OrbitalHub

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When NASA’s Space Launch System (SLS) powers into the sky, it must contend with some of the most extreme and complex aerodynamic conditions ever attempted. The ascent phase—especially during transonic and supersonic transitions and through maximum aerodynamic stress—is a crucible for design and engineering. Rather than rely solely on wind tunnels, NASA has increasingly turned to supercomputer-based computational fluid dynamics (CFD) simulations to model the flows around the twin solid rocket boosters, the core stage, and plume interactions. These simulations feed into aerodynamic databases used across vehicle design, structural loads, control algorithms, and safety margins.

The challenge in modeling the flow around SLS boosters is immense. As the vehicle accelerates, shock waves form, flow separation regions emerge, boundary layers evolve, and the rocket plumes themselves strongly interact with the surrounding airstream. Moreover, during events like booster separation, multiple plumes fire simultaneously—up to 22 different exhaust sources in some analyses, combining output from the core engines, boosters, and separation motors. Resolving those off-body interactions, transient flow features, and the coupling between vehicle aerodynamics and plume dynamics demands very high fidelity simulations. The NASA team has used solvers such as OVERFLOW, FUN3D, and Cart3D to explore a wide envelope of flight conditions.

Running these simulations requires massive computational resources. Each case can consume thousands to tens of thousands of core-hours, depending on flow complexity, grid resolution, and the number of interacting plumes. To build a full aerodynamic database that spans multiple Mach numbers, angles of attack, mass fractions, and thrust conditions, NASA runs hundreds to thousands of individual cases. The supercomputers at the NASA Advanced Supercomputing (NAS) facility, including Pleiades, Electra, and others, serve as the backbone of these efforts. Through careful meshing strategies, solver optimizations, and parallel computing techniques, engineers map out pressure distributions, shear stresses, and load profiles for every relevant component of the booster-core assembly.

These simulation results are not academic exercises—they directly inform the safety and performance of SLS missions. The aerodynamics databases are used by structural engineers to assess bending loads, by guidance and control teams to refine trajectory models, and by separation system designers to ensure that boosters detach cleanly without risking collision with the core. When flight data come in, the models themselves can be validated and refined, closing the loop between simulation and real world performance. As SLS evolves—especially with future variants and heavier payloads—the simulation infrastructure will scale accordingly, enabling continuous improvements in confidence, margin, and mission success.

Video credit: NASA/NAS/Gerrit-Daniel Stich, Michael Barad, Timothy Sandstrom, Derek Dalle

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Early on the morning of September 24, 2025, a SpaceX Falcon 9 rocket thundered off Pad 39A at Kennedy Space Center, carrying into space a powerful trio: NASA’s Interstellar Mapping and Acceleration Probe (IMAP), the Carruthers Geocorona Observatory, and NOAA’s SWFO-L1 (Space Weather Follow On – Lagrange 1). The launch marked a bold new chapter in humanity’s efforts to monitor and understand the Sun’s influence across the solar system. The weather was nearly perfect—a 90 percent favorable forecast—and the three spacecraft were stacked together in a “cosmic carpool” bound for a vantage point some 1.6 million kilometers from Earth, at the L1 Lagrange point between the Sun and Earth.

IMAP is the centerpiece of the mission package. Designed to probe the boundary of the heliosphere—the region where the solar wind collides with the interstellar medium—it will sample energetic particles streaming outward from the Sun and inward from beyond, charting the invisible frontier that shields our solar system from cosmic rays. Its array of ten instruments includes devices to detect solar wind electrons, energetic ions, interstellar dust, and magnetic fields, among others. IMAP will also provide near–real-time data useful for space weather prediction, offering up to thirty minutes of advance warning for harmful solar radiation events.

Accompanying IMAP is the Carruthers Geocorona Observatory, a smaller NASA payload dedicated to observing the Earth’s exosphere—the tenuous outermost layer of our atmosphere. From its L1 vantage point, Carruthers will use ultraviolet imaging to monitor the geocorona’s glow, revealing how it responds to solar storms and seasonal changes. The mission is named in honor of George Carruthers, a pioneering space physicist and ultraviolet astronomer.

Meanwhile, NOAA’s SWFO-L1 is the operational arm of this venture, designed for continuous, real-time space weather monitoring. With instruments including a solar wind plasma sensor, magnetometer, and coronagraph, SWFO-L1 will keep watch on solar emissions and storms that could affect Earth’s satellites, communications networks, power grids, and crewed missions beyond low Earth orbit.

Following liftoff, the mission deployment sequence unfolded about 83 minutes later, with IMAP separating first, followed by Carruthers and SWFO-L1 in carefully timed intervals. Engineers expected to receive IMAP’s first signal roughly ten minutes after deployment, while Carruthers’ communications would follow about half an hour later. All spacecraft are destined for halo orbits around L1, providing unobstructed views of solar activity and the heliosphere’s edge.

This launch is more than a technological feat—it’s a leap toward safeguarding life and infrastructure on Earth, as well as deepening our knowledge of how the Sun, Earth, and the galaxy interact. In the coming months and years, IMAP, Carruthers, and SWFO-L1 will collectively map invisible space weather dynamics, chart the Sun’s magnetic bubble, monitor the Earth’s exosphere, and provide vital data for future human missions venturing beyond our planet.

Video credit: NASA/SpaceX

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On August 26, 2025, SpaceX finally pushed its Starship system through a full, ambitious test flight that many in the space-community had long awaited. After a series of earlier mishaps and scrapped attempts, the tenth integrated flight test marked a turning point: the vehicle performed a full-duration ascent burn, reached its planned velocity, deployed test payloads, and survived a fiery reentry before splashing down as intended.

The flight began from Starbase, Texas, with the Super Heavy booster igniting all 33 Raptor engines for launch. After climbing to altitude, Starship’s upper stage (Ship 37) separated and ignited its six engines, continuing on a suborbital trajectory.

During its coast phase, it deployed eight Starlink simulator payloads—marking the first time Starship successfully released a mock satellite mass during a test flight.

The upper stage also accomplished a Raptor engine relight in space, a key demonstration for future deorbit or orbit-raising maneuvers.

As the vehicle reentered Earth’s atmosphere, Starship faced some stress and damage—particularly in the aft skirt and in sections of its heat-shield and flaps.

Despite these challenges, the spacecraft managed a controlled “flip” maneuver, guiding itself nose-first toward the splashdown zone in the Indian Ocean.

Meanwhile, the booster executed a series of burns to reverse course, though it intentionally disabled one of its center engines during the landing burn as part of testing engine-out capability. It hovered briefly over the water before cutting engines and splashing in the Gulf of Mexico, where it broke up on impact.

While not perfect, Flight 10 delivered on many of its critical test objectives. The mission pushed Starship closer to full reusability, validated maneuvers needed for future missions, and restored confidence in the system after earlier failures.

The success of payload deployment and engine relighting in space stand out as especially important steps for upcoming missions to orbit and beyond. Challenges remain—especially refining heat-shield durability, improving structural margins during reentry, and achieving consistent booster recoveries. But the trajectory is now clearer: if the lessons from Flight 10 are applied well, Starship may well be on its way to realizing SpaceX’s goals for lunar, Martian, and deep-space missions.

Video credit: SpaceX

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Axiom Mission 4 (Ax-4) is currently unfolding as a landmark mission in the ongoing expansion of commercial spaceflight. Organized by Axiom Space, in partnership with NASA and SpaceX, Ax-4 is the fourth private astronaut mission to the International Space Station (ISS) and is part of NASA’s Commercial Low Earth Orbit Development program. As the line between government and private spaceflight continues to blur, Ax-4 is demonstrating what multinational, commercially driven space exploration looks like in practice.

Ax-4 launched aboard a SpaceX Falcon 9 rocket from Launch Complex 39A at NASA’s Kennedy Space Center in Florida, carrying the Crew Dragon Freedom spacecraft. After a successful launch and orbital insertion, the spacecraft docked with the ISS, beginning an approximately two-week mission in low Earth orbit.

The Ax-4 crew is led by Peggy Whitson, a former NASA astronaut and Axiom’s Director of Human Spaceflight. Whitson, who holds the U.S. record for cumulative days in space, brings unmatched experience and leadership to the mission. She is joined by three private astronauts representing the emerging generation of global space explorers:

Shubhanshu Shukla (India), a payload specialist and biomedical researcher.

Sławosz Uznański-Wiśniewski (Poland), a European Space Agency (ESA) reserve astronaut and nuclear physicist.

Tibor Kapu (Hungary), a flight and aerospace engineer.

Together, the crew represents a powerful combination of scientific, medical, and operational expertise, with participation from multiple national space programs and agencies.

Ax-4 plays a vital role in the commercialization of low Earth orbit. It serves as a live test case for integrating international and non-agency astronauts into the ISS framework—something that NASA sees as essential to its future LEO strategy. The mission supports NASA’s plan to transition routine orbital operations to commercial providers by the end of the decade, freeing government resources for Artemis missions and Mars exploration.

Furthermore, Ax-4 directly contributes to Axiom Space’s long-term vision of building Axiom Station, a free-flying commercial space station currently under development. Lessons from Ax-4—ranging from crew logistics to science payload management—inform Axiom’s engineering and operational planning for launching its first module, which will initially attach to the ISS before eventually separating into an independent platform.

This mission also sets a precedent for international inclusion in crewed spaceflight. Shubhanshu Shukla’s participation highlights India’s growing role in the commercial space sector, while Sławosz Uznański-Wiśniewski represents a step forward for ESA’s reserve astronaut program. Tibor Kapu’s presence underscores Hungary’s commitment to reentering human spaceflight after decades of absence.

The international nature of Ax-4 reinforces Axiom Space’s role as a facilitator of access to orbit for nations that lack launch capabilities or domestic astronaut corps. By enabling sovereign astronauts to fly as mission specialists, Axiom broadens the scope of participation in space exploration and science.

As Ax-4 continues, the mission is collecting critical data—not just from its scientific payloads, but from the structure and coordination of commercial spaceflight itself. The success of this mission will help define best practices for future mixed-nationality crews, commercial research operations, and astronaut training.

Looking forward, Axiom Mission 5 (Ax-5) is already in planning for 2025, expected to feature even more ambitious goals in terms of duration, research, and international collaboration. As commercial spaceflight moves from novelty to infrastructure, missions like Ax-4 will be remembered as formative efforts that redefined how, and by whom, space is explored.

Video credit: NASA

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Recent planetary geology research has brought significant attention to peculiar surface features on Mars known as boxwork formations. These geological structures, first identified in terrestrial caves like those of Wind Cave National Park in South Dakota, are intricate networks of intersecting ridges that form angular, often polygonal patterns on rock surfaces. On Mars, these formations provide intriguing evidence of the planet’s aqueous and diagenetic history, and they continue to fuel ongoing debates about Mars’ past habitability and climate.

Boxwork formations on Mars refer to polygonal or lattice-like patterns of raised ridges that commonly appear to crisscross the surface of sedimentary rocks. They are most often observed in eroded areas where the surrounding, less-resistant matrix has been stripped away, leaving behind the more resilient mineralized veins. These features resemble fossilized skeletons of a once-buried fracture network, now exposed by aeolian (wind-driven) erosion. The ridges are typically centimeters to meters in height and can span several meters in length, forming grid- or honeycomb-like patterns.

Boxwork-like features were first clearly documented on Mars by high-resolution imaging instruments aboard NASA’s Mars Reconnaissance Orbiter (MRO), particularly by the High Resolution Imaging Science Experiment (HiRISE) and the Context Camera (CTX). Notable observations include:

Gale Crater, explored by the Curiosity rover, where polygonal fracture patterns in sedimentary rocks were observed and interpreted as evidence of past fluid movement through rock.

Nilosyrtis region and Northeast Syrtis, both imaged by HiRISE, show spectacular examples of boxwork-like ridges.

Murray Buttes, inside Gale Crater, features boxwork textures that suggest extensive fracture-filling and mineral precipitation processes.

More recently, the Perseverance rover, exploring Jezero Crater since 2021, has detected similar linear ridges within ancient deltaic deposits, although their exact classification as boxwork is still under study.

These features are often associated with hydrated minerals, especially sulfates and clays, suggesting an interaction between water and rock over extended periods.

The most widely accepted model for the formation of boxwork on Mars involves mineral-filled fractures, a process consistent with what is observed in analogous terrestrial environments. The prevailing theory includes several key stages:

Fracturing of Host Rock: Martian bedrock, likely composed of volcanic or sedimentary materials, develops a network of fractures due to tectonic stress, desiccation (drying), or thermal contraction.

Fluid Infiltration and Mineral Precipitation: Subsurface fluids, likely brines or groundwater, percolate through the fractures, depositing minerals such as hematite, silica, sulfates, or carbonates along the walls of the fractures.

Cementation: Over time, these mineral deposits harden and cement the fracture walls.

Erosion of Host Matrix: Wind erosion or chemical weathering preferentially removes the surrounding, softer rock, leaving behind the more resistant mineral veins as raised ridges—creating the boxwork pattern.

In some cases, researchers hypothesize that the mineralization may have occurred during early diagenesis (sediment-to-rock transformation), potentially linked to hydrothermal systems or long-standing subsurface aquifers. The distribution and composition of these ridges support the idea that groundwater was once active and persistent in Martian history.

Boxwork structures are crucial for reconstructing Mars’ environmental history. They serve as indirect evidence for past water activity and reveal subsurface fluid pathways, potentially pointing to habitats that could have supported microbial life. Their mineralogical composition, especially when hydrated phases are present, offers insights into the chemical conditions that prevailed during their formation.

Moreover, the preservation of such delicate structures indicates limited subsequent geological disturbance, suggesting that some regions on Mars have remained relatively unchanged for billions of years. As such, they are prime targets for future in-situ analysis and sample return missions, especially those seeking biosignatures or geochemical proxies of past life.

Video credit: NASA Jet Propulsion Laboratory

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When Firefly Aerospace and Northrop Grumman joined forces, they sparked the creation of Eclipse—a medium-lift rocket that stands at the cutting edge of launch innovation. Announced in 2022 under the working name “Beta” or “MLV,” Eclipse was envisioned not just as a successor to Northrop’s Antares and Firefly’s Alpha rockets, but as a leap forward in reusability, performance, and production efficiency.

From its inception, Eclipse has been designed to bring a powerful payload capacity to low Earth orbit—an impressive 16,300 kilograms—as well as the ability to loft 3,200 kilograms to geosynchronous transfer orbits and 2,300 kilograms on lunar trajectories. The rocket’s 59-meter-tall frame, built from lightweight carbon-fiber composites, carries a sprawling 5.4-meter-diameter fairing—giving it both muscle and versatility.

The magic inside Eclipse lies in its propulsion system. The first stage supports seven Miranda engines—descendants of Firefly’s Alpha-series Reaver and Lightning family—each running on RP‑1 and liquid oxygen through a refined tap-off combustion cycle. Together, they push out over 7,160 kN of thrust with a vacuum specific impulse of 305 seconds.

Beyond raw power, Eclipse is engineered for reusability. Its first stage is built to return to the launch site after deployment—a configuration that aligns Eclipse with the reusable strategies pioneered by rockets like SpaceX’s Falcon 9 and Blue Origin’s New Glenn . Testing is already well underway, with more than sixty hot-fire tests of Miranda engines and a full 206-second mission duty cycle burn completed, matching projected flight conditions.

The blend of technologies aboard Eclipse is a deliberate fusion of legacy and innovation. The avionics system draws directly from Northrop’s flight-proven Antares platform, while the carbon-composite airframe and tap-off engine cycle are honed from Firefly’s work on Alpha. This synergy has already attracted a major vote of confidence in the form of a $50 million investment from Northrop Grumman, aimed at accelerating hardware production and qualification campaigns.

Eclipse’s versatility extends beyond the engineering lab to the launchpad. Wallops Island, Virginia’s Mid-Atlantic Regional Spaceport (LP‑0A) has been designated as its primary launch site, with alternate configurations ready at Vandenberg’s SLC‑2W and Cape Canaveral’s SLC‑20. What makes Eclipse particularly compelling is the market niche it fills. With a payload capacity of some 16 metric tons to LEO, it strikes a balance between heft and cost that suits emerging satellite constellations, space station supply missions, national security payloads, and science platforms alike.

For U.S. national security, the timing is right: Eclipse is lined up for consideration under the Space Force’s NSSL Phase 3 Lane 1, which prioritizes newer medium-class rockets. Behind the scenes, the factories in central Texas are humming. Firefly has doubled its production space in Briggs, Texas, to support both Antares 330 and Eclipse vehicle assembly. Mirrored in Wallops and Vandenberg, these facilities are designed for speed and scalability, with testing, machining, and composite fabrications all co-located.

Video credit: Northrop Grumman