Cable system which supports the test subject on the Reduced Gravity Walking Simulator. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. A.W. Vigil described the purpose of the simulator as follows: "When the astronauts land on the moon they will be in an unfamiliar environment involving, particularly, a gravitational field only one-sixth as strong as on earth. A novel method of simulating lunar gravity has been developed and is supported by a puppet-type suspension system at the end of a long pendulum. A floor is provided at the proper angle so that one-sixth of the subject's weight is supported by the floor with the remainder being supported by the suspension system. This simulator allows almost complete freedom in vertical translation and pitch and is considered to be a very realistic simulation of the lunar walking problem. For this problem this simulator suffers only slightly from the restrictions in lateral movement it puts on the test subject. This is not considered a strong disadvantage for ordinary walking problems since most of the motions do, in fact, occur in the vertical plane. However, this simulation technique would be severely restrictive if applied to the study of the extra-vehicular locomotion problem, for example, because in this situation complete six degrees of freedom are rather necessary. This technique, in effect, automatically introduces a two-axis attitude stabilization system into the problem. The technique could, however, be used in preliminary studies of extra-vehicular locomotion where, for example, it might be assumed that one axis of the attitude control system on the astronaut maneuvering unit may have failed." -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, (Washington: NASA, 1995); A.W. Vigil, "Discussion of Existing and Planned Simulators for Space Research," Paper presented at Conference on the Role of Simulation in Space Technology," Blacksburg, VA, August 17-21, 1964.

Test subject wearing the pressurized "space" suit for the Reduced Gravity Walking Simulator located at the Lunar Landing Facility. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. A.W. Vigil described the purpose of the simulator in his paper "Discussion of Existing and Planned Simulators for Space Research," "When the astronauts land on the moon they will be in an unfamiliar environment involving, particularly, a gravitational field only one-sixth as strong as on earth. A novel method of simulating lunar gravity has been developed and is supported by a puppet-type suspension system at the end of a long pendulum. A floor is provided at the proper angle so that one-sixth of the subject's weight is supported by the floor with the remainder being supported by the suspension system. This simulator allows almost complete freedom in vertical translation and pitch and is considered to be a very realistic simulation of the lunar walking problem. For this problem this simulator suffers only slightly from the restrictions in lateral movement it puts on the test subject. This is not considered a strong disadvantage for ordinary walking problems since most of the motions do, in fact, occur in the vertical plane. However, this simulation technique would be severely restrictive if applied to the study of the extra-vehicular locomotion problem, for example, because in this situation complete six degrees of freedom are rather necessary. This technique, in effect, automatically introduces a two-axis attitude stabilization system into the problem. The technique could, however, be used in preliminary studies of extra-vehicular locomotion where, for example, it might be assumed that one axis of the attitude control system on the astronaut maneuvering unit may have failed." -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, (Washington: NASA, 1995), p. 377; A.W. Vigil, "Discussion of Existing and Planned Simulators for Space Research," Paper presented at Conference on the Role of Simulation in Space Technology," Blacksburg, VA, August 17-21, 1964.

A test subject being suited up for studies on the Reduced Gravity Walking Simulator located in the hangar at Langley Research Center. The initial version of this simulator was located inside the hangar. Later a larger version would be located at the Lunar Landing Facility. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. Francis B. Smith wrote in his paper "Simulators For Manned Space Research," "I would like to conclude this talk with a discussion of a device for simulating lunar gravity which is very effective and yet which is so simple that its cost is in the order of a few thousand dollars at most, rather than hundreds of thousands. With a little ingenuity, one could almost build this type simulator in his backyard for children to play on. The principle is ...if a test subject is suspended in a sling so that his body axis makes an angle of 9 1/2 degrees with the horizontal and if he then "stands" on a platform perpendicular to his body axis, the component of the earth's gravity forcing him toward the platform is one times the sine of 9 1/2 degrees or approximately 1/6 of the earth's normal gravity field. That is, a 180 pound astronaut "standing" on the platform would exert a force of only 30 pounds - the same as if he were standing upright on the lunar surface." -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, NASA SP-4308; Francis B. Smith, "Simulators For Manned Space Research," Paper for 1966 IEEE International Convention, New York, NY, March 21-25, 1966

Walter Cronkite in the Reduced Gravity Simulator. Various views of Cronkite in the Lunar Landing Research Facility's Reduced Gravity Simulator which was used to train the astronauts for weightlessness. L68-8308 Caption: "During a 1968 visit to Langley, then CBS News Anchorman Walter Cronkite tries out the Reduced Gravity Simulator, a series of cable-supported slings designed to approximate the Moon's gravity, 1/6th that of Earth's." Photograph published in Winds of Change, 75th Anniversary NASA publication, p 91, by James Schultz.

Walter Cronkite in the Reduced Gravity Simulator. Various views of Cronkite in the Lunar Landing Research Facility's Reduced Gravity Simulator which was used to train the astronauts for weightlessness. L68-8308 Caption: "During a 1968 visit to Langley, then CBS News Anchorman Walter Cronkite tries out the Reduced Gravity Simulator, a series of cable-supported slings designed to approximate the Moon's gravity, 1/6th that of Earth's." Photograph published in Winds of Change, 75th Anniversary NASA publication, p 91, by James Schultz.

The Reduced-Gravity Program provides the unique weightless or zero-g environment of space flight for testing and training of human and hardware reactions. The reduced-gravity environment is obtained with a specially modified KC-135A turbojet transport which flies parabolic arcs to produce weightless periods of 20 to 25 seconds. KC-135A cargo bay test area is approximately 60 feet long, 10 feet wide, and 7 feet high. The image shows KC-135A in flight.

Special "space" suit for the Reduced Gravity Walking Simulator located at the Lunar Landing Facility. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. A.W. Vigil described the purpose of the simulator in his paper "Discussion of Existing and Planned Simulators for Space Research," "When the astronauts land on the moon they will be in an unfamiliar environment involving, particularly, a gravitational field only one-sixth as strong as on earth. A novel method of simulating lunar gravity has been developed and is supported by a puppet-type suspension system at the end of a long pendulum. A floor is provided at the proper angle so that one-sixth of the subject's weight is supported by the floor with the remainder being supported by the suspension system. This simulator allows almost complete freedom in vertical translation and pitch and is considered to be a very realistic simulation of the lunar walking problem. For this problem this simulator suffers only slightly from the restrictions in lateral movement it puts on the test subject. This is not considered a strong disadvantage for ordinary walking problems since most of the motions do, in fact, occur in the vertical plane. However, this simulation technique would be severely restrictive if applied to the study of the extra-vehicular locomotion problem, for example, because in this situation complete six degrees of freedom are rather necessary. This technique, in effect, automatically introduces a two-axis attitude stabilization system into the problem. The technique could, however, be used in preliminary studies of extra-vehicular locomotion where, for example, it might be assumed that one axis of the attitude control system on the astronaut maneuvering unit may have failed." -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, (Washington: NASA, 1995), p. 377; A.W. Vigil, "Discussion of Existing and Planned Simulators for Space Research," Paper presented at Conference on the Role of Simulation in Space Technology," Blacksburg, VA, August 17-21, 1964.

A "suited" test subject on the Reduced Gravity Walking Simulator located in the hangar at Langley Research Center. The initial version of this simulator was located inside the hangar. Later a larger version would be located at the Lunar Landing Facility. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. Francis B. Smith wrote in "Simulators For Manned Space Research:" "The cables which support the astronaut are supported by an overhead trolley about 150 feet above the center line of the walkway and the support is arranged so that the subject is free to walk, run, jump, and perform other self-locomotive tasks in a more-or-less normal manner, even though he is constrained to move in one place." "The studies thus far show that an astronaut should have no particular difficulty in walking in a pressurized space suit on a hard lunar surface. Rather, the pace was faster and the suit was found to be more comfortable and less fatiguing under lunar "g" than under earth "g." When the test subject wished to travel hurriedly any appreciable distance, a long loping gait at about 10 feet per second was found to be most comfortable." -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, (Washington: NASA, 1995), p. 377; Francis B. Smith, "Simulators For Manned Space Research," Paper for 1966 IEEE International Convention, New York, NY, March 21-25, 1966.

Astronaut Walt Cunningham on the Reduced Gravity Walking Simulator located at the Lunar Landing Facility. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. A.W. Vigil described the purpose of the simulator in his paper "Discussion of Existing and Planned Simulators for Space Research," "When the astronauts land on the moon they will be in an unfamiliar environment involving, particularly, a gravitational field only one-sixth as strong as on earth. A novel method of simulating lunar gravity has been developed and is supported by a puppet-type suspension system at the end of a long pendulum. A floor is provided at the proper angle so that one-sixth of the subject's weight is supported by the floor with the remainder being supported by the suspension system. This simulator allows almost complete freedom in vertical translation and pitch and is considered to be a very realistic simulation of the lunar walking problem. For this problem this simulator suffers only slightly from the restrictions in lateral movement it puts on the test subject. This is not considered a strong disadvantage for ordinary walking problems since most of the motions do, in fact, occur in the vertical plane. However, this simulation technique would be severely restrictive if applied to the study of the extra-vehicular locomotion problem, for example, because in this situation complete six degrees of freedom are rather necessary. This technique, in effect, automatically introduces a two-axis attitude stabilization system into the problem. The technique could, however, be used in preliminary studies of extra-vehicular locomotion where, for example, it might be assumed that one axis of the attitude control system on the astronaut maneuvering unit may have failed." -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, (Washington: NASA, 1995), p. 377; A.W. Vigil, "Discussion of Existing and Planned Simulators for Space Research," Paper presented at Conference on the Role of Simulation in Space Technology," Blacksburg, VA, August 17-21, 1964.

Dr. von Braun inside the KC-135 in flight. The KC-135 provide NASA's Reduced-Gravity Program the unique weightlessness or zero-g environment of space flight for testing and training of human and hardware reactions. The recent version, KC-135A, is a specially modified turbojet transport which flies parabolic arcs to produce weightlessness periods of 20 to 25 seconds and its cargo bay test area is approximately 60 feet long, 10 feet wide, and 7 feet high.

Reduced Gravity Walking Simulator located in the hangar at Langley Research Center. The initial version of this simulator was located inside the hangar. Later a larger version would be located at the Lunar Landing Facility. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. A.W. Vigil wrote in his paper Discussion of Existing and Planned Simulators for Space Research, When the astronauts land on the moon they will be in an unfamiliar environment involving, particularly, a gravitational field only one-sixth as strong as on earth. A novel method of simulating lunar gravity has been developed and is supported by a puppet-type suspension system at the end of a long pendulum. A floor is provided at the proper angle so that one-sixth of the subject' s weight is supported by the floor with the remainder being supported by the suspension system. This simulator allows almost complete freedom in vertical translation and pitch and is considered to be a very realistic simulation of the lunar walking problem. For this problem this simulator suffers only slightly from the restrictions in lateral movement it puts on the test subject. This is not considered a strong disadvantage for ordinary walking problems since most of the motions do, in fact, occur in the vertical plane. However, this simulation technique would be severely restrictive if applied to the study of the extra-vehicular locomotion problem, for example, because in this situation complete six degrees of freedom are rather necessary. This technique, in effect, automatically introduces a two-axis attitude stabilization system into the problem. The technique could, however, be used in preliminary studies of extra-vehicular locomotion where, for example, it might be assumed that one axis of the attitude control system on the astronaut maneuvering unit may have failed. -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, NASA SP-4308, p. 377 A.W. Vigil, Discussion of Existing and Planned Simulators for Space Research, Paper presented at Conference on the Role of Simulation in Space Technology, Blacksburg, VA, August 17-21, 1964.

Experimental study on material flammability and flame spreading in partial gravity aboard the DC-9 aircraft, based at GRC. Pictured in the center is John Yaniec, the DC-9 test director, who is coordinating reduced-gravity maneuver timing between the experimenters and the cockpit and ensuring safe behavior of the research cadre. Pictured on the left is crew member Jerry Auschuetz who is monitoring the experiment. Floating on the right is researcher Kurt Sacksteder.

STS064-10-011 (12 Sept. 1994) --- The Solid Surface Combustion Experiment (SSCE), designed to supply information on flame spread over solid fuel surfaces in the reduced-gravity environment of space, is pictured during flight day four operations. The middeck experiment measured the rate of spreading, the solid-phase temperature, and the gas-phase temperature of flames spreading over rectangular fuel beds. STS-64 marked the seventh trip into space for the Lewis Research Center experiment. Photo credit: NASA or National Aeronautics and Space Administration

jsc2018e009198 (February 21, 2018) --- (From left) 2017 NASA astronaut candidates Bob Hines, Matthew Dominick, Jasmin Moghbeli, and Raja Chari take hold to their surroundings during their reduced gravity flight aboard Canadian Space Agency’s Dassault Falcon 20 Jet. Photo Credit: (NASA/Robert Markowitz)

jsc2018e009222 (February 21, 2018) --- (From left) 2017 NASA astronaut candidates Warren Hoburg, Kayla Barron, Frank Rubio, and Zena Cardman take hold to their surroundings during their reduced gravity flight aboard Canadian Space Agency’s Dassault Falcon 20 Jet. Photo Credit: (NASA/Robert Markowitz)

jsc2018e009094 (February 21, 2018) --- 2017 NASA astronaut candidates Warren Hoburg, Zena Cardman, Frank Rubio, and Kayla Barron latch on to each other during a reduced gravity flight aboard Canadian Space Agency’s Dassault Falcon 20 Jet. Photo Credit: (NASA/Robert Markowitz)

Lunar Landing Walking Simulator: Researchers at Langley study the ability of astronauts to walk, run and perform other tasks required during lunar exploration. The Reduced Gravity Simulator gave researchers the opportunity to look at the effects of one-sixth normal gravity on self-locomotion. Several Apollo astronauts practiced lunar waling at the facility.

Astronaut Roger Chaffee on the Reduced Gravity Walking Simulator located at the Lunar Landing Facility. The purpose of this simulator was to study the subject while walking, jumping or running. Researchers conducted studies of various factors such as fatigue limit, energy expenditure, and speed of locomotion. A.W. Vigil, described the simulator as follows: "When the astronauts land on the moon they will be in an unfamiliar environment involving, particularly, a gravitational field only one-sixth as strong as on earth. A novel method of simulating lunar gravity has been developed and is supported by a puppet-type suspension system at the end of a long pendulum. A floor is provided at the proper angle so that one-sixth of the subject's weight is supported by the floor with the remainder being supported by the suspension system. This simulator allows almost complete freedom in vertical translation and pitch and is considered to be a very realistic simulation of the lunar walking problem. For this problem this simulator suffers only slightly from the restrictions in lateral movement it puts on the test subject. This is not considered a strong disadvantage for ordinary walking problems since most of the motions do, in fact, occur in the vertical plane. However, this simulation technique would be severely restrictive if applied to the study of the extra-vehicular locomotion problem, for example, because in this situation complete six degrees of freedom are rather necessary. This technique, in effect, automatically introduces a two-axis attitude stabilization system into the problem. The technique could, however, be used in preliminary studies of extra-vehicular locomotion where, for example, it might be assumed that one axis of the attitude control system on the astronaut maneuvering unit may have failed." -- Published in James R. Hansen, Spaceflight Revolution: NASA Langley Research Center From Sputnik to Apollo, NASA SP-4308, p. 377; A.W. Vigil, "Discussion of Existing and Planned Simulators for Space Research," Paper presented at Conference on the Role of Simulation in Space Technology," Blacksburg, VA, August 17-21, 1964.

CAPE CANAVERAL, Fla. – Experiments are placed inside the FASTRACK Space Experiment Platform viewed in the Life Science Building at NASA's Kennedy Space Center. The space experiment rack is under development for flight aboard NASA's first commercially-provided research flights on Zero Gravity Corporation's reduced gravity aircraft. It is being developed jointly by Kennedy and Space Florida to facilitate NASA and commercial use of reusable U.S. suborbital flight vehicles currently under development. FASTRACK will enable investigators to test experiments, apparatus and analytical techniques in hardware compatible with the International Space Station, and to perform science that can be carried out during the reduced gravity available for brief periods during aircraft parabolas. Flight testing of the FASTRACK will be performed on four consecutive days between September 9-12 from Ellington Field near NASA's Johnson Space Center, Houston. Photo credit: NASA/Troy Cryder

CAPE CANAVERAL, Fla. – Experiments are placed inside the FASTRACK Space Experiment Platform viewed in the Life Science Building at NASA's Kennedy Space Center. The space experiment rack is under development for flight aboard NASA's first commercially-provided research flights on Zero Gravity Corporation's reduced gravity aircraft. It is being developed jointly by Kennedy and Space Florida to facilitate NASA and commercial use of reusable U.S. suborbital flight vehicles currently under development. FASTRACK will enable investigators to test experiments, apparatus and analytical techniques in hardware compatible with the International Space Station, and to perform science that can be carried out during the reduced gravity available for brief periods during aircraft parabolas. Flight testing of the FASTRACK will be performed on four consecutive days between September 9-12 from Ellington Field near NASA's Johnson Space Center, Houston. Photo credit: NASA/Troy Cryder

iss064e049400 (3/31/2021) --- A view of the Plant Water Management 3 and 4 investigation aboard the International space Station (ISS). The Plant Water Management 3 and 4 investigation demonstrates passive measures for controlling fluid delivery and uptake in plant growth systems. Reduced gravity creates challenges in providing adequate fluid and nutrition for plant growth. This investigation examines using other physical properties such as surface tension, wetting and system geometry to replace the role of gravity.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

iss064e049289 (3/30/2021) --- A view of the Plant Water Management 3 and 4 investigation aboard the International space Station (ISS). The Plant Water Management 3 and 4 investigation demonstrates passive measures for controlling fluid delivery and uptake in plant growth systems. Reduced gravity creates challenges in providing adequate fluid and nutrition for plant growth. This investigation examines using other physical properties such as surface tension, wetting and system geometry to replace the role of gravity.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

iss064e049484 (3/31/2021) --- A view of the Plant Water Management 3 and 4 investigation aboard the International space Station (ISS). The Plant Water Management 3 and 4 investigation demonstrates passive measures for controlling fluid delivery and uptake in plant growth systems. Reduced gravity creates challenges in providing adequate fluid and nutrition for plant growth. This investigation examines using other physical properties such as surface tension, wetting and system geometry to replace the role of gravity.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Astronaut Rex Walheim uses the Active Response Gravity Offload System (ARGOS) to perform early evaluations of the Orion Crew Survival System (OCSS) suit in Building 9 of Johnson Space Center in Houston on June 5, 2012. ARGOS is designed to simulate reduced gravity environments, such as lunar, Martian, or microgravity, using a system similar to an overhead bridge crane. Part of Batch image transfer from Flickr.

Ted Brunzie and Peter Mason observe the float package and the data rack aboard the DC-9 reduced gravity aircraft. The float package contains a cryostat, a video camera, a pump and accelerometers. The data rack displays and record the video signal from the float package on tape and stores acceleration and temperature measurements on disk.

STS063-29-002 (3-11 Feb. 1995) --- On the Space Shuttle Discovery's middeck, astronaut C. Michael Foale, mission specialist, checks on the Solid Surface Combustion Experiment (SSCE). Foale was joined by four other NASA astronauts James D. Wetherbee, commander; Eileen M. Collins, pilot; Bernard A. Harris, Jr., payload commander; Janice E. Voss, mission specialist, and a Russian cosmonaut, Vladimir G. Titov; for eight days of research in Earth-orbit.

With the lights out, the ISRU Pilot Excavator digs in regolith bin during testing inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

With the lights out, the ISRU Pilot Excavator digs in regolith bin during testing inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

The ISRU Pilot Excavator digs in the regolith bin during testing inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

With the lights out, the ISRU Pilot Excavator digs in the regolith bin during testing inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

The ISRU Pilot Excavator digs its way through the regolith bin during testing inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

The ISRU Pilot Excavator digs in the regolith bin during testing inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab operates a test of the ISRU Pilot Excavator in regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

AJ Nick, a robotic engineer with the Granular Mechanics and Regolith Operations Lab, monitors the Regolith Advanced Surface Systems Operations Robot (RASSOR) from a control room during testing in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

With the lights out, the ISRU Pilot Excavator digs in regolith bin during testing inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

A team from the Granular Mechanics and Regolith Operations Lab tests the Regolith Advanced Surface Systems Operations Robot (RASSOR) in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

The ISRU Pilot Excavator is tested in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on July 28, 2022. Tests use a gravity assist offload system to simulate reduced gravity conditions found on the Moon. On the surface of the Moon, mining robots like the Pilot Excavator will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. The Pilot Excavator can scoop up icy regolith which can be used to make operations on the Moon sustainable.

CAPE CANAVERAL, Fla. – In the Life Science Building at NASA's Kennedy Space Center, a space experiment rack is under development for flight aboard NASA's first commercially-provided research flights on Zero Gravity Corporation's reduced gravity aircraft. Known as the FASTRACK Space Experiment Platform, the rack is designed to support two standard lockers that fit inside the space shuttle's crew middeck. It is being developed jointly by Kennedy and Space Florida to facilitate NASA and commercial use of reusable U.S. suborbital flight vehicles currently under development. FASTRACK will enable investigators to test experiments, apparatus and analytical techniques in hardware compatible with the International Space Station, and to perform science that can be carried out during the reduced gravity available for brief periods during aircraft parabolas. Flight testing of the FASTRACK will be performed on four consecutive days between September 9-12 from Ellington Field near NASA's Johnson Space Center, Houston. Photo credit: NASA/Troy Cryder

CAPE CANAVERAL, Fla. – In the Life Science Building at NASA's Kennedy Space Center, this space experiment rack is under development for flight aboard NASA's first commercially-provided research flights on Zero Gravity Corporation's reduced gravity aircraft. Known as the FASTRACK Space Experiment Platform, the rack is designed to support two standard lockers that fit inside the space shuttle's crew middeck. It is being developed jointly by Kennedy and Space Florida to facilitate NASA and commercial use of reusable U.S. suborbital flight vehicles currently under development. FASTRACK will enable investigators to test experiments, apparatus and analytical techniques in hardware compatible with the International Space Station, and to perform science that can be carried out during the reduced gravity available for brief periods during aircraft parabolas. Flight testing of the FASTRACK will be performed on four consecutive days between September 9-12 from Ellington Field near NASA's Johnson Space Center, Houston. Photo credit: NASA/Troy Cryder

Group photo representating past and present Multi-Media Services (MMS) photographer and videographers that have supported Zero-G Reduced Gravity Office operations throughout the year prior to the programs final flight on August 29, 2014. Photo Date: August 18, 2014. Location: Ellington Field - Hangar 990. Photographer: Robert Markowitz

jsc2022e072967 (4/12/2021) --- Image of bovine ovary Granulosa cells. Coordinated by the Italian Space Agency (ASI), OVOSPACE investigates how microgravity influences the maturation and development ovarian cells in mammals, including Granulosa cells. This experiment could help scientists understand how long-term settlement on the Moon or Mars might affect the fertility of astronauts living in reduced gravity for long durations. Image courtesy of Professor Mariano Bizzarri, Department of Experimental Medicine, Sapienza University of Rome.

jsc2024e043917 (7/10/2024) --- Packed Bed Reactor Experiment-Water Recovery (PBRE-WR) examines flow rates of gas and liquid through a filtering substrate in the space station water processor, replacing oxygen with nitrogen. This preflight image shows the PBRE-WR test section with alumina packed bed material loaded. Scientists aim to learn more about how reduced gravity affects the performance and reliability of various filtration systems

The first United States Microgravity Laboratory (USML-1) flew in orbit inside the Spacelab science module for extended periods, providing scientists and researchers greater opportunities for research in materials science, fluid dynamics, biotechnology (crystal growth), and combustion science. In this photograph, Astronaut Bornie Dunbar and Astronaut Larry DeLucas are conducting the Lower Body Negative Pressure (LBNP) experiment, which is to protect the health and safety of the crew and to shorten the time required to readapt to gravity when they return to Earth. When humans go into space, the lack of gravity causes many changes in the body. One change is that fluids normally kept in the lower body by gravity, shift upward to the head and chest. This is why astronauts' faces appear chubby or puffy. The change in fluid volume also affects the heart. The reduced fluid volume means that there is less blood to circulate through the body. Crewmembers may experience reduced blood flow to the brain when returning to Earth. This leads to fainting or near-fainting episodes. With the use of LBNP to simulate the pull of gravity in conjunction with fluids, salt tablets can recondition the cardiovascular system. This treatment, called "soak," is effective up to 24 hours. The LBNP uses a three-layer collapsible cylinder that seals around the crewmember's waist which simulates the effects of gravity and helps pull fluids into the lower body. The data collected will be analyzed to determine physiological changes in the crewmembers and effectiveness of the treatment. The USML-1 was launched aboard the Space Shuttle Orbiter Columbia (STS-50) on June 25, 1992.

The stimulus of gravity affects RNA production, which helps maintain the strength of human muscles on Earth (top), as seen in this section of muscle fiber taken from an astronaut before spaceflight. Astronauts in orbit and patients on Earth fighting muscle-wasting diseases need countermeasures to prevent muscle atrophy, indicated here with white lipid droplets (bottom) in the muscle sample taken from the same astronaut after spaceflight. Kerneth Baldwin of the University of California, Irvine, is conducting research on how reducing the stimulus of gravity affects production of the RNA that the body uses as a blueprint for making muscle proteins. Muscle proteins are what give muscles their strength, so when the RNA blueprints aren't available for producing new proteins to replace old ones -- a situation that occurs in microgravity -- the muscles atrophy. When the skeletal muscle system is exposed to microgravity during spaceflight, the muscles undergo a reduced mass that translates to a reduction in strength. When this happens, muscle endurance decreases and the muscles are more prone to injury, so individuals could have problems in performing extravehicular activity [space walks] or emergency egress because their bodies are functionally compromised.

Drew Smith, a robotics engineer, makes adjustments to the Regolith Advanced Surface Systems Operations Robot (RASSOR) during testing in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Smith and other members of the Granular Mechanics and Regolith Operations Lab run tests, which simulates the Moon’s reduced gravity using the gravity assist offload system to see how RASSOR excavates regolith. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

Drew Smith, a robotics engineer, makes adjustments to the Regolith Advanced Surface Systems Operations Robot (RASSOR) during testing in the regolith bin inside Swamp Works at NASA’s Kennedy Space Center in Florida on June 5, 2019. Smith and other members of the Granular Mechanics and Regolith Operations Lab run tests, which simulates the Moon’s reduced gravity using the gravity assist offload system to see how RASSOR excavates regolith. On the surface of the Moon, mining robots like RASSOR will excavate the regolith and take the material to a processing plant where usable elements such as hydrogen, oxygen and water can be extracted for life support systems. RASSOR can scoop up icy regolith which can be used to make operations on the Moon sustainable.

S73-32113 (9 Aug. 1973) --- Scientist-astronaut Owen K. Garriott, Skylab 3 science pilot, serves as test subject for the Skylab ?Human Vestibular Function? M131 Experiment, as seen in this photographic reproduction taken from a television transmission made by a color TV camera aboard the Skylab space station in Earth orbit. The objectives of the Skylab M131 experiment are to obtain data pertinent to establishing the validity of measurements of specific behavioral/physiological responses influenced by vestibular activity under one-g and zero-g conditions; to determine man?s adaptability to unusual vestibular conditions and predict habitability of future spacecraft conditions involving reduced gravity and Coriollis forces; and to measure the accuracy and variability in man?s judgment of spatial coordinates based on atypical gravity receptor cues and inadequate visual cues. Photo credit: NASA

Astronaut Chiaki Mukai conducts the Lower Body Negative Pressure (LBNP) experiment inside the International Microgravity Laboratory-2 (IML-2) mission science module. Dr. Chiaki Mukai is one of the National Space Development Agency of Japan (NASDA) astronauts chosen by NASA as a payload specialist (PS). She was the second NASDA PS who flew aboard the Space Shuttle, and was the first female astronaut in Asia. When humans go into space, the lack of gravity causes many changes in the body. One change is that fluids normally kept in the lower body by gravity shift upward to the head and chest. This is why astronauts' faces appear chubby or puffy. The change in fluid volume also affects the heart. The reduced fluid volume means that there is less blood to circulate through the body. Crewmembers may experience reduced blood flow to the brain when returning to Earth. This leads to fainting or near-fainting episodes. With the use of the LBNP to simulate the pull of gravity in conjunction with fluids, salt tablets can recondition the cardiovascular system. This treatment, called "soak," is effective up to 24 hours. The LBNP uses a three-layer collapsible cylinder that seals around the crewmember's waist which simulates the effects of gravity and helps pull fluids into the lower body. The data collected will be analyzed to determine physiological changes in the crewmembers and effectiveness of the treatment. The IML-2 was the second in a series of Spacelab flights designed by the international science community to conduct research in a microgravity environment Managed by the Marshall Space Flight Center, the IML-2 was launched on July 8, 1994 aboard the STS-65 Space Shuttle Orbiter Columbia mission.

STS073-101-018 (20 October-5 November 1995) --- Payload specialist Fred W. Leslie maneuvers his body to a position conducive to research at the Crystal Growth Furnace (CGF) aboard the science module in the cargo bay of the Earth-orbiting Space Shuttle Columbia. Crystallization has been discovered to be more effectively studied in the weightless environment of space than on Earth, because the gravity-induced phenomena that obscure or change the process or change the process are greatly reduced or eliminated. Leslie was joined by a second guest researcher and five NASA astronauts for 16 full days of in-space research in support of the United States Microgravity Laboratory (USML-2) mission.

jsc2024e043916 (3/29/2024) ---The Packed Bed Reactor Experiment – Water Recovery (PBRE-WR) completed a series of tests in the Microgravity Science Glovebox on the International Space Station. Image of PBRE-WR during low flow conditions. Bubbles and voids (darker spots) are captured using a high-speed video camera at 10 fps. They are measured to determine gas holdup during various test conditions. In this image, the liquid flow was 20 kg/hr and the gas flow was 100 gr/hr. Scientists aim to learn more about how reduced gravity affects the performance and reliability of various filtration systems.

iss055e005543 (March 26, 2018) --- Expedition 55 Flight Engineer and astronaut Scott Tingle is pictured conducting the Transparent Alloys experiment inside the Destiny lab module's Microgravity Science Glovebox. The Transparent Alloys study is a set of five experiments that seeks to improve the understanding of melting-solidification processes in plastics without the interference of Earth's gravity environment. Results may impact the development of new light-weight, high-performance structural materials for space applications. Observations may also impact fuel efficiency, consumption and recycling of materials on Earth potentially reducing costs and increasing industrial competitiveness.

S73-34171 (9 Aug. 1973) --- Scientist-astronaut Owen K. Garriott, Skylab 3 science pilot, serves as test subject for the Skylab ?Human Vestibular Function? M131 Experiment, as seen in this photographic reproduction taken from a television transmission made by a color TV camera aboard the Skylab space station in Earth orbit. The objectives of the Skylab M131 experiment are to obtain data pertinent to establishing the validity of measurements of specific behavioral/physiological responses influenced by vestibular activity under one-g and zero-g conditions; to determine man?s adaptability to unusual vestibular conditions and predict habitability of future spacecraft conditions involving reduced gravity and Coriollis forces; and to measure the accuracy and variability in man?s judgment of spatial coordinates based on atypical gravity receptor cues and inadequate visual cures. Dr. Garriott is seated in the experiment?s litter chair which can rotate the test subject at predetermined rotational velocity or programmed acceleration/decelerational profile. Photo credit: NASA

Engineers at NASA's Jet Propulsion Laboratory – from left, Matthew Cameron-Hooper, and Thomas Reynoso – prepare flight-like landing gear in the Europa Lander landing gear testbed in summer 2022. Europa Lander is a concept for a potential future mission that would look for signs of life in the icy surface material of Jupiter's moon Europa. The moon is thought to contain a global ocean of salty water beneath its frozen crust. If life exists in that ocean, signs of its existence called biosignatures could potentially find their way to the surface. In this mission concept, a spacecraft would land on Europa and collect and study samples from about 4 inches (10 centimeters) beneath the surface, looking for signs of life. The Europa Lander landing gear testbed was developed to test and inform the design of the landing gear for the spacecraft: It mimics the landing loads and ground interaction forces that a single flight landing gear would experience when touching down on the Europan surface. It does this by using gravity offloading to simulate the reduced gravity on Europa, and by replicating the mass and inertial properties of a flight lander as well as all the degrees of freedom that the landing gear would experience. https://photojournal.jpl.nasa.gov/catalog/PIA26198

Engineers test the mechanical landing system for the proposed Europa Lander project at NASA's Jet Propulsion Laboratory on Sept. 15, 2022. This test, using the Europa Lander landing gear testbed, fully exercises the Europa Lander landing gear mechanism through a simulated dynamic landing. Europa Lander is a concept for a potential future mission that would look for signs of life in the icy surface material of Jupiter's moon Europa. The moon is thought to contain a global ocean of salty water beneath its frozen crust. If life exists in that ocean, signs of its existence called biosignatures could potentially find their way to the surface. In this mission concept, a spacecraft would land on Europa and collect and study samples from about 4 inches (10 centimeters) beneath the surface, looking for signs of life. The Europa Lander landing gear testbed was developed to test and inform the design of the landing gear for the spacecraft: It mimics the landing loads and ground interaction forces that a single flight landing gear would experience when touching down on the Europan surface. It does this by using gravity offloading to simulate the reduced gravity on Europa, and by replicating the mass and inertial properties of a flight lander as well as all the degrees of freedom that the landing gear would experience. Video available at https://photojournal.jpl.nasa.gov/catalog/PIA26199

CAPE CANAVERAL, Fla. – Technicians in the Life Science Building at NASA's Kennedy Space Center work on the FASTRACK Space Experiment Platform. The rack is designed to support two standard lockers that fit inside the space shuttle's crew middeck. It is being developed jointly by Kennedy and Space Florida to facilitate NASA and commercial use of reusable U.S. suborbital flight vehicles currently under development. FASTRACK will enable investigators to test experiments, apparatus and analytical techniques in hardware compatible with the International Space Station, and to perform science that can be carried out during the reduced gravity available for brief periods during aircraft parabolas. Flight testing of the FASTRACK will be performed on four consecutive days between September 9-12 from Ellington Field near NASA's Johnson Space Center, Houston. Photo credit: NASA/Troy Cryder

CAPE CANAVERAL, Fla. – Technicians in the Life Science Building at NASA's Kennedy Space Center work on the FASTRACK Space Experiment Platform. The rack is designed to support two standard lockers that fit inside the space shuttle's crew middeck. It is being developed jointly by Kennedy and Space Florida to facilitate NASA and commercial use of reusable U.S. suborbital flight vehicles currently under development. FASTRACK will enable investigators to test experiments, apparatus and analytical techniques in hardware compatible with the International Space Station, and to perform science that can be carried out during the reduced gravity available for brief periods during aircraft parabolas. Flight testing of the FASTRACK will be performed on four consecutive days between September 9-12 from Ellington Field near NASA's Johnson Space Center, Houston. Photo credit: NASA/Troy Cryder

CAPE CANAVERAL, Fla. – Several Lead Zirconate Titanate, or PZT, mass gaging sensors have been attached to a composite tank during a test inside a laboratory at the Cryogenics Testbed Facility at NASA's Kennedy Space Center in Florida. The PZT-based system was developed at Kennedy as a way to measure the mass of a fluid and the structural health of a tank using vibration signatures on Earth or in reduced/zero g gravity. The mass gaging technology has received approval to be on the first sub-orbital flight on the Virgin Galactic Space Plane in 2015. NASA experiments using the PZT technology will be used by Embry-Riddle Aeronautical University in conjunction with Carthage College on a fluid transfer experiment. Photo credit: NASA/Daniel Casper

CAPE CANAVERAL, Fla. – Rudy Werlink, a fluid systems engineer in the Engineering Directorate at NASA's Kennedy Space Center in Florida, monitors a test in a lab at the Cryogenics Testbed Facility using the Lead Zirconate Titanate, or PZT-based system that he developed. Werlink developed the PZT-based system at Kennedy as a way to measure the mass of a fluid and the structural health of a tank using vibration signatures on Earth or in reduced/zero g gravity. The mass gaging technology has received approval to be on the first sub-orbital flight on the Virgin Galactic Space Plane in 2015. NASA experiments using the PZT technology will be used by Embry-Riddle Aeronautical University in conjunction with Carthage College on a fluid transfer experiment. Photo credit: NASA/Daniel Casper

The Fluids and Combustion Facility (FCF) is a modular, multi-user facility to accommodate microgravity science experiments on board Destiny, the U.S. Laboratory Module for the International Space Station (ISS). The FCF will be a permanet facility aboard the ISS, and will be capable of accommodating up to ten science investigations per year. It will support the NASA Science and Technology Research Plans for the International Space Station (ISS) which require sustained systematic research of the effects of reduced gravity in the areas of fluid physics and combustion science. From left to right are the Combustion Integrated Rack, the Shared Rack, and the Fluids Integrated Rack. The FCF is being developed by the Microgravity Science Division (MSD) at the NASA Glenn Research Center. (Photo Credit: NASA/Marshall Space Flight Center)

Don Sirois, an Auburn University research associate, and Bruce Strom, a mechanical engineering Co-Op Student, are evaluating the dimensional characteristics of an aluminum automobile engine casting. More accurate metal casting processes may reduce the weight of some cast metal products used in automobiles, such as engines. Research in low gravity has taken an important first step toward making metal products used in homes, automobiles, and aircraft less expensive, safer, and more durable. Auburn University and industry are partnering with NASA to develop one of the first accurate computer model predictions of molten metals and molding materials used in a manufacturing process called casting. Ford Motor Company's casting plant in Cleveland, Ohio is using NASA-sponsored computer modeling information to improve the casting process of automobile and light-truck engine blocks.

Researchers have found that as melted metals and alloys (combinations of metals) solidify, they can form with different arrangements of atoms, called microstructures. These microstructures depend on the shape of the interface (boundary) between the melted metal and the solid crystal it is forming. There are generally three shapes that the interface can take: planar, or flat; cellular, which looks like the cells of a beehive; and dendritic, which resembles tiny fir trees. Convection at this interface can affect the interface shape and hide the other phenomena (physical events). To reduce the effects of convection, researchers conduct experiments that examine and control conditions at the interface in microgravity. Microgravity also helps in the study of alloys composed of two metals that do not mix. On Earth, the liquid mixtures of these alloys settle into different layers due to gravity. In microgravity, the liquid metals do not settle, and a solid more uniform mixture of both metals can be formed.

CAPE CANAVERAL, Fla. – A technician in the Life Science Building at NASA's Kennedy Space Center works on the FASTRACK Space Experiment Platform. The rack is designed to support two standard lockers that fit inside the space shuttle's crew middeck. It is being developed jointly by Kennedy and Space Florida to facilitate NASA and commercial use of reusable U.S. suborbital flight vehicles currently under development. FASTRACK will enable investigators to test experiments, apparatus and analytical techniques in hardware compatible with the International Space Station, and to perform science that can be carried out during the reduced gravity available for brief periods during aircraft parabolas. Flight testing of the FASTRACK will be performed on four consecutive days between September 9-12 from Ellington Field near NASA's Johnson Space Center, Houston. Photo credit: NASA/Troy Cryder

CAPE CANAVERAL, Fla. – Several Lead Zirconate Titanate, or PZT, mass gaging sensors have been attached to a composite tank during a test inside a laboratory at the Cryogenics Testbed Facility at NASA's Kennedy Space Center in Florida. The PZT-based system was developed at Kennedy as a way to measure the mass of a fluid and the structural health of a tank using vibration signatures on Earth or in reduced/zero g gravity. The mass gaging technology has received approval to be on the first sub-orbital flight on the Virgin Galactic Space Plane in 2015. NASA experiments using the PZT technology will be used by Embry-Riddle Aeronautical University in conjunction with Carthage College on a fluid transfer experiment. Photo credit: NASA/Daniel Casper

Researchers have found that as melted metals and alloys (combinations of metals) solidify, they can form with different arrangements of atoms, called microstructures. These microstructures depend on the shape of the interface (boundary) between the melted metal and the solid crystal it is forming. There are generally three shapes that the interface can take: planar, or flat; cellular, which looks like the cells of a beehive; and dendritic, which resembles tiny fir trees. Convection at this interface can affect the interface shape and hide the other phenomena (physical events). To reduce the effects of convection, researchers conduct experiments that examine and control conditions at the interface in microgravity. Microgravity also helps in the study of alloys composed of two metals that do not mix. On Earth, the liquid mixtures of these alloys settle into different layers due to gravity. In microgravity, the liquid metals do not settle, and a solid more uniform mixture of both metals can be formed.

Engineer Matthew Cameron-Hooper performs a checkout on some systems of the Europa Lander landing gear testbed at NASA's Jet Propulsion Laboratory in Southern California on May 27, 2022. Europa Lander is a concept for a potential future mission that would look for signs of life in the icy surface material of Jupiter's moon Europa. The moon is thought to contain a global ocean of salty water beneath its frozen crust. If life exists in that ocean, signs of its existence called biosignatures could potentially find their way to the surface. In this mission concept, a spacecraft would land on Europa and collect and study samples from about 4 inches (10 centimeters) beneath the surface, looking for signs of life. The Europa Lander landing gear testbed was developed to test and inform the design of the landing gear for the spacecraft: It mimics the landing loads and ground interaction forces that a single flight landing gear would experience when touching down on the Europan surface. It does this by using gravity offloading to simulate the reduced gravity on Europa, and by replicating the mass and inertial properties of a flight lander as well as all the degrees of freedom that the landing gear would experience. This system checkout confirmed two critical functionalities of the testbed: low friction of the horizontal degree of freedom that carries the test landing gear, and proper functioning of the gravity offloading system. Together these functionalities ensure that only ground interaction forces cause the test landing gear to come to a stop during a test, just as a flight landing gear would experience when landing on the Europan surface. Video available at https://photojournal.jpl.nasa.gov/catalog/PIA26200

This illustration is an artist’s concept of a Magnetic Launch Assist System, formerly referred as the Magnetic Levitation (Maglev) system, for space launch. Overcoming the grip of Earth’s gravity is a supreme challenge for engineers who design rockets that leave the planet. Engineers at the Marshall Space Flight Center have developed and tested Magnetic Launch Assist System technologies that could levitate and accelerate a launch vehicle along a track at high speeds before it leaves the ground. Using electricity and magnetic fields, a Magnetic Launch Assist system would drive a spacecraft along a horizontal track until it reaches desired speeds. A full-scale, operational track would be about 1.5-miles long and capable of accelerating a vehicle to 600 mph in 9.5 seconds. The major advantages of launch assist for NASA launch vehicles is that it reduces the weight of the take-off, landing gear and the wing size, as well as the elimination of propellant weight resulting in significant cost savings. The US Navy and the British MOD (Ministry of Defense) are planning to use magnetic launch assist for their next generation aircraft carriers as the aircraft launch system. The US Army is considering using this technology for launching target drones for anti-aircraft training.

A rectangular drop test vehicle perched above 450-foot shaft at the Zero Gravity Research Facility at NASA Lewis Research Center. The drop tower was designed to provide five seconds of microgravity during a normal drop, but had a pneumatic gun that could quickly propel the vehicle to the top of the shaft prior to its drop, thus providing ten seconds of microgravity. The shaft contained a steel-lined vacuum chamber 20 feet in diameter and 469 feet deep. The package was stopped at the bottom of the pit by a 15-foot deep deceleration cart filled with polystyrene pellets. During normal operations, a cylindrical 3-foot diameter and 11-foot long vehicle was used to house the experiments, instrumentation, and high speed cameras. The 4.5-foot long and 1.5-foot wide rectangular vehicle, seen in this photograph, was used less frequently. A 3-foot diameter orb was used for the ten second drops. After the test vehicle was prepared it was suspended above the shaft from the top of the chamber. A lid was used to seal the top of the chamber. The vacuum system reduced the pressure levels inside the chamber. The bolt holding the vehicle was then sheared and the vehicle plummeted into the deceleration cart.

This photo of the X-1A includes graphs of the flight data from Maj. Charles E. Yeager's Mach 2.44 flight on December 12, 1953. (This was only a few days short of the 50th anniversary of the Wright brothers' first powered flight.) After reaching Mach 2.44, then the highest speed ever reached by a piloted aircraft, the X-1A tumbled completely out of control. The motions were so violent that Yeager cracked the plastic canopy with his helmet. He finally recovered from a inverted spin and landed on Rogers Dry Lakebed. Among the data shown are Mach number and altitude (the two top graphs). The speed and altitude changes due to the tumble are visible as jagged lines. The third graph from the bottom shows the G-forces on the airplane. During the tumble, these twice reached 8 Gs or 8 times the normal pull of gravity at sea level. (At these G forces, a 200-pound human would, in effect, weigh 1,600 pounds if a scale were placed under him in the direction of the force vector.) Producing these graphs was a slow, difficult process. The raw data from on-board instrumentation recorded on oscillograph film. Human computers then reduced the data and recorded it on data sheets, correcting for such factors as temperature and instrument errors. They used adding machines or slide rules for their calculations, pocket calculators being 20 years in the future.

An inflight view from the left side of the Lunar Landing Research Vehicle, is shown in this 1964 NASA Flight Research Center photograph. The photograph was taken in front of the old NACA hangar located at the South Base, Edwards Air Force Base. When Apollo planning was underway in 1960, NASA was looking for a simulator to profile the descent to the Moon's surface. Three concepts surfaced: an electronic simulator, a tethered device, and the ambitious Dryden contribution, a free-flying vehicle. All three became serious projects, but eventually the NASA Flight Research Center's (FRC) Landing Research Vehicle (LLRV) became the most significant one. Hubert M. Drake is credited with originating the idea, while Donald Bellman and Gene Matranga were senior engineers on the project, with Bellman, the project manager. Simultaneously, and independently, Bell Aerosystems Company, Buffalo, N.Y., a company with experience in vertical takeoff and landing (VTOL) aircraft, had conceived a similar free-flying simulator and proposed their concept to NASA headquarters. NASA Headquarters put FRC and Bell together to collaborate. The challenge was; to allow a pilot to make a vertical landing on earth in a simulated Moon environment, one sixth of the earth's gravity and with totally transparent aerodynamic forces in a "free flight" vehicle with no tether forces acting on it. Built of tubular aluminum like a giant four-legged bedstead, the vehicle was to simulate a lunar landing profile from around 1500 feet to the Moon's surface. To do this, the LLRV had a General Electric CF-700-2V turbofan engine mounted vertically in gimbals, with 4200 pounds of thrust. The engine, using JP-4 fuel, got the vehicle up to the test altitude and was then throttled back to support five-sixths of the vehicle's weight, simulating the reduced gravity of the Moon. Two hydrogen-peroxide lift rockets with thrust that could be varied from 100 to 500 pounds handled the LLRV's rate of descent and horizontal transla

In this 1965 NASA Flight Reserch Center photograph the Lunar Landing Research Vehicle (LLRV) is shown at near maximum altitude over the south base at Edwards Air Force Base. When Apollo planning was underway in 1960, NASA was looking for a simulator to profile the descent to the moon's surface. Three concepts surfaced: an electronic simulator, a tethered device, and the ambitious Dryden contribution, a free-flying vehicle. All three became serious projects, but eventually the NASA Flight Research Center's (FRC) Landing Research Vehicle (LLRV) became the most significant one. Hubert M. Drake is credited with originating the idea, while Donald Bellman and Gene Matranga were senior engineers on the project, with Bellman, the project manager. Simultaneously, and independently, Bell Aerosystems Company, Buffalo, N.Y., a company with experience in vertical takeoff and landing (VTOL) aircraft, had conceived a similar free-flying simulator and proposed their concept to NASA headquarters. NASA Headquarters put FRC and Bell together to collaborate. The challenge was; to allow a pilot to make a vertical landing on Earth in a simulated moon environment, one sixth of the Earth's gravity and with totally transparent aerodynamic forces in a "free flight" vehicle with no tether forces acting on it. Built of tubular aluminum like a giant four-legged bedstead, the vehicle was to simulate a lunar landing profile from around 1500 feet to the moon's surface. To do this, the LLRV had a General Electric CF-700-2V turbofan engine mounted vertically in gimbals, with 4200 pounds of thrust. The engine, using JP-4 fuel, got the vehicle up to the test altitude and was then throttled back to support five-sixths of the vehicle's weight, simulating the reduced gravity of the moon. Two hydrogen-peroxide lift rockets with thrust that could be varied from 100 to 500 pounds handled the LLRV's rate of descent and horizontal translations. Sixteen smaller hydrogen-peroxide rockets, mounted in pairs, gav

This 1964 NASA Flight Reserch Center photograph shows a ground engine test underway on the Lunar Landing Research Vehicle (LLRV) number 1. When Apollo planning was underway in 1960, NASA was looking for a simulator to profile the descent to the Moon's surface. Three concepts surfaced: an electronic simulator, a tethered device, and the ambitious Dryden contribution, a free-flying vehicle. All three became serious projects, but eventually the NASA Flight Research Center's (FRC) Landing Research Vehicle (LLRV) became the most significant one. Hubert M. Drake is credited with originating the idea, while Donald Bellman and Gene Matranga were senior engineers on the project, with Bellman, the project manager. Simultaneously, and independently, Bell Aerosystems Company, Buffalo, N.Y., a company with experience in vertical takeoff and landing (VTOL) aircraft, had conceived a similar free-flying simulator and proposed their concept to NASA headquarters. NASA Headquarters put FRC and Bell together to collaborate. The challenge was; to allow a pilot to make a vertical landing on Earth in a simulated Moon environment, one sixth of the Earth's gravity and with totally transparent aerodynamic forces in a "free flight" vehicle with no tether forces acting on it. Built of tubular aluminum like a giant four-legged bedstead, the vehicle was to simulate a lunar landing profile from around 1500 feet to the Moon's surface. To do this, the LLRV had a General Electric CF-700-2V turbofan engine mounted vertically in gimbals, with 4200 pounds of thrust. The engine, using JP-4 fuel, got the vehicle up to the test altitude and was then throttled back to support five-sixths of the vehicle's weight, simulating the reduced gravity of the Moon. Two hydrogen-peroxide lift rockets with thrust that could be varied from 100 to 500 pounds handled the LLRV's rate of descent and horizontal translations. Sixteen smaller hydrogen-peroxide rockets, mounted in pairs, gave the pilot control in pitch, yaw,

A group photo of the LLRV personnel following the program's 100th flight. The photo was taken at South Base, and was near the hangar first used by the original NACA group, at what was then called Muroc. When Apollo planning was underway in 1960, NASA was looking for a simulator to profile the descent to the moon's surface. Three concepts surfaced: an electronic simulator, a tethered device, and the ambitious Dryden contribution, a free-flying vehicle. All three became serious projects, but eventually the NASA Flight Research Center's (FRC) Landing Research Vehicle (LLRV) became the most significant one. Hubert M. Drake is credited with originating the idea, while Donald Bellman and Gene Matranga were senior engineers on the project, with Bellman, the project manager. Simultaneously, and independently, Bell Aerosystems Company, Buffalo, N.Y., a company with experience in vertical takeoff and landing (VTOL) aircraft, had conceived a similar free-flying simulator and proposed their concept to NASA headquarters. NASA Headquarters put FRC and Bell together to collaborate. The challenge was; to allow a pilot to make a vertical landing on Earth in a simulated moon environment, one sixth of the Earth's gravity and with totally transparent aerodynamic forces in a "free flight" vehicle with no tether forces acting on it. Built of tubular aluminum like a giant four-legged bedstead, the vehicle was to simulate a lunar landing profile from around 1500 feet to the moon's surface. To do this, the LLRV had a General Electric CF-700-2V turbofan engine mounted vertically in gimbals, with 4200 pounds of thrust. The engine, using JP-4 fuel, got the vehicle up to the test altitude and was then throttled back to support five-sixths of the vehicle's weight, simulating the reduced gravity of the moon. Two hydrogen-peroxide lift rockets with thrust that could be varied from 100 to 500 pounds handled the LLRV's rate of descent and horizontal translations. Sixteen smaller hydrogen-peroxide r