Friday, 13 March 2026

Eruption at Mayon

The upper slopes of Mayon volcano appear brown, with several narrow channels radiating from the crater. A red infrared heat signature appears near the summit, with red streaks extending east and southeast. The lower slopes are green and forested. Farmland and towns are visible in the lower part of the image.
February 26, 2026

At any given moment, about 20 volcanoes on Earth are actively erupting. Often among them is Mayon—the most active volcano in the Philippines. The nearly symmetrical stratovolcano, on Luzon Island near the Albay and Lagonoy gulfs, rises more than 2,400 meters (8,000 feet) above sea level.

Historical records indicate Mayon has erupted 65 times in the past 5,000 years, with the latest episode beginning in January 2026. The Philippine Institute of Volcanology and Seismology (PHIVOLCS) first reported increased rockfalls near the volcano’s summit and inflation of the mountain’s upper slopes. On January 6, the alert level was increased to three on a five-level scale after lava began flowing from the crater and hot clouds of ash and debris called pyroclastic flows (also called pyroclastic density currents) moved down one side of the mountain.

The volcano was still puffing and lava flowing on February 26, when the OLI (Operational Land Imager) on Landsat 8 acquired this rare, relatively clear image. The natural-color scene is overlaid with infrared observations to highlight the lava’s heat signature. On that day, PHIVOLCS reported volcanic earthquakes, rockfalls, and pyroclastic flows. The longest pyroclastic flow had traveled about 4 kilometers (3 miles) through the Mi-isi Gully on the southeast flank. 

The level-three alert, which remained in place in March, prompted evacuations within a 6-kilometer (4-mile) radius of the crater, displacing hundreds of families from communities including Tabaco City, Malilpot, and Camalig. Past pyroclastic flows have proven extremely destructive, leading to more than 1,000 deaths in 1814, at least 400 deaths in 1897, and 77 deaths in 1993. More than 73,000 people were evacuated during an eruption in 1984.

Sulfur dioxide (SO2) emissions during the current eruption have averaged 2,466 tons per day, with a peak of 6,569 metric tons measured on February 4, 2026. That is the highest SO2 emission level for one day in 15 years, the PHIVOLCS announced in early February. That was later exceeded on March 6, when SO2 emissions reached as high as 7,633 metric tons

Multiple NASA satellites have also monitored the volcano’s sulfur dioxide emissions, showing sizable plumes of the gas drifting southwest on February 4 and March 6. The Philippine volcanology institute reported a peak in other activity on February 8 and 9, with 469 rockfalls, 12 major pyroclastic flows, and ashfall in the municipalities of Camalig and Guinobatan.

NASA Earth Observatory image by Michala Garrison, using Landsat data from the U.S. Geological Survey. Story by Adam Voiland.

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The upper slopes of Mayon volcano appear brown, with several narrow channels radiating from the crater. A red infrared heat signature appears near the summit, with red streaks extending east and southeast. The lower slopes are green and forested. Farmland and towns are visible in the lower part of the image.

February 26, 2026

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About Low Boom Flight Demonstrator (LBFD) Project

2 min read

Preparations for Next Moonwalk Simulations Underway (and Underwater)

NASA’s X-59 is seen in flight, with a blue sky and mountains behind it and land below it. The aircraft’s long nose and distinct silhouette are visible as it ferries to NASA’s Armstrong Flight Research Center in Edwards, California.
NASA’s X-59 quiet supersonic research aircraft cruises above Palmdale and Edwards, California, during its first flight, Tuesday, Oct. 28, 2025. The aircraft traveled to NASA’s Armstrong Flight Research Center in Edwards, California.
NASA/Lori Losey

The Low Boom Flight Demonstrator project (LBFD) is part of NASA’s effort to help enable new aircraft noise standards that are required to open the market to commercial supersonic flight over land.

The federal government banned all civilian supersonic flights over land more than fifty years ago due to sonic boom noise. If new standards are established, the U.S. aviation industry can position itself to lead the commercial supersonic market, and passengers will benefit from significantly shorter travel times.

Over the past decade, fundamental research and experimentation have demonstrated the possibility of supersonic flight with greatly reduced sonic boom noise – one of several key areas needed to transform commercial supersonic flight.  

NASA’s X-59, part of the LBFD project, sits on the ramp of Lockheed Martin’s Skunk Works facility, facing toward the site’s main hangar during sunset.
NASA’s X-59 quiet supersonic research aircraft sits on a ramp at Lockheed Martin Skunk Works in Palmdale, California, during sunset. The one-of-a-kind aircraft is powered by a General Electric F414 engine, a variant of the engines used on F/A-18 fighter jets. The engine is mounted above the fuselage to reduce the number of shockwaves that reach the ground. The X-59 is the centerpiece of NASA’s Quesst mission, which aims to demonstrate quiet supersonic flight and enable future commercial travel over land – faster than the speed of sound.
Lockheed Martin Corporation/Garr

The LBFD project will demonstrate a reduced sonic boom by utilizing a purpose-built experimental aircraft designated the X-59.

The LBFD project supports a multi-phase effort aimed at demonstrating the X-59’s ability to fly supersonic without generating loud sonic booms. The LBFD project leads Phase 1 of the Quesst mission, involving the design, fabrication, ground tests, and checkout flights of the X-59.

After ensuring the aircraft is safe and performing as expected, the LBFD project will support the rest of the mission team during Phase 2 to prove the aircraft is producing a quiet sound to people on the ground and is safe for operations in the National Airspace System.

At the conclusion of Phase 2, the X-59 aircraft will transfer to the Integrated Aviation Systems Program’s Flight Demonstrations and Capabilities project.

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About Integrated Aviation Systems Program (IASP)

1 min read

Preparations for Next Moonwalk Simulations Underway (and Underwater)

Graphic depiction of several NASA airplanes over a small city surrounded by trees.
NASA / Lillian Gipson

The Integrated Aviation Systems Program (IASP) conducts research and integrated, systems-level demonstrations in a flight environment to prove, mature and transition them into future aircraft and systems. The program aims to determine feasibility and accelerate development of less mature technologies, and for more mature technologies, execute highly complex flight demonstrations to prove and accelerate technology transition to industry.

IASP Projects

The program’s portfolio currently consists of these projects: Subsonic Flight DemonstratorElectrified Powertrain Flight Demonstration, Low Boom Flight Demonstrator, and Flight Demonstrations and Capabilities

A white and blue NASA F-15 research jet climbs to altitude with an approximately 3-foot experimental wing design mounted beneath its fuselage. Viewed in profile against a blue sky with mountains in the distance, the test article resembles a ventral fin below the aircraft. The work is part of NASA's Integrated Aviation Systems Program (IASP).
NASA’s Crossflow Attenuated Natural Laminar Flow (CATNLF) scale-model wing flies for the first time on a NASA F-15 research jet during a test flight from NASA’s Armstrong Flight Research Center in Edwards, California. The 75-minute flight confirmed the aircraft could maneuver safely with the approximately 3-foot-tall test article mounted beneath it. NASA will continue flight tests to collect data that validates the CATNLF design and its potential to improve laminar flow, reducing drag and lowering fuel costs for future commercial aircraft.
NASA/Carla Thomas
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NASA to Cover Upcoming US Spacewalks 94, 95 Outside Space Station

NASA astronaut and Expedition 72 Flight Engineer Anne McClain is pictured near one of the International Space Station's main solar arrays during a spacewalk to upgrade the orbital outpost's power generation system and relocate a communications antenna.
NASA astronaut Anne McClain works near one of the International Space Station’s main solar arrays during a May 1, 2025, spacewalk to upgrade the station’s power system and relocate a communications antenna.
Credit: NASA

NASA astronauts will conduct a pair of spacewalks beginning Wednesday, March 18, outside of the International Space Station to prepare for the installation of two roll-out solar arrays. Experts from NASA will preview the spacewalks during a news conference at 2 p.m. EDT, Monday, March 16, at the agency’s Johnson Space Center in Houston.

Watch NASA’s live coverage of the news conference on the agency’s YouTube channel. Learn how to stream NASA content through a variety of online platforms, including social media.

NASA participants include:

  • Bill Spetch, operations integration manager, International Space Station Program
  • Diana Trujillo, spacewalk flight director, Flight Operations Directorate
  • Ronak Dave, spacewalk flight director, Flight Operations Directorate

Media interested in participating in person or by phone must contact the NASA Johnson newsroom no later than 10 a.m. on March 16 by calling 281-483-5111 or emailing jsccommu@mail.nasa.gov. To ask questions by phone, reporters must dial into the news conference no later than 15 minutes prior to the start of the call. Questions also may be submitted on social media using #AskNASA. NASA’s media accreditation policy is available online.

On March 18, NASA astronauts Jessica Meir and Chris Williams will conduct U.S. spacewalk 94, exiting the orbiting laboratory’s Quest airlock to prepare the 2A power channel for the future International Space Station Roll-Out Solar Arrays (IROSA) installation. It will be Meir’s fourth spacewalk and Williams’ first.

Watch NASA’s live coverage beginning at 6:30 a.m. on NASA+, Amazon Prime, and the agency’s YouTube channel. U.S. spacewalk 94 will begin at approximately 8 a.m. and is expected to last about six and a half hours.

For U.S. spacewalk 95, two NASA astronauts will prepare the station’s 3B power channel for a future IROSA installation. NASA will provide more information on the date and time of the spacewalk, the crew members assigned to the activity, and coverage details closer to the operation.

The spacewalks will be the 278th and 279th supporting space station assembly, maintenance and upgrades. They also are the first two station spacewalks of 2026 and the first for Expedition 74. Spacewalks 94 and 95 originally were scheduled for January, but the target dates were adjusted after the early departure of NASA’s SpaceX Crew‑11 mission.

Learn more about International Space Station research and operations at:

https://www.nasa.gov/station

-end-

Josh Finch / Jimi Russell
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202-358-1100
joshua.a.finch@nasa.gov / james.j.russell@nasa.gov

Sandra Jones
Johnson Space Center, Houston
281-483-5111
sandra.p.jones@nasa.gov

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Mar 12, 2026
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Thursday, 12 March 2026

Efficient Large Displacement/Large Rotation Dynamic Simulations Using Nonlinear Dynamic Substructures

Download PDF: Efficient Large Displacement/Large Rotation Dynamic Simulations Using Nonlinear Dynamic Substructures

Utilizing reduced-order dynamic math models (DMM) in linear system-level dynamic analyses is a well-known practice that enables extreme computational efficiencies. But what about nonlinear system dynamics? Reduced-order DMMs have found their way into contact dynamics. The engineer must look no further than the Henkel-Mar pad separation analysis methodology to verify this fact. More sophisticated applications of DMMs in contact dynamics are possible when certain repetitive geometry pattens are present. For example, Figure 1 shows a type of pipe known as a “flexible” pipe used by the subsea industry. This design features four layers of helically wound steel wires that provide the pipe with its stick/slip behavior during bending, thereby enabling a longer fatigue life in harsh ocean environments. With these helically wound armor layers presenting a repetitive contact topology, contact surfaces can be constructed and tracked enabling the friction logic to operate resulting in the friction hysteretic moment-curvature plot provided in Figure 1 (top). 

Flexible pipe used in subsea industry; moment-curvature of the flexible pipe using reduced-order dynamic math models for surface contact
Flexible pipe used in subsea industry; moment-curvature of the flexible pipe using reduced-order dynamic math models for surface contact 

As seen from Figure 1, the pipe was subjected to many bending cycles and executed in essentially a real-time computation. A single bending cycle of the same pipe in full finite element model (FEM) resolution (i.e., no use of DMMs) would require 48 hours of computation on 36 central processing units (CPUs) running in parallel given the very large order of the FEM.   

What about utilizing DMMs for computationally efficient nonlinear dynamics involving large displacements and rotations? Before addressing this question, the residual flexibility mixed boundary transformation (RFMB1) must be defined. The RFMB coordinate transformation is given as follows: 

The RFMB transformation connects physical and modal degrees of freedom (DoFs) to a reduced set of generalized coordinates

The transformation is a mix of the following submatrices: constraint modes (ψ) due to unit displacements on the b-set boundary degrees of freedom (DoFs) that remain fixed during the eigenvalue problem, residual flexibility (g) due to unit forces at the c-set boundary DoFs that remain free during the eigenvalue problem, and a truncated set of normal modes (φ) computed with the b-set DoFs constrained. It can be shown that the transformation retains full flexibility at the DMM physical DoFs and retains the full dynamics of the FEM up to the user-selected truncation frequency for the normal modes. The reduction of DoFs, and hence the computational efficiency, arises from the number of kept modes (k) being significantly less than the number of interior FEM DoFs. 

Cantilever beam model composed of 20 DMMs
Cantilever beam model composed of 20 DMMs
Cantilever beam rolled up using the 20 NDS DMMs
Cantilever beam rolled up using the 20 NDS DMMs
Same beam bent into “catenary-like” configuration by turning on gravity
Same beam bent into “catenary-like” configuration by turning on gravity

To enable DMM large displacements/rotations, four coordinates are added to the above RFMB to track large rotations. These quaternions replace the rigid-body modes that are only valid for infinitesimal rotations. With this process, the RFMB is transformed into a nonlinear dynamic substructure (NDS). Solution algorithms need to be modified accordingly as well to allow for equilibrium iterations since the problem now is highly nonlinear. As an example, consider the undeformed cantilever beam model (Figure 2) composed of 20 DMMs (single DMM of a beam composed of 5 CBAR elements repeated 20x).   

A moment is applied at the free end (right end) of Figure 2. While small displacement theory is limited and breaks down after a few degrees of rotation, the cantilever beam can be completely rolled up using NDS (see Figure 3) in a highly nonlinear dynamic simulation. Also note that the entire nonlinear dynamic simulation was executed in seconds on a laptop and included all dynamic effects. Similarly, the beam can be bent into a “catenary-like2” shape by turning on gravity and enforcing displacements at each end to the required coupling location (see Figure 4). 

One application for this large displacement/rotation NDS capability has been to include umbilical models in the coupled loads analysis (CLA) framework. Figure 5 shows the Interim Cryogenic Propulsion Stage (ICPS) umbilical that was integrated into the Space Launch System (SLS) CLA. The SLS CLA is an integrated assembly of various component DMMs (boosters, core stage, mobile launcher (ML), upper stage, etc.) to which the ICPS umbilical (ICPSU) and its hoses as NDS DMMs can now be added. For each hose, one end connects to the SLS vehicle and the other end to the ML structure. As an example, Figure 6 shows the evolution of the deformations of the forward vent hose (modeled with 20 NDS DMMs) as it goes from the undeformed geometry (straight line) into its prelaunch geometry during the initial condition setup in the CLA. 

As the timed command for umbilical separation is given, the vehicle-side ground plate separates (using the Henkel-Mar contact/separation algorithm) and the ML gantry rotates the separating umbilical away from the already lifting vehicle (the gantry was brought into the CLA as a NDS capable of large rotations). Figure 7 captures the post-separation forward vent hose dynamics (extracted from the CLA). From this, 100  ICPSU hose clearances to the lifting vehicle can be computed. 

The power of the reduced-order models does not end with linear dynamics. It is possible to introduce large displacements and rotations into reduced-order models to enable seamless integration into large substructured integrated system dynamic analyses such as a CLA. For the specific case of the SLS, this capability allowed us to integrate umbilicals into the CLA to more accurately capture the impact of system flexibilities, dynamic response to forcing functions, pad separation “twang” effects, ML dynamics, and gantry/umbilical timings on clearances.  

For information, contact Dr. Dexter Johnson.  dexter.johnson@nasa.gov 

ICPSU model integratedinto the SLS CLA
ICPSU model integratedinto the SLS CLA
ICPSU forward vent hose evolution of deformations from undeformed (straight line) to prelaunch configuration (locking in preloads) during the CLA initial conditions setup (extracted from the CLA)
ICPSU forward vent hose evolution of deformations from undeformed (straight line) to prelaunch configuration (locking in preloads) during the CLA initial conditions setup (extracted from the CLA)
Forward vent hose post-separation dynamics (extracted from the CLA)
Forward vent hose post-separation dynamics (extracted from the CLA)


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Dust Outbreak Reaches Europe

March 1–9, 2026

Winter winds lofted clouds of dust from the Sahara Desert, carrying it north toward the Mediterranean and dispersing it widely across Europe in March 2026. When the dust combined with moisture-laden weather systems, a dirty rain fell in parts of Spain, France, and the United Kingdom.

This animation highlights the concentration and movement of dust throughout the region from March 1 to March 9. It depicts dust column mass density—a measure of the amount of dust contained in a column of air—produced with a version of the GEOS (Goddard Earth Observing System) model. The model integrates satellite data with mathematical equations that represent physical processes in the atmosphere.

The animation shows dust plumes originating in northwestern Africa being blown both to the west across the Atlantic Ocean and north toward the Mediterranean. As plumes spread throughout Western Europe over several days, people observed hazy skies from southern England, where sunrises and sunsets took on an eerie glow, to the Alps in Switzerland and Italy, where a dust layer encroached on the Matterhorn.

Not all of the dust remained aloft. Storms encountered some of the dust, causing particles to fall to the ground with rain and coat surfaces with a brownish residue. A low-pressure system, named Storm Regina by Portugal’s weather service, moved across the Iberian Peninsula and brought so-called blood rain to southern and eastern Spain, along with parts of France and the southern UK in early March, according to news reports.

Over the Mediterranean, areas of “dusty cirrus” clouds developed higher in the atmosphere, where dust particles can act as condensation nuclei for ice crystals, according to MeteoSwiss, Switzerland’s Federal Office for Meteorology and Climatology. Scientists are studying these clouds to better understand their formation and how they affect weather, climate, and even solar power generation.

In a new analysis, researchers used NASA’s MERRA-2 (Modern-Era Retrospective Analysis for Research and Applications, Version 2), observations from MODIS (Moderate Resolution Imaging Spectroradiometer), and other satellite products to parse the effect of airborne Saharan dust on solar power in Hungary. They found that photovoltaic performance dropped to 46 percent on high-dust days, compared with 75 percent or more on low-dust days. They determined the greatest losses occurred because dust enhanced the presence and reflectance of cirrus clouds and reduced the amount of radiation that reached solar panels.

Some research suggests more frequent and intense wintertime dust events have affected Europe in recent years. Researchers have proposed several factors contributing to these outbreaks, including drier-than-normal conditions in northwestern Africa and weather patterns more often driving winds north from the Sahara.

NASA Earth Observatory animation by Lauren Dauphin, using GEOS-FP data from the Global Modeling and Assimilation Office at NASA GSFC. Story by Lindsey Doermann.

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Eruption at Mayon

Science Earth Observatory Eruption at Mayon Earth Earth Observatory Image of the Day EO Explorer All Topics Atmospher...