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60 Years Ago: Lunar Landing Research Vehicle Takes Flight
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By NASA
President John F. Kennedy’s national commitment to land a man on the Moon and return him safely to the Earth before the end of the decade posed multiple challenges, among them how to train astronauts to land on the Moon, a place with no atmosphere and one-sixth the gravity on Earth. The Lunar Landing Research Vehicle (LLRV) and its successor the Lunar Landing Training Vehicle (LLTV) provided the training tool to simulate the final 200 feet of the descent to the lunar surface. The ungainly aircraft made its first flight on Oct. 30, 1964, at NASA’s Flight Research Center (FRC), now NASA’s Armstrong Flight Research Center (AFRC) in California. The Apollo astronauts who completed landings on the Moon attributed their successes largely to training in these vehicles.
The first Lunar Landing Research Vehicle silhouetted against the rising sun on the dry lakebed at Edwards Air Force Base in California’s Mojave Desert.
In December 1961, NASA Headquarters in Washington, D.C., received an unsolicited proposal from Bell Aerosystems in Buffalo, New York, for a design of a flying simulator to train astronauts on landing a spacecraft on the Moon. Bell’s approach, using their design merged with concepts developed at NASA’s FRC, won approval and the space agency funded the design and construction of two Lunar Landing Research Vehicles (LLRV). At the time of the proposal, NASA had not yet chosen the method for getting to and landing on the Moon, but once NASA decided on Lunar Orbit Rendezvous in July 1962, the Lunar Module’s (LM) flying characteristics matched Bell’s proposed design closely enough that the LLRV served as an excellent trainer.
Two views of the first Lunar Landing Research Vehicle shortly after its arrival and prior to assembly at the Flight Research Center, now NASA’s Armstrong Flight Research Center, in California.
Bell Aerosystems delivered the LLRV-1 to FRC on April 8, 1964, where it made history as the first pure fly-by-wire aircraft to fly in Earth’s atmosphere. Its design relied exclusively on an interface with three analog computers to convert the pilot’s movements to signals transmitted by wire and to execute his commands. The open-framed LLRV used a downward pointing turbofan engine to counteract five-sixths of the vehicle’s weight to simulate lunar gravity, two rockets provided thrust for the descent and horizontal translation, and 16 LM-like thrusters provided three-axis attitude control. The astronauts could thus simulate maneuvering and landing on the lunar surface while still on Earth. The LLRV pilot could use an aircraft-style ejection seat to escape from the vehicle in case of loss of control.
Left: The Lunar Landing Research Vehicle-1 (LLRV-1) during an engine test at NASA’s Flight Research Center (FRC), now NASA’s Armstrong Fight Research Center, in California’s Mojave Desert. Right: NASA chief test pilot Joseph “Joe” A. Walker, left, demonstrates the features of LLRV-1 to President Lyndon B. Johnson during his visit to FRC.
Engineers conducted numerous tests to prepare the LLRV for its first flight. During one of the engine tests, the thrust generated was higher than anticipated, lifting crew chief Raymond White and the LLRV about a foot off the ground before White could shut off the engines. On June 19, during an official visit to FRC, President Lyndon B. Johnson inspected the LLRV featured on a static display. The Secret Service would not allow the President to sit in the LLRV’s cockpit out of an overabundance of caution since the pyrotechnics were installed, but not yet armed, in the ejection seat. Following a Preflight Readiness Review held Aug. 13 and 14, managers cleared the LLRV for its first flight.
Left: NASA chief test pilot Joseph “Joe” A. Walker during the first flight of the Lunar Landing Research Vehicle (LLRV). Right: Walker shortly after the first LLRV flight.
In the early morning of Oct. 30, 1964, FRC chief pilot Joseph “Joe” A. Walker arrived at Edwards Air Force Base’s (AFB) South Base to attempt the first flight of the LLRV. Walker, a winner of both the Collier Trophy and the Harmon International Trophy, had flown nearly all experimental aircraft at Edwards including 25 flights in the X-15 rocket plane. On two of his X-15 flights, Walker earned astronaut wings by flying higher than 62 miles, the unofficial boundary between the Earth’s atmosphere and space. After strapping into the LLRV’s ejection seat, Walker ran through the preflight checklist before advancing the throttle to begin the first flight. The vehicle rose 10 feet in the air, Walker performed a few small maneuvers and then made a soft landing after having flown for 56 seconds. He lifted off again, performed some more maneuvers, and landed again after another 56 seconds. On his third flight, the vehicle’s electronics shifted into backup mode and he landed the craft after only 29 seconds. Walker seemed satisfied with how the LLRV handled on its first flights.
Left: Lunar Landing Research Vehicle-2 (LLRV-2) during one of its six flights at the Flight Research Center, now NASA’s Armstrong Flight Research Center, in California in January 1967. Right: NASA astronaut Neil A. Armstrong with LLRV-1 at Ellington Air Force Base in March 1967.
Walker took LLRV-1 aloft again on Nov. 16 and eventually completed 35 test flights with the vehicle. Test pilots Donald “Don” L. Mallick, who completed the first simulated lunar landing profile flight during the LLRV’s 35th flight on Sept. 8, 1965, and Emil E. “Jack” Kluever, who made his first flight on Dec. 13, 1965, joined Walker to test the unique aircraft. Joseph S. “Joe” Algranti and Harold E. “Bud” Ream, pilots at the Manned Spacecraft Center (MSC), now NASA’s Johnson Space Center (JSC) in Houston, travelled to FRC to begin training flights with the LLRV in August 1966. Workers at FRC assembled the second vehicle, LLRV-2, during the latter half of 1966. In December 1966, after 198 flights workers transferred LLRV-1 to Ellington AFB near MSC for the convenience of astronaut training, and LLRV-2 followed in January 1967 after completing six test flights at FRC. The second LLRV made no further flights, partly because the three Lunar Landing Training Vehicles (LLTVs), more advanced models that better simulated the LM’s flying characteristics, began to arrive at Ellington in October 1967. Neil A. Armstrong completed the first astronaut flights aboard LLRV-1 on Mar. 23, 1967, and flew 21 flights before ejecting from the vehicle on May 6, 1968, seconds before it crashed. He later completed his lunar landing certification flights using LLTV-2 in June 1969, one month before peforming the actual feat on the Moon.
Left: Apollo 11 Commander Neil A. Armstrong prepares to fly a lunar landing profile in Lunar Landing Training Vehicle-2 (LLTV-2) in June 1969. Middle: Apollo 12 Commander Charles “Pete” Conrad prepares to fly LLTV-2 in July 1969. Right: Apollo 14 Commander Alan B. Shepard flies LLTV-3 in December 1970.
All Apollo Moon landing mission commanders and their backups completed their lunar landing certifications using the LLTV, and all the commanders attributed their successful landings to having trained in the LLTV. Apollo 8 astronaut William A. Anders, who along with Armstrong completed some of the early LLRV test flights, called the training vehicle “a much unsung hero of the Apollo program.” During the flight readiness review in January 1970 to clear LLTV-3 for astronaut flights, Apollo 11 Commander Armstrong and Apollo 12 Commander Charles “Pete” Conrad, who had by then each completed manual landings on the Moon, spoke positively of the LLTV’s role in their training. Armstrong’s overall impression of the LLTV: “All the pilots … thought it was an extremely important part of their preparation for the lunar landing attempt,” adding “It was a contrary machine, and a risky machine, but a very useful one.” Conrad emphasized that were he “to go back to the Moon again on another flight, I personally would want to fly the LLTV again as close to flight time as possible.” During the Apollo 12 technical debriefs, Conrad stated the “the LLTV is an excellent training vehicle for the final phases. I think it’s almost essential. I feel it really gave me the confidence that I needed.” During the postflight debriefs, Apollo 14 Commander Alan B. Shepard stated that he “did feel that the LLTV contributed to my overall ability to fly the LM during the landing.”
Left: Apollo 15 Commander David R. Scott flies Lunar Landing Training Vehicle-3 (LLTV-3) in June 1971. Middle: Apollo 16 Commander John W. Young prepares to fly LLTV-3 in March 1972. Right: Apollo 17 Commander Eugene A. Cernan prepares for a flight aboard LLTV-3 in October 1972.
David R. Scott, Apollo 15 commander, stated in the final mission report that “the combination of visual simulations and LLTV flying provided excellent training for the actual lunar landing. Comfort and confidence existed throughout this phase.” In the Apollo 15 postflight debrief, Scott stated that he “felt very comfortable flying the vehicle (LM) manually, because of the training in the LLTV, and there was no question in my mind that I could put it down where I wanted to. I guess I can’t say enough about that training. I think the LLTV is an excellent simulation of the vehicle.” Apollo 16 Commander John W. Young offered perhaps the greatest praise for the vehicle just moments after landing on the lunar surface: “Just like flying the LLTV. Piece of cake.” Young reiterated during the postflight debriefs that “from 200 feet on down, I never looked in the cockpit. It was just like flying the LLTV.” Apollo 17 Commander Eugene A. Cernan stated in the postflight debrief that “the most significant part of the final phases from 500 feet down, … was that it was extremely comfortable flying the bird. I contribute (sic) that primarily to the LLTV flying operations.”
Left: Workers move Lunar Landing Research Vehicle-2 from NASA’s Armstrong Flight Research Center for display at the Air Force Test Flight Museum at Edwards Air Force Base. Right: Lunar Landing Training Vehicle-3 on display outside the Teague Auditorium at NASA’s Johnson Space Center in Houston.
In addition to playing a critical role in the Moon landing program, these early research and test vehicles aided in the development of digital fly-by-wire technology for future aircraft. LLRV-2 is on display at the Air Force Flight Test Museum at Edwards AFB (on loan from AFRC). Visitors can view LLTV-3 suspended from the ceiling in the lobby of the Teague Auditorium at JSC.
The monograph Unconventional, Contrary, and Ugly: The Lunar Landing Research Vehicle provides an excellent and detailed history of the LLRV.
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Editor’s note: This article was published May 23, 2003, in NASA Armstrong’s X-Press newsletter. NASA’s Dryden Flight Research Center in Edwards, California, was redesignated Armstrong Flight Research Center on March 1, 2014. Ken Iliff was inducted into the National Hall of Fame for Persons with Disabilities in 1987. He died Jan. 4, 2016.
Alphonso Stewart, from left, Ken Iliff, and Dale Reed study lifting body aircraft models at NASA’s Armstrong (then Dryden) Flight Research Center in Edwards, California.NASA As an Iowa State University engineering student in the early 1960s, Ken Iliff was hard at work on a glider flight simulation.
Upon examining the final results – which, in those early days of the computer revolution, were viewed on a long paper printout – he noticed one glaring imperfection: the way he had programmed it, his doomed glider would determinedly accelerate as it headed for the ground.
The culprit was a single keystroke. At the time, programming was based on data that had been painstakingly entered into the computer by hand, on punch cards and piece by piece. Somewhere, Iliff had entered a plus sign instead of a minus sign.
The seemingly minor incident was to foreshadow great things to come in Iliff’s career.
Not long after graduation, the West Union, Iowa, native found himself at what was then called simply the NASA Flight Research Center located on Edwards Air Force Base.
“I just knew I didn’t want to be sitting somewhere in a big room full of engineers who were all doing the same thing,” Iliff said of choosing Dryden over other jobs and other NASA centers. “It was a small center doing important things, and it was in California. I knew I wanted to be there.”
Once at Dryden, the issue of data tidbits was central to the new hire’s workday. Iliff’s post called for him and many of his colleagues to spend much of their time “reading up” data – a laborious process of measuring data from film using a single reference line and a ruler. Measurements were made every tenth of a second; for a ten-second maneuver, a total of one hundred “traces” were taken for every quantity being recorded.
“I watched talented people spending entire days analyzing data,” he recalled. “And then, maybe two people would arrive at two entirely different conclusions” from the same data sets.
As has happened so often at the birth of revolutionary ideas, then, one day Iliff had a single, simple thought about the time-intensive and maddeningly inexact data analysis process:
“There just has to be a better way to do this.”
The remedy he devised was to result in a sea change at Dryden, and would reverberate throughout the world of computer-based scientific research.
Iliff’s work spanned the decades that encompassed some of Dryden’s greatest achievements, from the X-15 through the XB-70 and the tentative beginnings of the shuttle program. The solution he created to the problem of inaccuracy in data analysis focused on aerodynamic performance – how to formulate questions about an aircraft’s performance once answers about it are already known, how to determine the “why?” when the “what happens?” has already happened.
The work is known as “parameter estimation,” and is used in aerospace applications to extract precise definitions of aerodynamic, structural and performance parameters from flight data.
His methodology – cemented in computer coding Iliff developed using Fortran’s lumbering binary forerunner, machine code – allowed researchers to determine precisely the type of information previously derived only as best-estimate guesses through analysis of data collected in wind tunnels and other flight-condition simulators. In addition to aerospace science, parameter estimation is also used today in a wide array of research applications, including those involving submarines, economic models, and biomedicine.
With characteristic deference, Iliff now brushes off any suggestion of his discovery’s significance. Instead, he credits other factors for his successes, such as a Midwestern work ethic and Iowa State University’s early commitment to giving its engineering students good access to the new and emerging computer technology.
To hear him tell it, “all good engineers are a little bit lazy. We know how to innovate – how to find an easier way.
“I’d been trained well, and given the right tools – I was just in the right place at the right time.”
But however modestly he might choose to see it characterized, it’s fair to number Iliff’s among the longest and most distinguished careers to take root in the ranks of Dryden research engineers. Though his groundbreaking work will live forever in research science, when Iliff retired in December he brought to a close his official role in some of the most important chapters in Dryden history.
Ken Iliff worked for four decades on revolutionary aircraft and spacecraft, including the X-29 forward swept wing aircraft behind him, at NASA’s Armstrong (then Dryden) Flight Research Center in Edwards, California.NASA His pioneering work with parameter estimation carried through years of aerodynamic assessment and data analysis involving lifting-body and wing-body aircraft, from the X-15 through the M2-F1, M2-F2 and M2-F3 projects, the HL-10, the X-24B and NASA’s entire fleet of space shuttles. His contributions aided in flight research on the forward-swept-wing X-29 and the F/A-18 High Angle of Attack program, on F-15 spin research vehicles, on thrust vectoring and supermaneuverability.
Iliff began work on the space shuttle program when it was little more than a speculative “what’s next?” chapter in manned spaceflight, long before it reached officially sanctioned program status. Together with a group spearheaded by the late NASA research pilot and long-time Dryden Chief Engineer Milt Thompson – who Iliff describes unflinchingly as “my hero” – Iliff helped explore the vast range of possibilities for a new orbiting craft that would push NASA to its next frontier after landing on the moon.
In an environment much more informal than today’s, when there were few designations of “program manager” or “task monitor” or “deputy director” among NASA engineers like Iliff and Thompson, a handful of creative, disciplined minds were at work dreaming up a reusable aircraft that would launch, orbit the Earth and return. Iliff’s role was to offer up the rigor of comparison in size, speed and performance among potential aircraft designs; Thompson and Iliff’s group was responsible, for example, for the decision to abandon the notion of jet engines on the orbiter, decreeing them too heavy, too risky and too inefficient.
Month in and month out, Iliff and his colleagues painstakingly researched and developed the myriad design details that eventually materialized into the shuttle fleet. There was, in Iliff’s words, “a love affair between the shuttle and the engineers.”
And in a display typifying the charged environment of creative collaboration that governed the effort – an effort many observe wryly that it would be difficult to replicate at NASA, today or anytime – the body of research was compiled into the now-legendary aero-data book, a living document that records in minute detail every scrap of design and performance data recorded about the shuttles’ flight activity.
Usually with more than a touch of irony, the compiling of the aero-data book has been described with phrases like “a remarkably democratic process,” involving as it did the need for a hundred independent minds and strong personalities to agree on indisputable facts about heat, air flow, turbulence, drag, stability and a dozen other aerodynamic principles. But Iliff says the success of the mammoth project, last updated in 1996, was ultimately enabled by a shared commitment to a culture that was unique to Dryden, one that made the Center great.
“Well, big, complicated things don’t always come out like you think they will,” Iliff said.
“But we understood completely the idea of ‘informed risk.’ We had a thorough understanding of risks before taking them – nobody ever did anything on the shuttle that they thought was dangerous, or likely to fail.
“The truly great thing (about that era at Dryden) was that they mentored us, and let us take those risks, and helped us get good right away. That was how we were able to do what we did.”
It was an era that Iliff says he was thrilled to be a part of, and which he admits was difficult to leave. It was also, he adds with a note of uncharacteristic nostalgia, a time that would be hard to reinvent today after the intrusion of so many bureaucratic tentacles into the hot zone that spawned Dryden’s greatest achievements.
A man not much given to dwelling on the past, however, Iliff has moved on to a retirement he is making the most of. Together with his wife, Mary Shafer, also retired from her career as a Dryden engineer, he plans to dedicate time to cataloging the couple’s extensive travel experiences with new video and graphics software, and adding to the travel library with footage from new trips. Iraq ranks high on the short list.
During his 40-year tenure, Iliff held the post of senior staff scientist of Dryden’s research division from 1988 to 1994, when he became the Center’s chief scientist. Among numerous awards he received were the prestigious Kelly Johnson Award from the Society of Flight Test Engineers (1989), an award permanently housed in the Smithsonian National Air and Space Museum, and NASA’s highest scientific honor, the NASA Exceptional Scientific Achievement Award (1976).
He was inducted into the National Hall of Fame for Persons with Disabilities in 1987, and served on many national aeronautic and aerospace committees throughout his career. He is a Fellow in the American Institute of Aeronautics and Astronautics (AIAA) and is the author of more than 100 technical papers and reports. He has given eleven invited lectures for NATO and AGARD (Advisory Group for Aerospace Research and Development), and served on four international panels as an expert in aircraft and spacecraft dynamics. Recently, he retired from his position as an adjunct professor of electrical engineering at the University of California, Los Angeles.
Iliff holds dual bachelor of science degrees in mathematics and aerospace engineering from Iowa State University; a master of science in mechanical engineering from the University of Southern California; a master of engineering degree in engineering management and a Ph.D. in electrical engineering, both from UCLA.
Iliff’s is the kind of legacy shared by a select group of American engineers, and to read the papers these days, there’s the suggestion that his is a vanishing breed. NASA and other science-based organizations are often depicted as scrambling for new engineering talent – particularly of the sort personified by Iliff and his pioneering achievements.
But, typical of the visionary approach he applies to life in general as well as to science, Iliff takes a wider view.
“I remember, after the X-1 – people figured all the good things had been done,” he said, with a smile in his voice. “And of course, they had not.
“If I was starting out now, I’d be starting in work with DNA, or biomedicine – improving lives with drug research. There are so many exciting things to be discovered there. They might not be as showy as lighting off a rocket, but they’re there.
“I’ve seen cycles. We’re at a low spot right now – but military, or space, will eventually be at the center again.”
And when that day comes, Iliff says he hopes officials in the flight research world will heed the example of Dryden’s early years, and give its engineers every opportunity to succeed unfettered – as he had been.
“Beware the ‘Chicken Littles’ out there,” he said. “I hope the government will be strong enough to resist them.”
Sarah Merlin
Former X-Press newsletter assistant editor
Former Dryden historian Curtis Peebles contributed to this article.
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Last Updated Oct 29, 2024 EditorDede DiniusContactJay Levinejay.levine-1@nasa.govLocationArmstrong Flight Research Center Related Terms
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6 min read
Preparations for Next Moonwalk Simulations Underway (and Underwater)
With one of its solar arrays deployed, NASA’s Lunar Trailblazer sits in a clean room at Lockheed Martin Space. The large silver grate attached to the spacecraft is the radiator for HVM³, one of two instruments that the mission will use to better understand the lunar water cycle.Lockheed Martin Space There’s water on the Moon, but scientists only have a general idea of where it is and what form it is in. A trailblazing NASA mission will get some answers.
When NASA’s Lunar Trailblazer begins orbiting the Moon next year, it will help resolve an enduring mystery: Where is the Moon’s water? Scientists have seen signs suggesting it exists even where temperatures soar on the lunar surface, and there’s good reason to believe it can be found as surface ice in permanently shadowed craters, places that have not seen direct sunlight for billions of years. But, so far, there have been few definitive answers, and a full understanding of the nature of the Moon’s water cycle remains stubbornly out of reach.
This is where Lunar Trailblazer comes in. Managed by NASA’s Jet Propulsion Laboratory and led by Caltech in Pasadena, California, the small satellite will map the Moon’s surface water in unprecedented detail to determine the water’s abundance, location, form, and how it changes over time.
“Making high-resolution measurements of the type and amount of lunar water will help us understand the lunar water cycle, and it will provide clues to other questions, like how and when did Earth get its water,” said Bethany Ehlmann, principal investigator for Lunar Trailblazer at Caltech. “But understanding the inventory of lunar water is also important if we are to establish a sustained human and robotic presence on the Moon and beyond.”
Future explorers could process lunar ice to create breathable oxygen or even fuel. And they could also conduct science. Using information from Lunar Trailblazer, future human or robotic scientific investigations could sample the ice for later study to determine where the water came from. For example, the presence of ammonia in ice samples may indicate the water came from comets; sulfur, on the other hand, could show that it was vented to the surface from the lunar interior when the Moon was young and volcanically active.
This artist’s concept depicts NASA’s Lunar Trailblazer in lunar orbit about 60 miles (100 kilometers) from the surface of the Moon. The spacecraft weighs only 440 pounds (200 kilograms) and measures 11.5 feet (3.5 meters) wide when its solar panels are fully deployed.Lockheed Martin Space “In the future, scientists could analyze the ice in the interiors of permanently shadowed craters to learn more about the origins of water on the Moon,” said Rachel Klima, Lunar Trailblazer deputy principal investigator at the Johns Hopkins Applied Physics Laboratory in Laurel, Maryland. “Like an ice core from a glacier on Earth can reveal the ancient history of our planet’s atmospheric composition, this pristine lunar ice could provide clues as to where that water came from and how and when it got there.”
Understanding whether water molecules move freely across the surface of the Moon or are locked inside rock is also scientifically important. Water molecules could move from frosty “cold traps” to other locations throughout the lunar day. Frost heated by the Sun sublimates (turning from solid ice to a gas without going through a liquid phase), allowing the molecules to move as a gas to other cold locations, where they could form new frost as the Sun moves overhead. Knowing how water moves on the Moon could also lead to new insights into the water cycles on other airless bodies, such as asteroids
Two Instruments, One Mission
Two science instruments aboard the spacecraft will help unlock these secrets: the High-resolution Volatiles and Minerals Moon Mapper (HVM3) infrared spectrometer and the Lunar Thermal Mapper (LTM) infrared multispectral imager.
Developed by JPL, HVM3 will detect and map the spectral fingerprints, or wavelengths of reflected sunlight, of minerals and the different forms of water on the lunar surface. The spectrometer can use faint reflected light from the walls of craters to see the floor of even permanently shadowed craters.
The LTM instrument, which was built by the University of Oxford and funded by the UK Space Agency, will map the minerals and thermal properties of the same lunar landscape. Together they will create a picture of the abundance, location, and form of water while also tracking how its distribution changes over time.
“The LTM instrument precisely maps the surface temperature of the Moon while the HVM3 instrument looks for the spectral signature of water molecules,” said Neil Bowles, instrument scientist for LTM at the University of Oxford. “Both instruments will allow us to understand how surface temperature affects water, improving our knowledge of the presence and distribution of these molecules on the Moon.”
Weighing only 440 pounds (200 kilograms) and measuring 11.5 feet (3.5 meters) wide when its solar panels are fully deployed, Lunar Trailblazer will orbit the Moon about 60 miles (100 kilometers) from the surface. The mission was selected by NASA’s SIMPLEx (Small Innovative Missions for Planetary Exploration) program in 2019 and will hitch a ride on the same launch as the Intuitive Machines-2 delivery to the Moon through NASA’s Commercial Lunar Payload Services initiative. Lunar Trailblazer passed a critical operational readiness review in early October at Caltech after completing environmental testing in August at Lockheed Martin Space in Littleton, Colorado, where it was assembled.
The orbiter and its science instruments are now being put through flight system software tests that simulate key aspects of launch, maneuvers, and the science mission while in orbit around the Moon. At the same time, the operations team led by IPAC at Caltech is conducting tests to simulate commanding, communication with NASA’s Deep Space Network, and navigation.
More About Lunar Trailblazer
Lunar Trailblazer is managed by JPL, and its science investigation and mission operations are led by Caltech with the mission operations center at IPAC. Managed for NASA by Caltech, JPL also provides system engineering, mission assurance, the HVM3 instrument, as well as mission design and navigation. Lockheed Martin Space provides the spacecraft, integrates the flight system, and supports operations under contract with Caltech.
SIMPLEx mission investigations are managed by the Planetary Missions Program Office at NASA’s Marshall Space Flight Center in Huntsville, Alabama, as part of the Discovery Program at NASA Headquarters in Washington. The program conducts space science investigations in the Planetary Science Division of NASA’s Science Mission Directorate at NASA Headquarters.
For more information about Lunar Trailblazer, visit:
https://www.jpl.nasa.gov/missions/lunar-trailblazer
News Media Contacts
Karen Fox / Molly Wasser
NASA Headquarters, Washington
202-358-1600
karen.c.fox@nasa.gov / molly.l.wasser@nasa.gov
Ian J. O’Neill
Jet Propulsion Laboratory, Pasadena, Calif.
818-354-2649
ian.j.oneill@jpl.nasa.gov
Gordon Squires
IPAC, Pasadena, Calif.
626-395-3121
squires@ipac.caltech.edu
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Last Updated Oct 29, 2024 Related Terms
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By European Space Agency
Image: The construction phase of ESA’s Ariel mission has started at Airbus Defence and Space in Toulouse (France) with the assembly of the spacecraft’s structural model. This marks a significant step forward for this mission designed to meticulously inspect the atmospheres of a thousand exoplanets and uncover their nature.
In the image we see Ariel’s structural model coming together at the Airbus facilities. This model replicates the mechanical framework of the spacecraft and the mass of its various units for a first round of tough testing.
The Ariel’s structural model consists of two main components: a flight-like replica of the service module (bottom right) and a simplified mechanical mock-up of the payload module (top right). This assembly mimics the structure of the flight spacecraft, where the science instruments make up the payload while the service module houses the essential components for the functioning of the spacecraft, such as the propulsion, and the power and communication systems.
The goal for the end of the year is to complete the mechanical test campaign of the spacecraft’s structural model. This will ensure that Ariel’s design is up-to-spec and can withstand the mechanical strains expected during launch.
The testing phase will include vibration and acoustic test campaigns. During vibration tests the model will be progressively shaken at different strengths on a vibrating table, or 'the shaker'. During acoustic tests, it will be placed in a reverberating chamber and ‘bombarded’ with very intense noise, like it will encounter during launch.
This model will also be used to assess how the loads are distributed and to perform a first ‘separation and shock’ test using the same mounting system as will be used to mount the spacecraft on the Ariane 6.
When ready, Ariel will be launched by an Ariane 6.2 rocket and journey to the second Lagrangian Point from where it will carry out its uniquely detailed studies of remote worlds.
Image description: A collage of three photographs that show the assembly of the model of a spacecraft in a large white hall. The first image on the left shows the entire model, with a person next to it who is nearly equal in height. The second image on the upper right zooms in on the top part of the mock science instrument: a circular fan-like structure with a big rectangular silver box on top. The third image on the lower right focuses on the bottom of the model, which looks like a large round silver box.
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By NASA
This image shows nine candidate landing regions for NASA’s Artemis III mission, with each region containing multiple potential sites for the first crewed landing on the Moon in more than 50 years. The background image of the lunar South Pole terrain within the nine regions is a mosaic of LRO (Lunar Reconnaissance Orbiter) WAC (Wide Angle Camera) images.Credit: NASA As NASA prepares for the first crewed Moon landing in more than five decades, the agency has identified an updated set of nine potential landing regions near the lunar South Pole for its Artemis III mission. These areas will be further investigated through scientific and engineering study. NASA will continue to survey potential areas for missions following Artemis III, including areas beyond these nine regions.
“Artemis will return humanity to the Moon and visit unexplored areas. NASA’s selection of these regions shows our commitment to landing crew safely near the lunar South Pole, where they will help uncover new scientific discoveries and learn to live on the lunar surface,” said Lakiesha Hawkins, assistant deputy associate administrator, Moon to Mars Program Office.
NASA’s Cross Agency Site Selection Analysis team, working closely with science and industry partners, added, and excluded potential landing regions, which were assessed for their science value and mission availability.
The refined candidate Artemis III lunar landing regions are, in no priority order:
Peak near Cabeus B Haworth Malapert Massif Mons Mouton Plateau Mons Mouton Nobile Rim 1 Nobile Rim 2 de Gerlache Rim 2 Slater Plain These regions contain diverse geological characteristics and offer flexibility for mission availability. The lunar South Pole has never been explored by a crewed mission and contains permanently shadowed areas that can preserve resources, including water.
“The Moon’s South Pole is a completely different environment than where we landed during the Apollo missions,” said Sarah Noble, Artemis lunar science lead at NASA Headquarters in Washington. “It offers access to some of the Moon’s oldest terrain, as well as cold, shadowed regions that may contain water and other compounds. Any of these landing regions will enable us to do amazing science and make new discoveries.”
To select these landing regions, a multidisciplinary team of scientists and engineers analyzed the lunar South Pole region using data from NASA’s Lunar Reconnaissance Orbiter and a vast body of lunar science research. Factors in the selection process included science potential, launch window availability, terrain suitability, communication capabilities with Earth, and lighting conditions. Additionally, the team assessed the combined trajectory capabilities of NASA’s SLS (Space Launch System) rocket, the Orion spacecraft, and Starship HLS (Human Landing System) to ensure safe and accessible landing sites.
The Artemis III geology team evaluated the landing regions for their scientific promise. Sites within each of the nine identified regions have the potential to provide key new insights into our understanding of rocky planets, lunar resources, and the history of our solar system.
“Artemis III will be the first time that astronauts will land in the south polar region of the Moon. They will be flying on a new lander into a terrain that is unique from our past Apollo experience,” said Jacob Bleacher, NASA’s chief exploration scientist. “Finding the right locations for this historic moment begins with identifying safe places for this first landing, and then trying to match that with opportunities for science from this new place on the Moon.”
NASA’s site assessment team will engage the lunar science community through conferences and workshops to gather data, build geologic maps, and assess the regional geology of eventual landing sites. The team also will continue surveying the entire lunar South Pole region for science value and mission availability for future Artemis missions. This will include planning for expanded science opportunities during Artemis IV, and suitability for the LTV (Lunar Terrain Vehicle) as part of Artemis V.
The agency will select sites within regions for Artemis III after it identifies the mission’s target launch dates, which dictate transfer trajectories, or orbital paths, and surface environment conditions.
Under NASA’s Artemis campaign, the agency will establish the foundation for long-term scientific exploration at the Moon, land the first woman, first person of color, and its first international partner astronaut on the lunar surface, and prepare for human expeditions to Mars for the benefit of all.
For more information on Artemis, visit:
https://www.nasa.gov/specials/artemis
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James Gannon / Molly Wasser
Headquarters, Washington
202-358-1600
james.h.gannon@nasa.gov / molly.l.wasser@nasa.gov
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Last Updated Oct 28, 2024 EditorJessica TaveauLocationNASA Headquarters Related Terms
Artemis Artemis 3 Earth's Moon Exploration Systems Development Mission Directorate Human Landing System Program Humans in Space Space Launch System (SLS) View the full article
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