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Three Martian dust devils can be seen near the rim of Jezero Crater in this short video made of images taken by a navigation camera aboard NASA’s Perseverance rover on Sept. 6, 2025. The microphone on the rover’s SuperCam previously captured audio when a dust devil passed over.NASA/JPL-Caltech/SSI

Perseverance confirmed a long-suspected phenomenon in which electrical discharges and their associated shock waves can be born within Red Planet mini-twisters.

NASA’s Perseverance Mars rover has recorded the sounds of electrical discharges —sparks — and mini-sonic booms in dust devils on Mars. Long theorized, the phenomenon has now been confirmed through audio and electromagnetic recordings captured by the rover’s SuperCam microphone. The discovery, published Nov. 26 in the journal Nature, has implications for Martian atmospheric chemistry, climate, and habitability, and could help inform the design of future robotic and human missions to Mars.

A frequent occurrence on the Red Planet, dust devils form from rising and rotating columns of warm air. Air near the planet’s surface becomes heated by contact with the warmer ground and rises through the denser, cooler air above. As other air moves along the surface to take the place of the rising warmer air, it begins to rotate. When the incoming air rises into the column, it picks up speed like spinning ice skaters bringing their arms closer to their body. The air rushing in also picks up dust, and a dust devil is born.

SuperCam has recorded 55 distinct electrical events over the course of the mission, beginning on the mission’s 215thMartian day, or sol, in 2021. Sixteen have been recorded when dust devils passed directly over the rover.

Decades before Perseverance landed, scientists theorized that the friction generated by tiny dust grains swirling and rubbing against each other in Martian dust devils could generate enough of an electrical charge to eventually produce electrical arcs. Called the triboelectric effect, it’s the phenomenon at play when someone walks over a carpet in socks and then touches a metal doorknob, generating a spark. In fact, that is about the same level of discharge as what a Martian dust devil might produce.

“Triboelectric charging of sand and snow particles is well documented on Earth, particularly in desert regions, but it rarely results in actual electrical discharges,” said Baptiste Chide, a member of the Perseverance science team and a planetary scientist at L’Institut de Recherche en Astrophysique et Planétologie in France. “On Mars, the thin atmosphere makes the phenomenon far more likely, as the amount of charge required to generate sparks is much lower than what is required in Earth’s near-surface atmosphere.”

Perseverance’s SuperCam instrument carries a microphone to analyze the sounds of the instrument’s laser when it zaps rocks, but the team has also captured the sounds of wind and even the first audio recording of a Martian dust devil. Scientists knew it could pick up electromagnetic disturbance (static) and sounds of electrical discharges in the atmosphere. What they didn’t know was if such events happened frequently enough, or if the rover would ever be close enough, to record one. Then they began to assess data amassed over the mission, and it didn’t take long to find the telltale sounds of electrical activity.

The SuperCam microphone on NASA’s Perseverance captured this recording of the sounds of electrical discharge as a dust devil passed over the Mars rover on Oct. 12, 2024. The three crackles can be heard in between the sounds of the dust devil’s front and trailing walls.
Credit: NASA/JPL-Caltech/LANL/CNES/CNRS/ISAE-Supaero Crackle, pop

“We got some good ones where you can clearly hear the ‘snap’ sound of the spark,” said coauthor Ralph Lorenz, a Perseverance scientist at the Johns Hopkins Applied Physics Lab in Laurel, Maryland. “In the Sol 215 dust devil recording, you can hear not only the electrical sound, but also the wall of the dust devil moving over the rover. And in the Sol 1,296 dust devil, you hear all that plus some of the particles impacting the microphone.”

Thirty-five other discharges were associated with the passage of convective fronts during regional dust storms. These fronts feature intense turbulence that favor triboelectric charging and charge separation, which occurs when two objects touch, transfer electrons, and separate — the part of the triboelectric effect that results in a spark of static electricity.

Researchers found electrical discharges did not seem to increase during the seasons when dust storms, which globally increase the presence of atmospheric dust, are more common on Mars. This result suggests that electrical buildup is more closely tied to the localized, turbulent lifting of sand and dust rather than high dust density alone.

While exploring the rim of Jezero Crater on Mars, NASA’s Perseverance rover captured new images of multiple dust devils in January 2025. These captivating phenomena have been documented for decades by the agency’s Red Planet robotic explorers.
Credit: NASA/JPL-Caltech/LANL/CNES/CNRS/INTA-CSIC/Space Science Institute/ISAE-Supaero/University of Arizona Profound effects

The proof of these electrical discharges is a discovery that dramatically changes our understanding of Mars. Their presence means that the Martian atmosphere can become sufficiently charged to activate chemical reactions, leading to the creation of highly oxidizing compounds, such as chlorates and perchlorates. These strong substances can effectively destroy organic molecules (which constitute some of the components of life) on the surface and break down many atmospheric compounds, completely altering the overall chemical balance of the Martian atmosphere.

This discovery could also explain the puzzling ability of Martian methane to vanish rapidly, offering a crucial piece of the puzzle for understanding the constraints life may have faced and, therefore, the planet’s potential to be habitable.

Given the omnipresence of dust on Mars, the presence of electrical charges generated by particles rubbing together would seem likely to influence dust transport on Mars as well. How dust travels on Mars plays a central role in the planet’s climate but remains poorly understood.

Confirming the presence of electrostatic discharges will also help NASA understand potential risks to the electronic equipment of current robotic missions. That no adverse electrostatic discharge effects have been reported in several decades of Mars surface operations may attest to careful spacecraft grounding practices. The findings could also inform safety measures developed for future astronauts exploring the Red Planet.

More about Perseverance

Managed for NASA by Caltech, the Jet Propulsion Laboratory in Southern California built and manages operations of the Perseverance rover on behalf of the agency’s Science Mission Directorate as part of NASA’s Mars Exploration Program portfolio.

To learn more about Perseverance visit:
https://science.nasa.gov/mission/mars-2020-perseverance

News Media Contacts

DC Agle
Jet Propulsion Laboratory, Pasadena, Calif.
818-393-9011
agle@jpl.nasa.gov

Karen Fox / Molly Wasser
NASA Headquarters, Washington
202-358-1600 / 240-419-1732
karen.c.fox@nasa.gov / molly.l.wasser@nasa.gov

2025-132

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Details Last Updated Dec 03, 2025 Related Terms

• Perseverance (Rover)
• Mars
• Mars 2020

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This NASA/ESA Hubble Space Telescope image features the spiral galaxy NGC 4535.

ESA/Hubble & NASA, F. Belfiore, J. Lee and the PHANGS-HST Team

This NASA/ESA Hubble Space Telescope image features the spiral galaxy NGC 4535, which is situated about 50 million light-years away in the constellation Virgo (the Maiden). Through a small telescope, this galaxy appears extremely faint, giving it the nickname ‘Lost Galaxy’. With a mirror spanning nearly eight feet (2.4 meters) across and its location above Earth’s light-obscuring atmosphere, Hubble can easily observe dim galaxies like NGC 4535 and pick out features like its massive spiral arms and central bar of stars.

This image features NGC 4535’s young star clusters, which dot the galaxy’s spiral arms. Glowing-pink clouds surround many of these bright-blue star groupings. These clouds, called H II (‘H-two’) regions, are a sign that the galaxy is home to especially young, hot, and massive stars that blaze with high-energy radiation. Such massive stars shake up their surroundings by heating their birth clouds with powerful stellar winds, eventually exploding as supernovae.

The image incorporates data from an observing program designed to catalog roughly 50,000 H II regions in nearby star-forming galaxies like NGC 4535. Hubble released a previous image of NGC 4535 in 2021. Both the 2021 image and this new image incorporate observations from the PHANGS observing program, which seeks to understand the connections between young stars and cold gas. Today’s image adds a new dimension to our understanding of NGC 4535 by capturing the brilliant red glow of the nebulae that encircle massive stars in their first few million years of life.

Image credit: ESA/Hubble & NASA, F. Belfiore, J. Lee and the PHANGS-HST Team

ESA/Hubble & NASA, F. Belfiore, J. Lee and the PHANGS-HST Team

This NASA/ESA Hubble Space Telescope image features the spiral galaxy NGC 4535, which is situated about 50 million light-years away in the constellation Virgo (the Maiden). Through a small telescope, this galaxy appears extremely faint, giving it the nickname ‘Lost Galaxy’. With a mirror spanning nearly eight feet (2.4 meters) across and its location above Earth’s light-obscuring atmosphere, Hubble can easily observe dim galaxies like NGC 4535 and pick out features like its massive spiral arms and central bar of stars.

This image features NGC 4535’s young star clusters, which dot the galaxy’s spiral arms. Glowing-pink clouds surround many of these bright-blue star groupings. These clouds, called H II (‘H-two’) regions, are a sign that the galaxy is home to especially young, hot, and massive stars that blaze with high-energy radiation. Such massive stars shake up their surroundings by heating their birth clouds with powerful stellar winds, eventually exploding as supernovae.

The image incorporates data from an observing program designed to catalog roughly 50,000 H II regions in nearby star-forming galaxies like NGC 4535. Hubble released a previous image of NGC 4535 in 2021. Both the 2021 image and this new image incorporate observations from the PHANGS observing program, which seeks to understand the connections between young stars and cold gas. Today’s image adds a new dimension to our understanding of NGC 4535 by capturing the brilliant red glow of the nebulae that encircle massive stars in their first few million years of life.

Image credit: ESA/Hubble & NASA, F. Belfiore, J. Lee and the PHANGS-HST Team

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Conventionally, the moon is thought to have formed during one big impact, but a three-impact model might make more sense

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3 min read

Preparations for Next Moonwalk Simulations Underway (and Underwater) A space toxicologist at NASA JSC.NASA

Hazardous Materials Summary Tables (HMSTs) are a compilation of the chemical, biological, and flammability hazards of materials on a given flight or mission. HMSTs are required by Safety for all Programs, including but not limited to ISS, Commercial Crew Program (CCP), Multi Purpose Crew Vehicle (MPCV), and Gateway. Johnson Space Center (JSC) toxicologists evaluate the toxic hazard level of all liquids, gases, particles, or gels flown on or to any manned U.S. spacecraft. The biosafety hazard level and flammability levels are assigned by JSC microbiologists and materials experts and are documented in an HMST and in a computerized in-flight version of the HMST called the HazMat (Hazardous Materials) database.

How To Obtain Toxicological Hazard Assessments

“Requirements for Submission of Data Needed for Toxicological Assessment of Chemical and Biologicals to be Flown on Manned Spacecraft”

• JSC 27472 (PDF, 766KB) defines the terms “chemicals” and “biological materials” as applied to items being flown on or to any U.S. spacecraft. It explains who must submit information to the JSC toxicologists concerning the materials to be flown and specifies what information is needed. It provides schedules, formats, and contact information.
• Additional US requirements for biological materials can be found on the Biosafety Review Board (BRB) page.
• Additional US requirements for environmental control and life support (ECLS) assessments can be found in JSC 66869 (PDF, 698KB).

Data Submission

For all flights to ISS and all Artemis requests (Orion, Gateway, Human Lander System (HLS)), please submit data via the electronic hazardous materials summary table (eHMST) tool. If you do not have access to this tool, please submit a NAMS request for access to JSC – CMC External Tools. Please reference eHMST training for more information

NOTE:  For experimental payloads/hardware planned for launch on a Russian vehicle, stowed and/or operated on the Russian Segment of ISS, or planned for return or disposal on a Russian vehicle, we strongly encourage payload providers to submit biological and chemical data to the Russian Institute for Biomedical Problems (moukhamedieva@imbp.ru OR barantseva@imbp.ru).

Hazard Assessments

Toxicological hazard assessments are conducted according to JSC 26895 – Guidelines for Assessing the Toxic Hazard of Spacecraft Chemicals and Test Materials. The resulting Toxicity Hazard Level (THL) in combination with the BioSafety Level (BSL) and Flammability Hazard Level (FHL) form the basis for the combined Hazard Response Level (HRL) used for labeling and operational response per flight rule B20-16.

Toxicology and Environmental Chemistry Share

Details Last Updated Dec 03, 2025 EditorRobert E. LewisLocationJohnson Space Center Related Terms

• Human Health and Performance

Explore More 5 min read Toxicology and Environmental Chemistry Article 3 years ago 4 min read Exposure Guidelines (SMACs and SWEGs) Article 3 years ago 4 min read Toxicology Analysis of Spacecraft Air Article 2 days ago Keep Exploring Discover Related Topics

Missions

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3 min read

Preparations for Next Moonwalk Simulations Underway (and Underwater) A space toxicologist at NASA JSC.NASA

Hazardous Materials Summary Tables (HMSTs) are a compilation of the chemical, biological, and flammability hazards of materials on a given flight or mission. HMSTs are required by Safety for all Programs, including but not limited to ISS, Commercial Crew Program (CCP), Multi Purpose Crew Vehicle (MPCV), and Gateway. Johnson Space Center (JSC) toxicologists evaluate the toxic hazard level of all liquids, gases, particles, or gels flown on or to any manned U.S. spacecraft. The biosafety hazard level and flammability levels are assigned by JSC microbiologists and materials experts and are documented in an HMST and in a computerized in-flight version of the HMST called the HazMat (Hazardous Materials) database.

How To Obtain Toxicological Hazard Assessments

“Requirements for Submission of Data Needed for Toxicological Assessment of Chemical and Biologicals to be Flown on Manned Spacecraft”

• JSC 27472 (PDF, 766KB) defines the terms “chemicals” and “biological materials” as applied to items being flown on or to any U.S. spacecraft. It explains who must submit information to the JSC toxicologists concerning the materials to be flown and specifies what information is needed. It provides schedules, formats, and contact information.
• Additional US requirements for biological materials can be found on the Biosafety Review Board (BRB) page.
• Additional US requirements for environmental control and life support (ECLS) assessments can be found in JSC 66869 (PDF, 698KB).

Data Submission

For all flights to ISS and all Artemis requests (Orion, Gateway, Human Lander System (HLS)), please submit data via the electronic hazardous materials summary table (eHMST) tool. If you do not have access to this tool, please submit a NAMS request for access to JSC – CMC External Tools. Please reference eHMST training for more information

NOTE:  For experimental payloads/hardware planned for launch on a Russian vehicle, stowed and/or operated on the Russian Segment of ISS, or planned for return or disposal on a Russian vehicle, we strongly encourage payload providers to submit biological and chemical data to the Russian Institute for Biomedical Problems (moukhamedieva@imbp.ru OR barantseva@imbp.ru).

Hazard Assessments

Toxicological hazard assessments are conducted according to JSC 26895 – Guidelines for Assessing the Toxic Hazard of Spacecraft Chemicals and Test Materials. The resulting Toxicity Hazard Level (THL) in combination with the BioSafety Level (BSL) and Flammability Hazard Level (FHL) form the basis for the combined Hazard Response Level (HRL) used for labeling and operational response per flight rule B20-16.

Toxicology and Environmental Chemistry Share

Details Last Updated Dec 03, 2025 EditorRobert E. LewisLocationJohnson Space Center Related Terms

• Human Health and Performance

Explore More 5 min read Toxicology and Environmental Chemistry Article 3 years ago 4 min read Exposure Guidelines (SMACs and SWEGs) Article 3 years ago 4 min read Toxicology Analysis of Spacecraft Air Article 2 days ago Keep Exploring Discover Related Topics

Missions

Humans in Space

Climate Change

Solar System

4 min read

Preparations for Next Moonwalk Simulations Underway (and Underwater) SpaceX Crew-1 Pilot Victor Glover and Mission Specialist Shannon Walker work with a Grab Sample Container (GSC) in the SpaceX Crew Dragon Resilience spacecraft while en route to the ISS.NASA

Toxicology and Environmental Chemistry (TEC) monitors airborne contaminants in both spacecraft air and water. In-flight monitors are employed to provide real-time insight into the environmental conditions on ISS. Archival samples are collected and returned to Earth for full characterization of ISS air and water.

Real-time in-flight air analytical instruments include the Air Quality Monitors (AQM), carbon dioxide (CO2 monitors), and a compound specific analyzer for combustion products (CSA-CP). Real-time in-flight water monitoring capabilities include the colorimetric water quality monitoring kit (CWQMK) and the ISS total organic carbon analyzer (TOCA).

Post-flight analyses are performed on archival samples of spacecraft air and water obtained at specific times and locations during a mission. Air archival samples are collected using “grab sample containers” (GSC) and formaldehyde badges. The U.S. and Russian water recovery systems on the ISS process atmospheric moisture (U.S. and Russian systems) and urine distillate (U.S. system only) into clean, potable water for the crew to use.  The Water Kit is utilized to collect archival samples of the potable water and are routinely returned to the ground to monitor the quality of the water produced by the systems.  Samples of condensate and wastewater are also collected and returned to check for the presence of contaminants that could break through the water recovery systems.   

Results of Post-Flight Analysis of In-Flight Air Samples  (Most Recent First)     

• Increment 71 Report Including NG-21 Ingress and Boeing-CFT Ascent (1MB)
• Increment 70 including SpaceX-29, Axiom-3, NG-20, and SpaceX-30 Ingresses (817KB)
• Increment 69 Report Including Ax2 SpX28 NG19 Ingress (1MB)
• Increment 68 Report NG18 SpX26 SpX27 Ingress (845KB)
• Increment 65 Report with SpX22, MLM, NG16, SpX23 Ingresses (1.5MB)
• Increment 67 Report with OFT2 and SpX25 Ingress (962KB)
• Increment 66 Report SpX-24 NG-17 Ingress (835KB)
• Increment 64 including SpX-21 and NG-15 Ingress (897KB)
• Increment 63 Including HTV-9 and NG-14 Ingress (884KB)
• Increment 62-63 Benzene Anomaly Report (442KB)
• Increment 62 Including NG-13 and SpX-20 Ingress (747KB)
• Increment 61 including NG-12 and SpX-19 Egress (1.1MB)
• Increment 60 including SpX-18 and HTV8 Ingress (1.27MB)
• Increment 59 including NG-11 and SpX-17 Ingress (3.4MB)
• Increment 58 Report (2.78MB)
• Increment 57 including NG-10 and SpX-16 Ingress (2.71MB)
• SpaceX Demo-1 Ingress SM and DM1 Contingencies (792KB)
• Increment 56, HTV-7 and Node 1 Contingency Report (3.5MB)
• Increment 55 and SpX14 and OA9 Ingresses Report (1.9MB)
• Increment 54, including SpX-13 Ingress (877KB)
• Increment 53, including OA-8 Ingress and Node 1 Contingency Investigation (743KB)
• Increment 52 Report, including JEM odor contingency, SpX-11 and SpX-12 ingress, and WPA MF bed contingency samples
• Increment 51 and OA-7 Ingress Report (1.47MB)
• Increment 50 and HTV-6, SpX-10 Ingresses (2.72 MB)
• Increment 49 OA-5 Ingress and Oil Paint Odor Investigation Report (3.12MB)
• Increment 48, SpX-9 Ingress, and Oil Paint Odor Investigation Report (3.43MB)
• Increment 47, BEAM/OA-6/SpX-8 Ingresses, and Node 3 Siloxane Investigation Report (4.82MB)
• Increment 46 and Node 3 Contingency Report (4.4MB)
• Increment 45 and OA-4 Ingress (3MB)
• Increment 44 and HTV-5 Ingress Report (1.6MB)
• Increment 43, SpX-6 Ingress, Ethanol Investigation, and Node 1 Contingency Report (6.2MB)
• Increment 42 Report (4MB)
• Increment 41 Report (3.3MB)
• Space X-5 First Ingress Air Quality and Node 3 Contingency Report (2MB)
• SpaceX-4 First Ingress Air Quality Report (1.32MB)
• Increment 40, Orb-2/ATV-5 Ingresses, and SM Contingency (2.92 MB)
• Increment 39 and SpX-3 Ingress (5.75 MB)
• Increment 38 and Orb-1 Ingress (8.02 MB)
• Increment 37 and Orb-D1 Ingress (5.9 MB)
• Increment 36 and HTV-4 Ingress (7.22 MB)
• Increment 35 Report (4.04 MB)
• Increment 34 Report (5.64 MB)
• Feb. 2013 Contingency Sample Report (1.91 MB)
• Space X-2 First Entry Sample Analyses (1.56 MB)
• Soyuz 31S Return Samples (2.98 MB)
• Space X-1 First Entry Sample Analysis (39 KB)
• Revised Soyuz 30 Return Samples (7.46 MB)
• Space X-Demo First Entry Sample Analysis (767 KB)
• Soyuz 28 and Soyuz 29 Return Samples (1 MB)
• Soyuz 27 Return Samples (824 KB)
• STS-134, ULF7, 26S (2 MB)
• STS-133 / ISS-ULF5 (396 KB)
• Soyuz 25S Mission Report (286 KB)
• Soyuz 24S Return Samples of ISS Air (740 KB)
• Soyuz 23S Return Samples (593 KB)
• STS-132 / ISS-ULF4 (1.31 MB)
• STS-131 / ISS-19A (3.55 MB)
• STS-130 / ISS-20A (1.27 MB)
• STS-129 / ISS-ULF3 (1.4 MB)

Toxicology and Environmental Chemistry Share

Details Last Updated Dec 04, 2025 EditorRobert E. LewisLocationJohnson Space Center Related Terms

• Human Health and Performance

Explore More 5 min read Toxicology and Environmental Chemistry Article 3 years ago 3 min read Hazardous Material Summary Tables (HMSTs) Article 2 days ago 4 min read Exposure Guidelines (SMACs and SWEGs) Article 3 years ago Keep Exploring Discover More Topics From NASA

Missions

Humans in Space

Climate Change

Solar System

4 min read

Preparations for Next Moonwalk Simulations Underway (and Underwater) SpaceX Crew-1 Pilot Victor Glover and Mission Specialist Shannon Walker work with a Grab Sample Container (GSC) in the SpaceX Crew Dragon Resilience spacecraft while en route to the ISS.NASA

Toxicology and Environmental Chemistry (TEC) monitors airborne contaminants in both spacecraft air and water. In-flight monitors are employed to provide real-time insight into the environmental conditions on ISS. Archival samples are collected and returned to Earth for full characterization of ISS air and water.

Real-time in-flight air analytical instruments include the Air Quality Monitors (AQM), carbon dioxide (CO2 monitors), and a compound specific analyzer for combustion products (CSA-CP). Real-time in-flight water monitoring capabilities include the colorimetric water quality monitoring kit (CWQMK) and the ISS total organic carbon analyzer (TOCA).

Post-flight analyses are performed on archival samples of spacecraft air and water obtained at specific times and locations during a mission. Air archival samples are collected using “grab sample containers” (GSC) and formaldehyde badges. The U.S. and Russian water recovery systems on the ISS process atmospheric moisture (U.S. and Russian systems) and urine distillate (U.S. system only) into clean, potable water for the crew to use.  The Water Kit is utilized to collect archival samples of the potable water and are routinely returned to the ground to monitor the quality of the water produced by the systems.  Samples of condensate and wastewater are also collected and returned to check for the presence of contaminants that could break through the water recovery systems.   

Results of Post-Flight Analysis of In-Flight Air Samples  (Most Recent First)     

• Increment 71 Report Including NG-21 Ingress and Boeing-CFT Ascent (1MB)
• Increment 70 including SpaceX-29, Axiom-3, NG-20, and SpaceX-30 Ingresses (817KB)
• Increment 69 Report Including Ax2 SpX28 NG19 Ingress (1MB)
• Increment 68 Report NG18 SpX26 SpX27 Ingress (845KB)
• Increment 65 Report with SpX22, MLM, NG16, SpX23 Ingresses (1.5MB)
• Increment 67 Report with OFT2 and SpX25 Ingress (962KB)
• Increment 66 Report SpX-24 NG-17 Ingress (835KB)
• Increment 64 including SpX-21 and NG-15 Ingress (897KB)
• Increment 63 Including HTV-9 and NG-14 Ingress (884KB)
• Increment 62-63 Benzene Anomaly Report (442KB)
• Increment 62 Including NG-13 and SpX-20 Ingress (747KB)
• Increment 61 including NG-12 and SpX-19 Egress (1.1MB)
• Increment 60 including SpX-18 and HTV8 Ingress (1.27MB)
• Increment 59 including NG-11 and SpX-17 Ingress (3.4MB)
• Increment 58 Report (2.78MB)
• Increment 57 including NG-10 and SpX-16 Ingress (2.71MB)
• SpaceX Demo-1 Ingress SM and DM1 Contingencies (792KB)
• Increment 56, HTV-7 and Node 1 Contingency Report (3.5MB)
• Increment 55 and SpX14 and OA9 Ingresses Report (1.9MB)
• Increment 54, including SpX-13 Ingress (877KB)
• Increment 53, including OA-8 Ingress and Node 1 Contingency Investigation (743KB)
• Increment 52 Report, including JEM odor contingency, SpX-11 and SpX-12 ingress, and WPA MF bed contingency samples
• Increment 51 and OA-7 Ingress Report (1.47MB)
• Increment 50 and HTV-6, SpX-10 Ingresses (2.72 MB)
• Increment 49 OA-5 Ingress and Oil Paint Odor Investigation Report (3.12MB)
• Increment 48, SpX-9 Ingress, and Oil Paint Odor Investigation Report (3.43MB)
• Increment 47, BEAM/OA-6/SpX-8 Ingresses, and Node 3 Siloxane Investigation Report (4.82MB)
• Increment 46 and Node 3 Contingency Report (4.4MB)
• Increment 45 and OA-4 Ingress (3MB)
• Increment 44 and HTV-5 Ingress Report (1.6MB)
• Increment 43, SpX-6 Ingress, Ethanol Investigation, and Node 1 Contingency Report (6.2MB)
• Increment 42 Report (4MB)
• Increment 41 Report (3.3MB)
• Space X-5 First Ingress Air Quality and Node 3 Contingency Report (2MB)
• SpaceX-4 First Ingress Air Quality Report (1.32MB)
• Increment 40, Orb-2/ATV-5 Ingresses, and SM Contingency (2.92 MB)
• Increment 39 and SpX-3 Ingress (5.75 MB)
• Increment 38 and Orb-1 Ingress (8.02 MB)
• Increment 37 and Orb-D1 Ingress (5.9 MB)
• Increment 36 and HTV-4 Ingress (7.22 MB)
• Increment 35 Report (4.04 MB)
• Increment 34 Report (5.64 MB)
• Feb. 2013 Contingency Sample Report (1.91 MB)
• Space X-2 First Entry Sample Analyses (1.56 MB)
• Soyuz 31S Return Samples (2.98 MB)
• Space X-1 First Entry Sample Analysis (39 KB)
• Revised Soyuz 30 Return Samples (7.46 MB)
• Space X-Demo First Entry Sample Analysis (767 KB)
• Soyuz 28 and Soyuz 29 Return Samples (1 MB)
• Soyuz 27 Return Samples (824 KB)
• STS-134, ULF7, 26S (2 MB)
• STS-133 / ISS-ULF5 (396 KB)
• Soyuz 25S Mission Report (286 KB)
• Soyuz 24S Return Samples of ISS Air (740 KB)
• Soyuz 23S Return Samples (593 KB)
• STS-132 / ISS-ULF4 (1.31 MB)
• STS-131 / ISS-19A (3.55 MB)
• STS-130 / ISS-20A (1.27 MB)
• STS-129 / ISS-ULF3 (1.4 MB)

Toxicology and Environmental Chemistry Share

Details Last Updated Dec 04, 2025 EditorRobert E. LewisLocationJohnson Space Center Related Terms

• Human Health and Performance

Explore More 5 min read Toxicology and Environmental Chemistry Article 3 years ago 3 min read Hazardous Material Summary Tables (HMSTs) Article 2 days ago 4 min read Exposure Guidelines (SMACs and SWEGs) Article 3 years ago Keep Exploring Discover More Topics From NASA

Missions

Humans in Space

Climate Change

Solar System

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