for themselves: eight terabytes of data collected, 332 high-density data tapes (equivalent to more than 20,600 CDs) filled, 99.98 percent of targeted sites mapped on at least one occasion, and 94.6 percent of it mapped on at least two occasions. In fact, several sites, with a total land area larger than the United States, were mapped as many as four times during the flight. In years to come, it was expected that the SRTM data would support a range of civilian and military applications, including the enhancement of ground collision-avoidance systems for aircraft, civil engineering projects, land-use planning, disaster recovery, line-of-sight determination for cellular communications, the development of better flight simulators, logistical planning, air traffic management, missile and weapons guidance systems, and battlefield management tactics.
"There are a lot of benefits for our lives," explained Mamoru Mohri, drawing particular attention to a huge earthquake which hit the harbor city of Kobe, on the southern side of the Japanese island of Honshū in January 1995. "More than 5,000 people were killed. This tragedy happened because of the fact that some houses were built on a fault … and this fault could not be predicted to cause such serious damage. If we had known the land more precisely, thousands of lives could have been saved. There are many unstable ground areas in the world and in the future we may be able to alert people who live in such areas about imminent dangers."
Landing day for STS-99, on 22 February 2000, brought news of weather conditions which seemed grim and questionable to support Endeavour's return to Earth. High winds and potential heavy cloud cover seriously threatened the orbiter's return to KSC. On the West Coast of the United States, Edwards Air Force Base, Calif., had been activated and placed on standby to support the landing if necessary. The first KSC opportunity, which would have produced a landing on Runway 33 at 4:50 p.m. EST, was waved off, due to ongoing concerns about the weather, but the Mission Management Team (MMT) eventually opted for the second opportunity.
Kregel and Gorie guided Endeavour to a smooth touchdown on KSC's Runway 33 at 6:22 p.m. EST, closing out a spectacularly successful 11-day mission. They had uncovered the Home Planet as never before and had established themselves as the first humans to journey into space in the Year 2000. With the Mir space station having been vacated by its most recent long-duration crew in August 1999, the year had begun with not a single human being in orbit around Earth. The STS-99 crew gained the honor of being first purely by happenstance, but there surely could have been no better mission to begin a new millennium than one which turned our gaze back to the cradle from which we came and enhanced our understanding of its beauty, its majesty, and its mystery.

Copyright © 2015 AmericaSpace - All Rights Reserved