The Polar Night Nitric Oxide or PolarNOx experiment from Virginia Tech is launched aboard a NASA Black Brant IX sounding rocket at 8:45 a.m. EST, Jan. 27, from the Poker Flat Research Range in Alaska. PolarNOx is measuring nitric oxide in the polar night sky. Nitric oxide in the polar night sky is created by auroras. Under appropriate conditions it can be transported to the stratosphere where it may destroy ozone resulting in possible changes in stratospheric temperature and wind and may even impact the circulation at Earth’s surface. Credit: NASA/Wallops/Jamie Adkins <b><a href="http://www.nasa.gov/audience/formedia/features/MP_Photo_Guidelines.html" rel="nofollow">NASA image use policy.</a></b> <b><a href="http://www.nasa.gov/centers/goddard/home/index.html" rel="nofollow">NASA Goddard Space Flight Center</a></b> enables NASA’s mission through four scientific endeavors: Earth Science, Heliophysics, Solar System Exploration, and Astrophysics. Goddard plays a leading role in NASA’s accomplishments by contributing compelling scientific knowledge to advance the Agency’s mission. <b>Follow us on <a href="http://twitter.com/NASAGoddardPix" rel="nofollow">Twitter</a></b> <b>Like us on <a href="http://www.facebook.com/pages/Greenbelt-MD/NASA-Goddard/395013845897?ref=tsd" rel="nofollow">Facebook</a></b> <b>Find us on <a href="http://instagrid.me/nasagoddard/?vm=grid" rel="nofollow">Instagram</a></b>
Dr. Jennifer Williams, a NASA research chemical engineer, is inside the Prototype Development Laboratory at NASA’s Kennedy Space Center in Florida to begin testing on the Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) project on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a 10 percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied to spacecraft and launch vehicles.
Dr. Jennifer Williams, a NASA research chemical engineer, displays two fatigue samples that will be tested in the Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) experiments inside the Prototype Laboratory at NASA’s Kennedy Space Center in Florida on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a 10 percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied to spacecraft and launch vehicles.
Gerard Moscoso, a mechanical engineer technician with NASA, handles a sample that is being prepared for fatigue and corrosion testing for the Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) project inside the Prototype Development Laboratory at NASA’s Kennedy Space Center in Florida on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a ten percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied on spacecraft and launch vehicles.
Testing of the Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) experiment is underway inside the Prototype Development Laboratory at NASA’s Kennedy Space Center in Florida on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a ten percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied on spacecraft and launch vehicles.
Gerard Moscoso, a mechanical engineer technician with NASA, prepares the Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) specimens for testing inside the Prototype Development Laboratory at NASA’s Kennedy Space Center in Florida on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a 10 percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied on spacecraft and launch vehicles.
Gerard Moscoso, a mechanical engineer technician with NASA, prepares a sample for testing for the Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) project inside the Prototype Development Laboratory at NASA’s Kennedy Space Center in Florida on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a 10 percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied on spacecraft and launch vehicles.
From left, Dr. Jennifer Williams, a NASA research chemical engineer, and Gerard Moscoso, a mechanical engineer technician, inspect specimens prepared forthe Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) experiment inside the Prototype Development Laboratory at NASA’s Kennedy Space Center in Florida on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a 10 percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied used on spacecraft and launch vehicles.
Testing of the Plasma Rapid Oxidation Technique for Extending Component Tenability (PROTECT) experiment is underway inside the Prototype Development Laboratory at NASA’s Kennedy Space Center in Florida on Nov. 2, 2022. Plasma electrolytic oxidation is a surface coating technology that produces oxide layers on the surface of light metals and their alloys to improve their performance characteristics. These coatings are tailored to provide a combination of characteristics such as corrosion protection, wear resistance, thermal management, extreme hardness, and fatigue performance. PROTECT is expected to demonstrate a 10 percent improved fatigue performance and a 70 percent improvement in corrosion characteristics on the interior of treated 3-D printed metallic parts when compared to non-treated parts. PROTECT could be applied on spacecraft and launch vehicles.
Macro Photographs of 3D Print of NASA Meatball - Made out of GRX-810, an Oxide Dispersion Strengthened (ODS) High Temperature Alloy
This image from the Microwave Limb Sounder instrument on NASA Aura spacecraft depicts the relationship between nitrous oxide levels and ozone loss, 2004-2005 Arctic winter.
An ammonia oxidation plant at the Plum Brook Ordnance Works near Sandusky, Ohio, which later became the National Aeronautics and Space Administration’s (NASA) Plum Brook Station. During World War II the ordnance works produced trinitroluene (TNT), dinitrotoluene (DNT), and pentolite which were crated and shipped to an arsenal in Ravenna, Ohio. There, the explosives were packed into shells and sent to Allied forces overseas. Plum Brook was the third largest producer of TNT during World War II. Toluene, sulfuric acid, and nitric acid were used to manufacture the TNT. Nitric Acid is made by oxidizing ammonia, adding water, and concentrating it. The facility in this photograph was used for this oxidation. The structure included air compressors, filters, aftercoolers, power recovery systems, air receivers, heaters, ammonia gasifiers, gas mixers, cooler condensers, absorption columns, and bleaching columns. The Plum Brook Ordnance Works was shut down immediately after the war and remained vacant for the next ten years. NASA’s predecessor, the National Advisory Committee for Aeronautics (NACA), acquired the 500 acres of the site in 1955 to build a nuclear test reactor. By 1963, the agency had acquired the entire 9000 acres from the Army. Almost all of the military facilities were removed in the early 1960s. Plum Brook Station contained over 30 test facilities at its peak in the late 1960s. Today there are four major facilities in operation.
NASA Curiosity Mars rover used the Dust Removal Tool on its robotic arm to brush aside reddish, more-oxidized dust, revealing a gray patch of less-oxidized rock material at a target called Bonanza King, visible from the rover Mastcam.
Water vapor surges from the flame deflector of the A-2 Test Stand at NASA's Stennis Space Center on Jan. 9 during the first space shuttle main engine test of the year. The test was an engine acceptance test of flight engine 2058. It's the first space shuttle main engine to be completely assembled at Kennedy Space Center. Objectives also included first-time (green run) tests of a high-pressure oxidizer turbo pump and an Advanced Health System Monitor engine controller. The test ran for the planned duration of 520 seconds.
This diagram presents some of the processes and clues related to a long-ago lake on Mars that became stratified, with the shallow water richer in oxidants than deeper water was. The sedimentary rocks deposited within a lake in Mars' Gale Crater more than three billion years ago differ from each other in a pattern that matches what is seen in lakes on Earth. As sediment-bearing water flows into a lake, bedding thickness and particle size progressively decrease as sediment is deposited in deeper and deeper water as seen in examples of thick beds (PIA19074) from shallowest water, thin beds (PIA19075) from deeper water and even thinner beds (PIA19828) from deepest water. At sites on lower Mount Sharp, inside the crater, measurements of chemical and mineral composition by NASA's Curiosity Mars rover reveal a clear correspondence between the physical characteristics of sedimentary rock from different parts of the lake and how strongly oxidized the sediments were. Rocks with textures indicating that the sediments were deposited near the edge of a lake have more strongly oxidized composition than rocks with textures indicating sedimentation in deep water. For example, the iron mineral hematite is more oxidized than the iron mineral magnetite. An explanation for why such chemical stratification occurs in a lake is that the water closer to the surface is more exposed to oxidizing effects of oxygen in the atmosphere and ultraviolet light. On Earth, a stratified lake with a distinct boundary between oxidant-rich shallows and oxidant-poor depths provides a diversity of environments suited to different types of microbes. If Mars has ever hosted microbial live, the stratified lake at Gale Crater may have similarly provided a range of different habitats for life. https://photojournal.jpl.nasa.gov/catalog/PIA21500
This scene shows NASA's Curiosity Mars rover at a location called "Windjana," where the rover found rocks containing manganese-oxide minerals, which require abundant water and strongly oxidizing conditions to form. In front of the rover are two holes from the rover's sample-collection drill and several dark-toned features that have been cleared of dust (see inset images). These flat features are erosion-resistant fracture fills containing manganese oxides. The discovery of these materials suggests the Martian atmosphere might once have contained higher abundances of free oxygen than it does now. The rover used the Mars Hand Lens Imager (MAHLI) camera in April and May 2014 to take dozens of images that were combined into this self-portrait. http://photojournal.jpl.nasa.gov/catalog/PIA20752
Solid Oxide Electrolizer, SOE
This plot segregates various minerals examined by NASA Mars Exploration Rover Opportunity according to their different compositions; for example, those with more iron and magnesium oxides are located in the lower right corner.
Nitrogen mineralization (Nitrous Oxide Flux): Fertile Forest
cutaway Rockwell International Space Shuttle Main Engines: Powerhead (Left side - fuel preburner, fuel trubopump - Center - Main Combustion Chamber, nozzle forward manifold - Right side - oxidizer preburner, oxidizer turbopump, preburner boost pump)
An illustration of MOXIE (Mars Oxygen ISRU Experiment) and its components. An air pump pulls in carbon dioxide gas from the Martian atmosphere, which is then regulated and fed to the Solid OXide Electrolyzer (SOXE), where it is electrochemically split to produce pure oxygen. https://photojournal.jpl.nasa.gov/catalog/PIA24177
A 3 mm-diameter droplet of aluminum oxide, heated to 2371 deg. C (4,300 deg. F), is suspended in midair by six acoustic transducers. A gas jet (from the nozzle below the drop) helps position the drop for study, and a 500-watt laser melts the sample. Glasses made from aluminum oxide are highly promising for optical transmission and other properties. They are also highly reactive when molten. Containerless processing allows studies of how to form amorphous (glassy) rather than crystalline metal oxides. Credit: Bill Jellison, Containerless Research, Inc.
iss060e015022 (7/28/2019) — NASA astronaut Nick Hague is shown holding the Perfect Crystals investigation samples within Styrofoam containers in Node 3 aboard the International Space Station (ISS). Growth of Large, Perfect Protein Crystals for Neutron Crystallography (Perfect Crystals) crystallizes human manganese superoxide dismutase in order to analyze its shape. This sheds light on how the antioxidant protein helps protect the human body from oxidizing radiation and oxides created as a byproduct of metabolism.
Some key components of a NASA-funded instrument being developed for the payload of the European Space Agency ExoMars mission stand out in thisillustration of the instrument
ISS033-E-009153 (2 Oct. 2012) --- Japan Aerospace Exploration Agency astronaut Aki Hoshide, Expedition 33 flight engineer, performs a removal and replacement of the DKiV water pump and the E-K pre-treat tank with its hose in the Tranquility node of the International Space Station. E-K contains five liters of pre-treat solution, i.e., a mix of H2SO4 (sulfuric acid), CrO3 (chromium oxide, for oxidation and purple color) and H2O (water). The pre-treat liquid is mixed with water in the DKiV dispenser and used for toilet flushing.
A laboratory-created "chemical garden" made of a combination of black iron sulfide and orange iron hydroxide/oxide is shown in this photo. Chemical gardens are a nickname for chimney-like structures that form at bubbling vents on the seafloor. Some researchers think that life may have originated at structures like these billions of years ago. JPL's research team is part of the Icy Worlds team of the NASA Astrobiology Institute, based at NASA's Ames Research Center in Moffett Field, California. JPL is managed by the California Institute of Technology in Pasadena for NASA. http://photojournal.jpl.nasa.gov/catalog/PIA19835
iss050e035112 (1/24/2017) --- NASA astronaut Shane Kimbrough completing the Multi-user Droplet Combustion Apparatus (MDCA) reconfiguration to the Cool Flames Investigation (CFI) setup. The Combustion Integrated Rack (CIR) includes an optics bench, combustion chamber, fuel and oxidizer control, and five different cameras for performing combustion experiments in microgravity.
Dr. Richard Weber and Ms. Emma Clark from Materials Development Inc. during a visit to the MSFC electrostatic levitation (ESL) laboratory. Here they are preparing for ESL tests in support of Dr. Weber's NASA grant "Microgravity Investigation of Thermophysical Properties of Supercooled Molten Metal Oxides" (NNX17AH73G).
iss056e130654 (Aug. 10, 2018) --- The Combustion Integration Rack (CIR), pictured in its open configuration, is located in the U.S. Destiny laboratory module and includes an optics bench, combustion chamber, fuel and oxidizer control, and five different cameras for performing combustion experiments safely in microgravity.
At Launch Complex 34, Cape Canaveral Air Station, several studies are under way for groundwater cleanup of trichloroethylene at the site. Shown here is monitoring equipment for one of the methods, potassium permanganate oxidation. Concentrations of trichloroethylene solvent have been identified in the soil at the complex as a result of cleaning methods for rocket parts during the Apollo Program in the 60s. The environmental research project involves the Department of Defense, Environmental Protection Agency, Department of Energy and NASA, who formed the Interagency NDAPL Consortium (IDC), to study three contamination cleanup technologies: Six Phase Soil Heating, Steam Injection and In Situ Oxidation with Potassium Permanganate. All three methods may offer a way to remove the contaminants in months instead of decades. KSC hosted a two-day conference that presented information and demonstrations of the three technologies for representatives from environmental and federal agencies
jsc2019e039830 (6/25/2019) --- A preflight photo taken as part of Nano Antioxidants experiment. C2C12 skeletal muscle cells grown in laboratory on Earth. Confocal microscopy image showing cytoskeletal actin in red, vinculin in green, and cell nuclei in blue. The experiment aims at elaborating antioxidant nanoparticle-based countermeasures to skeletal muscle loss occurring both in space and on Earth, in order to enable long-term human exploration of space and therapy of musculodegenerative diseases. Nanoparticles under study are composed of cerium oxide, that mimics natural defense against oxidative stress and shows long-lasting antioxidant effects. The aim of the Nano Antioxidants investigation is to research innovative approaches for cellular stimulation to counteract the negative effects of long-term microgravity on the musculoskeletal system. (Image courtesy of Dr. Gianni Ciofani, IIT and PoliTo)
At Launch Complex 34, Cape Canaveral Air Station, several studies are under way for groundwater cleanup of trichloroethylene at the site. Shown here is monitoring equipment for one of the methods, potassium permanganate oxidation. Concentrations of trichloroethylene solvent have been identified in the soil at the complex as a result of cleaning methods for rocket parts during the Apollo Program in the 60s. The environmental research project involves the Department of Defense, Environmental Protection Agency, Department of Energy and NASA, who formed the Interagency NDAPL Consortium (IDC), to study three contamination cleanup technologies: Six Phase Soil Heating, Steam Injection and In Situ Oxidation with Potassium Permanganate. All three methods may offer a way to remove the contaminants in months instead of decades. KSC hosted a two-day conference that presented information and demonstrations of the three technologies for representatives from environmental and federal agencies
ISS038-E-042754 (5 Feb. 2014) --- Japan Aerospace Exploration Agency astronaut Koichi Wakata, Expedition 38 flight engineer, works on the Combustion Integrated Rack (CIR) in the Destiny laboratory of the International Space Station. This research rack, which includes an optics bench, combustion chamber, fuel and oxidizer control and five different cameras, allows a variety of combustion experiments to be performed safely aboard the station.
iss066e095422 (Dec. 21, 2021) --- NASA astronaut and Expedition 66 Flight Engineer Raja Chari displays the half-opened Combustion Integrated Rack aboard the International Space Station's U.S. Destiny laboratory module. The research device includes an optics bench, combustion chamber, fuel and oxidizer control, and five different cameras for performing combustion investigations safely in microgravity.
ISS040-E-072228 (21 July 2014) --- In the International Space Station’s Destiny laboratory, NASA astronaut Reid Wiseman, Expedition 40 flight engineer, sets up the Combustion Integrated Rack (CIR) for more ground-commanded tests. This facility, which includes an optics bench, combustion chamber, fuel and oxidizer control and five different cameras, allows a variety of combustion experiments to be performed safely aboard the station.
Chuquicamata, in Chile's Atacama Desert, is the largest open pit copper mine in the world, by excavated volume. The copper deposits were first exploited in pre-Hispanic times. Open pit mining began in the early 20th century when a method was developed to work low grade oxidized copper ores. The image was acquired September 2, 2007, covers an area of 19.5 by 29.3 km, and is located at 22.1 degrees south, 68.9 degrees west. http://photojournal.jpl.nasa.gov/catalog/PIA20973
ISS040-E-072156 (21 July 2014) --- In the International Space Station’s Destiny laboratory, NASA astronaut Reid Wiseman, Expedition 40 flight engineer, sets up the Combustion Integrated Rack (CIR) for more ground-commanded tests. This facility, which includes an optics bench, combustion chamber, fuel and oxidizer control and five different cameras, allows a variety of combustion experiments to be performed safely aboard the station.
ISS038-E-042758 (5 Feb. 2014) --- Japan Aerospace Exploration Agency astronaut Koichi Wakata, Expedition 38 flight engineer, works on the Combustion Integrated Rack (CIR) in the Destiny laboratory of the International Space Station. This research rack, which includes an optics bench, combustion chamber, fuel and oxidizer control and five different cameras, allows a variety of combustion experiments to be performed safely aboard the station.
jsc2023e054753 (9/27/2023) --- Optical Coherence tomography image demonstrating the retinal ultrastructure of the mouse retina. Preclinical Validation of a Modifier Gene Therapy to Prevent Spaceflight Associated Oxidative Stress and Apoptosis in Microgravity Mouse Model of Dry Macular Degeneration (Rodent Research-28 or RR-28) tests the effect of a gene therapy on retinal structure and function during spaceflight. (Image courtesy Oculogenex Inc.)
jsc2023e054752 (9/27/2023) --- Fluorescein angiogram of the microvascular circulation of the mouse retina. Preclinical Validation of a Modifier Gene Therapy to Prevent Spaceflight Associated Oxidative Stress and Apoptosis in Microgravity Mouse Model of Dry Macular Degeneration (Rodent Research-28 or RR-28) tests the effect of a gene therapy on retinal structure and function during spaceflight. (Image courtesy Oculogenex Inc.)
ISS038-E-042747 (5 Feb. 2014) --- Japan Aerospace Exploration Agency astronaut Koichi Wakata, Expedition 38 flight engineer, works on the Combustion Integrated Rack (CIR) in the Destiny laboratory of the International Space Station. This research rack, which includes an optics bench, combustion chamber, fuel and oxidizer control and five different cameras, allows a variety of combustion experiments to be performed safely aboard the station.
iss049e003808 (9/15/2016) --- NASA astronaut Kate Rubins is photographed replacing two Multi-user Droplet Combustion Apparatus (MDCA) Igniter Tips as part of the Combustion Integration Rack (CIR) Igniter Replacement operations. The CIR is used to perform combustion experiments in microgravity. The CIR can be reconfigured easily on orbit to accommodate a variety of combustion experiments. It consists of an optics bench, a combustion chamber, a fuel and oxidizer management system, environmental management systems, and interfaces for science diagnostics and experiment specific equipment.
Structure Of Flame Balls At Low Lewis-numbers (SOFBALL) Experiment Mounting Structure (EMS) was used to conduct the SOFBALL experiment on Combustion Module-1. The EMS was inserted into the CM-1 combustion chamber. The chamber was filled with a lean fuel/oxidizer mixture and a spark igniter on the EMS ignited the gas. Very small, weak flames, in the shape of spheres, were formed and studied.
ISS040-E-071994 (21 July 2014) --- In the International Space Station’s Destiny laboratory, NASA astronaut Reid Wiseman, Expedition 40 flight engineer, sets up the Combustion Integrated Rack (CIR) for more ground-commanded tests. This facility, which includes an optics bench, combustion chamber, fuel and oxidizer control and five different cameras, allows a variety of combustion experiments to be performed safely aboard the station.
jsc2021e058716 (11/10/2021) --- A preflight image of Graphene oxide aqueous dispersion. Space-production of Lightweight 3D Graphene Aerogels ( SUBSA-ugGA ) examines graphene-based hydrogel production on Earth and in microgravity conditions, towards producing aerogels with improved microstructure uniformity and material properties for both Earth and space applications. Image courtesy of UC Berkeley, Prof. Maboudian.
The static firing of a Saturn F-1 engine at the Marshall Space Flight Center's Static Test Stand. The F-1 engine is a single-start, 1,5000,000 Lb fixed-thrust, bipropellant rocket system. The engine uses liquid oxygen as the oxidizer and RP-1 (kerosene) as fuel. The five-engine cluster used on the first stage of the Saturn V produces 7,500,000 lbs of thrust.
KENNEDY SPACE CENTER, FLA. -- An external tank is suspended in the transfer aisle of the Vehicle Assembly Building before being placed into its storage compartment. The largest and heaviest element of the Space Shuttle, an external tank contains the liquid hydrogen fuel and liquid oxygen oxidizer for the three Space Shuttle main engines (SSMEs) in the orbiter during liftoff and ascent. When the SSMEs are shut down, the external tank is jettisoned, breaking up as it enters the Earth's atmopshere and impacting in a remote ocean area. It is not recovered
KENNEDY SPACE CENTER, FLA. -- STS-114 Mission Specialist Soichi Noguchi looks closely at low pressure oxidizer duct in the Space Shuttle Main Engine Shop at KSC. He and other crew members are touring several areas on the Center. The STS-114 mission is Logistics Flight 1, which is scheduled to deliver supplies and equipment plus the external stowage platform to the International Space Station.
Hot Jupiters are exoplanets that orbit their stars so tightly that their temperatures are extremely high, reaching over 2,400 degrees Fahrenheit (1600 Kelvin). They are also tidally locked, so one side of the planet always faces the sun and the other is in permanent darkness. Research suggests that the "dayside" is largely free of clouds, while the "nightside" is heavily clouded. This illustration represents how hot Jupiters of different temperatures and different cloud compositions might appear to a person flying over the dayside of these planets on a spaceship, based on computer modeling. Cooler planets are entirely cloudy, whereas hotter planets have morning clouds only. Clouds of different composition have different colors, whereas the clear sky is bluer than on Earth. For the hottest planets, the atmosphere is hot enough on the evening side to glow like a charcoal. Figure 1 shows an approximation of what various hot Jupiters might look like based on a combination of computer modeling and data from NASA's Kepler Space Telescope. From left to right it shows: sodium sulfide clouds (1000 to 1200 Kelvin), manganese sulfide clouds (1200 to 1600 Kelvin), magnesium silicate clouds (1600 to 1800 Kelvin), magnesium silicate and aluminum oxide clouds (1800 Kelvin) and clouds composed of magnesium silicate, aluminum oxide, iron and calcium titanate (1900 to 2200 Kelvin). http://photojournal.jpl.nasa.gov/catalog/PIA21074
This graphic shows proportions of minerals identified in mudstone exposures at the "Yellowknife Bay" location where NASA's Curiosity Mars rover first analyzed bedrock, in 2013, and at the "Murray Buttes" area investigated in 2016. Minerals were identified by X-ray diffraction analysis of sample powder from the rocks. The samples were acquired by drilling and delivered to the Chemistry and Mineralogy (CheMin) instrument inside the rover. Two key differences in the Murray Buttes mudstone include hematite rather than magnetite, and far less abundance of crystalline mafic minerals, compared to the Yellowknife Bay mudstone composition. Hematite and magnetite are both iron oxide minerals, with hematite as a more oxidized one. That difference could result from the Murray Buttes mudstone layer experiencing more weathering than the Yellowknife Bay mudstone. More weathering could also account for the lower abundance of crystalline mafics, which are volcanic-origin minerals such as pyroxene and olivine. The Yellowknife Bay site is on the floor of Gale Crater. The Murray Buttes site is on lower Mount Sharp, the layered mound in the center of the crater. http://photojournal.jpl.nasa.gov/catalog/PIA21149
Climate researchers from the National Center for Atmospheric Research (NCAR) and several universities install and perform functional checkouts of a variety of sensitive atmospheric instruments on NASA's DC-8 airborne laboratory prior to beginning the ARCTAS mission.
Acquired on April 1, 2018, this image from NASA's Mars Reconnaissance Orbiter shows Aram Chaos, a 280 kilometer-diameter ancient impact crater that lies within in the Southern Highlands of Mars. Uplifted blocks of light-toned layers, composed largely of the iron-oxide hematite and water-altered silicates, indicate that this crater once held a lake. Scientists suggest that these enormous flood channels were carved quickly within just weeks or months by catastrophic outflows of groundwater over 2.5 billion years ago from beneath Aram Chaos and nearby regions. Today dark (basaltic) dunes fill most of the low regions and the etched areas of the uplifted blocks obscure much of the original crater floor. Aram Chaos is located near the headwaters of Ares Vallis, a large outflow channel system that extends about 1700 kilometers towards the northwest across the ancient cratered highlands before emptying into the Northern Lowlands at Chryse Planitia near the Mars Pathfinder landing site. More information is available at https://photojournal.jpl.nasa.gov/catalog/PIA22585
A crane and rigging lines are used to install the Interim Cryogenic Propulsion Stage Umbilical (ICPSU) high up on the mobile launcher (ML) at NASA's Kennedy Space Center in Florida. The last of the large umbilicals to be installed, the ICPSU will provide super-cooled hydrogen and liquid oxygen to the Space Launch System (SLS) rocket's interim cryogenic propulsion stage, or upper stage, at T-0 for Exploration Mission-1. The umbilical is located at about the 240-foot-level of the mobile launcher and will supply fuel, oxidizer, gaseous helium, hazardous gas leak detection, electrical commodities and environment control systems to the upper stage of the SLS rocket during launch. Exploration Ground Systems is overseeing installation of the umbilicals on the ML.
KENNEDY SPACE CENTER, FLA. -- Following the Flight Readiness Review for the STS-117 mission, NASA officials presented the decisions of NASA senior managers in a television conference. Bill Gerstenmaier, associate administrator of NASA Space Operations Mission, confirmed the launch time and date of Space Shuttle Atlantis at 7:38 p.m. EDT on June 8. Seen here is Space Shuttle Program Manager Wayne Hale (left) demonstrating the level of scrutiny engineers apply to inspecting the smallest of components that make up the shuttle system. This housing and bolt insert are part of the main engine low pressure oxidizer turbopump (LPOTP). Photo credit: NASA/Kim Shiflett
Mawrth Vallis is a place on Mars that has fascinated scientists because of the clays and other hydrated minerals detected from orbit. In this image, the enhanced black colors are most likely basaltic sands and rocks, while the green, yellow, and blue colors correspond to the different hydrated minerals. This particular image was taken of a location in Mawrth Vallis that has a mineral called jarosite. Jarosite on Earth forms under wet, oxidizing, and acidic conditions. Another place on Mars where the Opportunity rover landed and explored also has jarosite. https://photojournal.jpl.nasa.gov/catalog/PIA23080
The Mount Whaleback open pit iron ore mine is located 6 km west of the town of Newman in the Pilbara region of Western Australia. It is currently the fifth largest iron mine in the world. The iron occurs in banded iron ore formations, created about 2.5 billion years ago when microorganisms first produced massive amounts of oxygen, oxidizing and precipitating the free iron in the oceans. The image was acquired October 2, 2017, covers an area of 14.4 by 17 km, and is located at 23.3 degrees south, 119.7 degrees east. https://photojournal.jpl.nasa.gov/catalog/PIA24016
KENNEDY SPACE CENTER, FLA. -- In the transfer aisle of the Vehicle Assembly Building, Atlantis awaits a vacancy in one of the Orbiter Processing Facility bays. Seen behind the right wing is an external tank being raised to a vertical position. The largest and heaviest element of the Space Shuttle, an external tank contains the liquid hydrogen fuel and liquid oxygen oxidizer for the three Space Shuttle main engines (SSMEs) in the orbiter during liftoff and ascent. When the SSMEs are shut down, the external tank is jettisoned, breaking up as it enters the Earth's atmopshere and impacting in a remote ocean area. It is not recovered
In this image, the gold-plated Mars Oxygen In-Situ Resource Utilization Experiment (MOXIE) Instrument shines after being installed inside the Perseverance rover. The largest white tube on the top surface of MOXIE takes in filtered carbon dioxide-rich Martian atmosphere. That CO2 is pressurized and passed through the Solid Oxide Electrolysis unit, where it is split into carbon monoxide and oxygen. The smallest tube snaking across the top of the unit sends the oxygen produced by MOXIE through a composition sensor to measure purity, then vents the oxygen out to the Martian atmosphere. This technology demonstration may guide the design of future, larger devices that could enable human exploration of Mars. https://photojournal.jpl.nasa.gov/catalog/PIA24203
A recently installed fertilizer-producing system sits near Launch Pad 39A. Using a "scrubber," the system captures nitrogen tetroxide vapor that develops as a by-product when it is transferred from ground storage tanks into the Shuttle storage tanks. Nitrogen tetroxide is used as the oxidizer for the hypergolic propellant in the Shuttle's on-orbit reaction control system. The scrubber then uses hydrogen peroxide to produce nitric acid, which, after adding potassium hydroxide, converts to potassium nitrate, a commercial fertilizer. Plans call for the resulting fertilizer to be used on the orange groves that KSC leases to outside companies
The dart and associated launching system was developed by engineers at MSFC to collect a sample of the aluminum oxide particles during the static fire testing of the Shuttle's solid rocket motor. The dart is launched through the exhaust and recovered post test. The particles are collected on sticky copper tapes affixed to a cylindrical shaft in the dart. A protective sleeve draws over the tape after the sample is collected to prevent contamination. The sample is analyzed under a scarning electron microscope under high magnification and a particle size distribution is determined. This size distribution is input into the analytical model to predict the radiative heating rates from the motor exhaust. Good prediction models are essential to optimizing the development of the thermal protection system for the Shuttle.
A crane and rigging lines are used to install the Interim Cryogenic Propulsion Stage Umbilical (ICPSU) high up on the mobile launcher (ML) at NASA's Kennedy Space Center in Florida. The last of the large umbilicals to be installed, the ICPSU will provide super-cooled hydrogen and liquid oxygen to the Space Launch System (SLS) rocket's interim cryogenic propulsion stage, or upper stage, at T-0 for Exploration Mission-1. The umbilical is located at about the 240-foot-level of the mobile launcher and will supply fuel, oxidizer, gaseous helium, hazardous gas leak detection, electrical commodities and environment control systems to the upper stage of the SLS rocket during launch. Exploration Ground Systems is overseeing installation of the umbilicals on the ML.
STS103-728-022 (19-27 December 1999)--- One of the astronauts aboard the Earth-orbiting Space Shuttle Discovery used a handheld 70mm camera to photograph the Tifernine dunes (note, the dunes are below the "beak" of sandstone rock). According to NASA scientists studying the STS-103 photo collection, the dunes were created when the dark sandstone rocks trapped sand. Winds, they continued, then piled the sand into dunes up to 457.2 m (1,500 ft). The color of the sandstone is due to a desert varnish, the scientists reported. The varnish is composed of manganese, iron oxides, hydroxides, and clay minerals, they said.
KENNEDY SPACE CENTER, FLA. -- In the transfer aisle of the Vehicle Assembly Building, Atlantis awaits a vacancy in one of the Orbiter Processing Facility bays. Seen behind the left wing is an external tank being raised to a vertical position. The largest and heaviest element of the Space Shuttle, an external tank contains the liquid hydrogen fuel and liquid oxygen oxidizer for the three Space Shuttle main engines (SSMEs) in the orbiter during liftoff and ascent. When the SSMEs are shut down, the external tank is jettisoned, breaking up as it enters the Earth's atmopshere and impacting in a remote ocean area. It is not recovered
This STS-48 onboard photo is of the Upper Atmosphere Research Satellite (UARS) in the grasp of the RMS (Remote Manipulator System) during deployment, September 1991. UARS gathers data related to the chemistry, dynamics, and energy of the ozone layer. UARS data is used to study energy input, stratospheric photo chemistry, and upper atmospheric circulation. UARS helps us understand and predict how the nitrogen and chlorine cycles, and the nitrous oxides and halo carbons which maintain them, relate to the ozone balance. It also observes diurnal variations in short-lived stratospheric chemical species important to ozone destruction. Data from UARS enables scientists to study ozone depletion in the upper atmosphere.
Construction workers with JP Donovan assist with preparations to lift and install the Interim Cryogenic Propulsion Stage Umbilical on the tower of the mobile launcher at NASA's Kennedy Space Center in Florida. The last of the large umbilicals to be installed, the ICPSU will provide super-cooled hydrogen and liquid oxygen to the Space Launch System (SLS) rocket's interim cryogenic propulsion stage, or upper stage, at T-0 for Exploration Mission-1. The umbilical is located at about the 240-foot-level of the mobile launcher and will supply fuel, oxidizer, gaseous helium, hazardous gas leak detection, electrical commodities and environment control systems to the upper stage of the SLS rocket during launch. Exploration Ground Systems is overseeing installation of the umbilicals on the ML.
iss059e059071 (5/7/2019) --- Photo documentation of the 12 Nano Antioxidants Experiment Containers in Kubik 5 marking the start of the experiment run in the Columbus module aboard the International Space Station (ISS). The aim of the Nano Antioxidants investigation is to research innovative approaches for cellular stimulation to counteract the negative effects of long-term microgravity on the musculoskeletal system. There are numerous possible applications of this research project in other crucial social domains, such as healthcare of the elderly and of people with muscle atrophy disorders, through the implementation of new therapeutic strategies in the treatment of diseases involving oxidative stress as causing factor.
KENNEDY SPACE CENTER, FLA. -- A recently installed fertilizer-producing system sits near Launch Pad 39A (upper left background). Using a "scrubber," the system captures nitrogen tetroxide vapor that develops as a by-product when it is transferred from ground storage tanks into the Shuttle storage tanks. Nitrogen tetroxide is used as the oxidizer for the hypergolic propellant in the Shuttle's on-orbit reaction control system. The scrubber then uses hydrogen peroxide to produce nitric acid, which, after adding potassium hydroxide, converts to potassium nitrate, a commercial fertilizer. The black tanker at left is collecting the potassium nitrate, which will be used on the orange groves that KSC leases to outside companies
A crane and rigging lines are used to install the Interim Cryogenic Propulsion Stage Umbilical (ICPSU) high up on the mobile launcher (ML) at NASA's Kennedy Space Center in Florida. The last of the large umbilicals to be installed, the ICPSU will provide super-cooled hydrogen and liquid oxygen to the Space Launch System (SLS) rocket's interim cryogenic propulsion stage, or upper stage, at T-0 for Exploration Mission-1. The umbilical is located at about the 240-foot-level of the mobile launcher and will supply fuel, oxidizer, gaseous helium, hazardous gas leak detection, electrical commodities and environment control systems to the upper stage of the SLS rocket during launch. Exploration Ground Systems is overseeing installation of the umbilicals on the ML.
iss059e059049 (5/7/2019) --- Canadian Space Agency (CSA) astronaut David Saint-Jacques is photographed during the installation of the Nano Antioxidants Experiment Containers in Kubik 5 aboard the International Space Station (ISS). The aim of the Nano Antioxidants investigation is to research innovative approaches for cellular stimulation to counteract the negative effects of long-term microgravity on the musculoskeletal system. There are numerous possible applications of this research project in other crucial social domains, such as healthcare of the elderly and of people with muscle atrophy disorders, through the implementation of new therapeutic strategies in the treatment of diseases involving oxidative stress as causing factor.
KENNEDY SPACE CENTER, FLA. -- Clyde Parrish, a NASA/KSC engineer, explains how the fertilizer scrubber control panel (center) works to turn nitrogen tetroxide vapor into fertilizer, potassium hydroxide. Parrish developed the system, which uses a "scrubber," to capture nitrogen tetroxide vapor that develops as a by-product when it is transferred from ground storage tanks into the Shuttle storage tanks. Nitrogen tetroxide is used as the oxidizer for the hypergolic propellant in the Shuttle's on-orbit reaction control system. The scrubber then uses hydrogen peroxide to produce nitric acid, which, after adding potassium hydroxide, converts to potassium nitrate. The resulting fertilizer will be used on the orange groves that KSC leases to outside companies
CAPE CANAVERAL, Fla. – Inside the Engine Shop at NASA’s Kennedy Space Center in Florida, a technician performs a boroscope test on a high pressure oxidizer pump on one of the Pratt Whitney Rocketdyne space shuttle main engines (SSMEs) positioned in a test cell. For the first time, all 15 main engines are in the Engine Shop at the same time. They are being prepared for shipment to NASA's Stennis Space Center in Mississippi for storage following the completion of the Space Shuttle Program. The engines are being repurposed for use on NASA’s Space Launch System heavy lift rocket. Photo credit: NASA_Dimitri Gerondidakis
KENNEDY SPACE CENTER, FLA. -- A recently installed fertilizer-producing system sits near Launch Pad 39A (upper left background). Using a "scrubber," the system captures nitrogen tetroxide vapor that develops as a by-product when it is transferred from ground storage tanks into the Shuttle storage tanks. Nitrogen tetroxide is used as the oxidizer for the hypergolic propellant in the Shuttle's on-orbit reaction control system. The scrubber then uses hydrogen peroxide to produce nitric acid, which, after adding potassium hydroxide, converts to potassium nitrate, a commercial fertilizer. The black tanker at left is collecting the potassium nitrate, which will be used on the orange groves that KSC leases to outside companies
CAPE CANAVERAL, Fla. – Inside the Engine Shop at NASA’s Kennedy Space Center in Florida, a technician performs a boroscope test on a high pressure oxidizer pump on one of the Pratt Whitney Rocketdyne space shuttle main engines (SSMEs) positioned in a test cell. For the first time, all 15 main engines are in the Engine Shop at the same time. They are being prepared for shipment to NASA's Stennis Space Center in Mississippi for storage following the completion of the Space Shuttle Program. The engines are being repurposed for use on NASA’s Space Launch System heavy lift rocket. Photo credit: NASA_Dimitri Gerondidakis
KENNEDY SPACE CENTER, FLA. -- Clyde Parrish, a NASA/KSC engineer, explains how the fertilizer scrubber control panel (center) works to turn nitrogen tetroxide vapor into fertilizer, potassium hydroxide. Parrish developed the system, which uses a "scrubber," to capture nitrogen tetroxide vapor that develops as a by-product when it is transferred from ground storage tanks into the Shuttle storage tanks. Nitrogen tetroxide is used as the oxidizer for the hypergolic propellant in the Shuttle's on-orbit reaction control system. The scrubber then uses hydrogen peroxide to produce nitric acid, which, after adding potassium hydroxide, converts to potassium nitrate. The resulting fertilizer will be used on the orange groves that KSC leases to outside companies
The engineering model (EM), an almost identical twin of MOXIE, is used for testing in the lab at NASA's Jet Propulsion Laboratory in Pasadena, California. Inside this gold-plated aluminum box is the Solid Oxide Electrolysis unit, or SOXE, the heart of MOXIE. Using an electrochemical process called electrolysis, SOXE takes in the carbon dioxide gas and splits it into carbon monoxide and oxygen, which is measured for purity, filtered, and then released back into the Mars atmosphere. Tubes to take in the Mars atmosphere and vent oxygen and carbon monoxide produced by the EM are connected at the top of the EM. The electronics needed to run this complex machine are housed inside the larger sidewall seen on the right. https://photojournal.jpl.nasa.gov/catalog/PIA24201
This STS-48 onboard photo is of the Upper Atmosphere Research Satellite (UARS) in the grasp of the RMS (Remote Manipulator System) during deployment, September 1991. UARS gathers data related to the chemistry, dynamics, and energy of the ozone layer. UARS data is used to study energy input, stratospheric photo chemistry, and upper atmospheric circulation. UARS helps us understand and predict how the nitrogen and chlorine cycles, and the nitrous oxides and halo carbons which maintain them, relate to the ozone balance. It also observes diurnal variations in short-lived stratospheric chemical species important to ozone destruction. Data from UARS enables scientists to study ozone depletion in the upper atmosphere.
A recently installed fertilizer-producing system sits near Launch Pad 39A. Using a "scrubber," the system captures nitrogen tetroxide vapor that develops as a by-product when it is transferred from ground storage tanks into the Shuttle storage tanks. Nitrogen tetroxide is used as the oxidizer for the hypergolic propellant in the Shuttle's on-orbit reaction control system. The scrubber then uses hydrogen peroxide to produce nitric acid, which, after adding potassium hydroxide, converts to potassium nitrate, a commercial fertilizer. Plans call for the resulting fertilizer to be used on the orange groves that KSC leases to outside companies
The Chemistry and Camera (ChemCam) instrument on NASA's Curiosity Mars rover examined a freshly brushed area on target rock "Christmas Cove" and found spectral evidence of hematite, an iron-oxide mineral. ChemCam sometimes zaps rocks with a laser, but can also be used, as in this case, in a "passive" mode. In this type of investigation, the instrument's telescope delivers to spectrometers the sunlight reflected from a small target point. The upper-left inset of this graphic is an image from ChemCam's Remote Micro-Imager with five labeled points that the instrument analyzed. The image covers an area about 2 inches (5 centimeters) wide, and the bright lines are fractures in the rock filled with calcium sulfate minerals. The five charted lines of the graphic correspond to those five points and show the spectrometer measurements of brightness at thousands of different wavelengths, from 400 nanometers (at the violet end of the visible-light spectrum) to 840 nanometers (in near-infrared). Sections of the spectrum measurements that are helpful for identifying hematite are annotated. These include a dip around 535 nanometers, the green-light portion of the spectrum at which fine-grained hematite tends to absorb more light and reflect less compared to other parts of the spectrum. That same green-absorbing characteristic of the hematite makes it appear purplish when imaged through special filters of Curiosity's Mast Camera and even in usual color images. The spectra also show maximum reflectance values near 750 nanometers, followed by a steep decrease in the spectral slope toward 840 nanometers, both of which are consistent with hematite. This ChemCam examination of Christmas Cove was part of an experiment to determine whether the rock had evidence of hematite under a tan coating of dust. The target area was brushed with Curiosity's Dust Removal Tool prior to these ChemCam passive observations on Sept. 17, 2017, during the 1,819th Martian day, or sol, of Curiosity's work on Mars. https://photojournal.jpl.nasa.gov/catalog/PIA22068
Space Vacuum Epitaxy Center works with industry and government laboratories to develop advanced thin film materials and devices by utilizing the most abundant free resource in orbit: the vacuum of space. SVEC, along with its affiliates, is developing semiconductor mid-IR lasers for environmental sensing and defense applications, high efficiency solar cells for space satellite applications, oxide thin films for computer memory applications, and ultra-hard thin film coatings for wear resistance in micro devices. Performance of these vacuum deposited thin film materials and devices can be enhanced by using the ultra-vacuum of space for which SVEC has developed the Wake Shield Facility---a free flying research platform dedicated to thin film materials development in space.
CAPE CANAVERAL, Fla. – Pratt & Whitney Rocketdyne technicians align a space shuttle main engine for installation on space shuttle Endeavour in Orbiter Processing Facility Bay 2 at NASA's Kennedy Space Center in Florida. The engine will fly on the shuttle's STS-130 mission to the International Space Station. Even though this engine weighs one-seventh as much as a locomotive engine, its high-pressure fuel pump alone delivers as much horsepower as 28 locomotives, while its high-pressure oxidizer pump delivers the equivalent horsepower of an additional 11 locomotives. The maximum equivalent horsepower developed by the shuttle's three main engines is more than 37 million horsepower. Endeavour is targeted to launch Feb. 4, 2010. Photo credit: NASA/Jim Grossmann
This image of the Nili Fossae region, to the west of the great Isidis basin, shows layered bedrock with many impact craters. Nili Fossae is one of the most mineralogically important sites on Mars. Remote observations by the infrared spectrometer onboard MRO (called CRISM) suggest the layers in the ancient craters contain clays, carbonates, and iron oxides, perhaps due to hydrothermal alteration of the crust. However, the impact craters have been degraded by many millions of years of erosion so the original sedimentary, impact ejecta, or lava flows are hard to distinguish. The bright linear features are sand dunes, also known as "transverse aeolian dunes," because the wind direction is at ninety degrees to their elongated orientation. This shows that the erosion of Nili Fossae continues to the present day with sand-sized particles broken off from the local rocks mobilized within the dunes. https://photojournal.jpl.nasa.gov/catalog/PIA23452
The mobile launcher (ML) is reflected in the sunglasses of a construction worker with JP Donovan at NASA's Kennedy Space Center in Florida. A crane is lifting the Interim Cryogenic Propulsion Stage Umbilical (ICPSU) up for installation on the tower of the ML. The last of the large umbilicals to be installed, the ICPSU will provide super-cooled hydrogen and liquid oxygen to the Space Launch System (SLS) rocket's interim cryogenic propulsion stage, or upper stage, at T-0 for Exploration Mission-1. The umbilical is located at about the 240-foot-level of the mobile launcher and will supply fuel, oxidizer, gaseous helium, hazardous gas leak detection, electrical commodities and environment control systems to the upper stage of the SLS rocket during launch. Exploration Ground Systems is overseeing installation of the umbilicals on the ML.
Construction workers with JP Donovan install the Interim Cryogenic Propulsion Stage Umbilical (ICPSU) at about the 240-foot-level of the mobile launcher (ML) tower at NASA's Kennedy Space Center in Florida. The last of the large umbilicals to be installed, the ICPSU will provide super-cooled hydrogen and liquid oxygen to the Space Launch System (SLS) rocket's interim cryogenic propulsion stage, or upper stage, at T-0 for Exploration Mission-1. The umbilical is located at about the 240-foot-level of the mobile launcher and will supply fuel, oxidizer, gaseous helium, hazardous gas leak detection, electrical commodities and environment control systems to the upper stage of the SLS rocket during launch. Exploration Ground Systems is overseeing installation of the umbilicals on the ML.
The sinuous ridges in this image display strong characteristics of ancient meandering riverbeds that are preserved as inverted topography (blue). The ancient river sediments that make up the ridges might have allowed fluids to produce cements (e.g., calcite or iron oxides) to make the channel lithology resistant to weathering and erosion. Later, physical and/or chemical processes removed the weaker surrounding flood plain material and left inverted river channels, or "positive relief." On closer inspection, degradation along sections of some inverted channels display large blocks of cemented sediment that were transported downslope by mass wasting. The sinuous character of the ridges resembles multi-thread river branches, implying that the ancient river flowed down a gentle to nearly horizontal slope (i.e., a moderate to low stream gradient). This ancient river was a mature meandering system, with flow from south to north. Multiple branches that diverted from the main flow later converged back with it. http://photojournal.jpl.nasa.gov/catalog/PIA20210
On top of the block house at Launch Complex 34, representatives from environmental and Federal agencies hear from Laymon Gray, with Florida State University, about the environmental research project that involves the Department of Defense, Environmental Protection Agency, Department of Energy and NASA in a groundwater cleanup effort. Concentrations of trichloroethylene solvent have been identified in the soil at the complex as a result of cleaning methods for rocket parts during the Apollo Program, which used the complex, in the 60s. The group formed the Interagency NDAPL Consortium (IDC) to study three contamination cleanup technologies: Six Phase Soil Heating, Steam Injection and In Situ Oxidation with Potassium Permanganate. All three methods may offer a way to remove the contaminants in months instead of decades. In the background (left) can be seen the cement platform and walkway from the block house to the pad. Beyond it is the Atlantic Ocean. KSC hosted a two-day conference that presented information and demonstrations of the three technologies being tested at the site
At Launch Complex 34, representatives from environmental and Federal agencies head for the block house during presentations about the environmental research project that involves the Department of Defense, Environmental Protection Agency, Department of Energy and NASA in a groundwater cleanup effort. Concentrations of trichloroethylene solvent have been identified in the soil at the complex as a result of cleaning methods for rocket parts during the Apollo Program, which used the complex, in the 60s. The group formed the Interagency NDAPL Consortium (IDC) to study three contamination cleanup technologies: Six Phase Soil Heating, Steam Injection and In Situ Oxidation with Potassium Permanganate. All three methods may offer a way to remove the contaminants in months instead of decades. KSC hosted a two-day conference that presented information and demonstrations of the three technologies being tested at the site
The Apollo program demonstrated that men could travel into space, perform useful tasks there, and return safely to Earth. But space had to be more accessible. This led to the development of the Space Shuttle. The Shuttle's major components are the orbiter spacecraft; the three main engines, with a combined thrust of more than 1.2 million pounds; the huge external tank (ET) that feeds the liquid hydrogen fuel and liquid oxygen oxidizer to the three main engines; and the two solid rocket boosters (SRBs), with their combined thrust of some 5.8 million pounds, that provide most of the power for the first two minutes of flight. Crucially involved with the Space Shuttle program virtually from its inception, the Marshall Space Flight Center (MSFC) played a leading role in the design, development, testing, and fabrication of many major Shuttle propulsion components.
A hole, created by recent hail storms, is identified as number two on the surface of the external tank (ET) mated to Space Shuttle Discovery at Launch Pad 39B. Workers are investigating the damage and potential problems for launch posed by ice forming in the holes, which may number as many as 150 over the entire tank. The average size of the holes is one-half inch in diameter and one-tenth inch deep. The external tank contains the liquid hydrogen fuel and liquid oxygen oxidizer and supplies them under pressure to the three space shuttle main engines in the orbiter during liftoff and ascent. The ET thermal protection system consists of sprayed-on foam insulation. The Shuttle Discovery is targeted for launch of mission STS-96 on May 20 at 9:32 a.m
jsc2024e065172 (10/3/2024) --- A temperature map is seen within a microgel suspension illuminated by the Colloidal Solids (COLIS) near infrared laser (NIR). Reference ground tests for the Colloidal Solids (COLIS) investigation show spatial variation of the sample temperature while illuminating an aqueous, dense suspension of thermosensitive microgels with a 0.5 s pulse of NIR laser light. The NIR beam propagates from left to right. The sample temperature with no NIR laser is uniform and set to 27°C. The temperature values are inferred from the change in scattered intensity at a scattering angle of 90°, as recorded by one of the complementary metal-oxide-semiconductor (CMOS) cameras of COLIS. Results from this investigation are expected to provide a deeper understanding of soft solid interactions with gravity and microgravity, paving the way for the design of new materials. Image courtesy of Redwire Space Laboratories, Kruibeke – Belgium.
CAPE CANAVERAL, Fla. - Space shuttle Discovery's forward reaction control system (FRCS), which helped steer the shuttle in orbit, is atop a transporter in Orbiter Processing Facility-2 at NASA's Kennedy Space Center in Florida. To maneuver, the FRCS used hypergolic fuel and oxidizer, which were purged from Discovery after its final spaceflight, STS-133. Next, the FRCS will be shipped to a maintenance facility at White Sands Space Harbor in New Mexico, where additional inspections will be performed and its components made safe to go on public display. The transition and retirement processing is expected to help rocket designers build next-generation spacecraft and prepare the shuttle for display. Photo credit: NASA/Jim Grossmann
CAPE CANAVERAL, Fla. – In the Astrotech payload processing facility in Titusville, Fla., the GOES-O satellite is moved toward a special stand for loading of its oxidizer and hydrazine propellants. The latest Geostationary Operational Environmental Satellite, GOES-O was developed by NASA for the National Oceanic and Atmospheric Administration, or NOAA. The GOES satellites continuously provide observations of 60 percent of the Earth including the continental United States, providing weather monitoring and forecast operations as well as a continuous and reliable stream of environmental information and severe weather warnings. Once in orbit, GOES-O will be designated GOES-14, and NASA will provide on-orbit checkout and then transfer operational responsibility to NOAA. The GOES-O satellite is targeted to launch from Cape Canaveral Air Force Station's Launch Complex 37 no earlier than May 12 onboard a United Launch Alliance Delta IV expendable launch vehicle. Photo credit: NASA/Troy Cryder
At Launch Complex 34, representatives from environmental and Federal agencies head for the block house during presentations about the environmental research project that involves the Department of Defense, Environmental Protection Agency, Department of Energy and NASA in a groundwater cleanup effort. Concentrations of trichloroethylene solvent have been identified in the soil at the complex as a result of cleaning methods for rocket parts during the Apollo Program, which used the complex, in the 60s. The group formed the Interagency NDAPL Consortium (IDC) to study three contamination cleanup technologies: Six Phase Soil Heating, Steam Injection and In Situ Oxidation with Potassium Permanganate. All three methods may offer a way to remove the contaminants in months instead of decades. KSC hosted a two-day conference that presented information and demonstrations of the three technologies being tested at the site
CAPE CANAVERAL, Fla. - Space shuttle Discovery's forward reaction control system (FRCS), which helped steer the shuttle in orbit, is moved to a transporter in Orbiter Processing Facility-2 at NASA's Kennedy Space Center in Florida. To maneuver, the FRCS used hypergolic fuel and oxidizer, which were purged from Discovery after its final spaceflight, STS-133. Next, the FRCS will be shipped to a maintenance facility at White Sands Space Harbor in New Mexico, where additional inspections will be performed and its components made safe to go on public display. The transition and retirement processing is expected to help rocket designers build next-generation spacecraft and prepare the shuttle for display. Photo credit: NASA/Jim Grossmann
CAPE CANAVERAL, Fla. – In the Astrotech payload processing facility in Titusville, Fla., the GOES-O satellite traverses the clean room toward a special stand for loading of its oxidizer and hydrazine propellants. The latest Geostationary Operational Environmental Satellite, GOES-O was developed by NASA for the National Oceanic and Atmospheric Administration, or NOAA. The GOES satellites continuously provide observations of 60 percent of the Earth including the continental United States, providing weather monitoring and forecast operations as well as a continuous and reliable stream of environmental information and severe weather warnings. Once in orbit, GOES-O will be designated GOES-14, and NASA will provide on-orbit checkout and then transfer operational responsibility to NOAA. The GOES-O satellite is targeted to launch from Cape Canaveral Air Force Station's Launch Complex 37 no earlier than May 12 onboard a United Launch Alliance Delta IV expendable launch vehicle. Photo credit: NASA/Troy Cryder
At Launch Pad 39B, two holes caused by hail on Space Shuttle Discovery's external tank (ET) are visible. Left of the tank is one of the solid rocket boosters. Workers are investigating the damage and potential problems for launch posed by ice forming in the holes, which may number as many as 150 over the entire tank. The average size of the holes is one-half inch in diameter and one-tenth inch deep. The external tank contains the liquid hydrogen fuel and liquid oxygen oxidizer and supplies them under pressure to the three space shuttle main engines in the orbiter during liftoff and ascent. The ET thermal protection system consists of sprayed-on foam insulation. The Shuttle Discovery is targeted for launch of mission STS-96 on May 20 at 9:32 a.m
CAPE CANAVERAL, Fla. – At NASA's Kennedy Space Center in Florida, Pratt and Whitney Rocketdyne aerospace technician Ken Burley constructs space shuttle main engine, or SSME, #2062 in the Space Shuttle Main Engine Processing Facility. This is the last SSME scheduled to be built at Kennedy before the end of the Space Shuttle Program. Three main engines are clustered at the aft end of the shuttle and have a combined thrust of more than 1.2 million pounds. Each engine utilizes liquid hydrogen for fuel and liquid oxygen as oxidizer and operates during the entire eight-and-a-half minute ride to orbit. Post-flight inspections and maintenance of each engine also are conducted in the SSME Processing Facility between shuttle missions. Photo credit: NASA_Jack Pfaller
CAPE CANAVERAL, Fla. - Crews in Orbiter Processing Facility-2 at NASA's Kennedy Space Center in Florida remove space shuttle Discovery's forward reaction control system (FRCS), which helped steer the shuttle in orbit. To maneuver, the FRCS used hypergolic fuel and oxidizer, which were purged from Discovery after its final spaceflight, STS-133. Next, the FRCS will be shipped to a maintenance facility at White Sands Space Harbor in New Mexico, where additional inspections will be performed and its components made safe to go on public display. The transition and retirement processing is expected to help rocket designers build next-generation spacecraft and prepare the shuttle for display. Photo credit: NASA/Jim Grossmann
CAPE CANAVERAL, Fla. – At NASA's Kennedy Space Center in Florida, Pratt and Whitney Rocketdyne aerospace technician Ken Burley inspects the construction of space shuttle main engine, or SSME, #2062 in the Space Shuttle Main Engine Processing Facility. This is the last SSME scheduled to be built at Kennedy before the end of the Space Shuttle Program. Three main engines are clustered at the aft end of the shuttle and have a combined thrust of more than 1.2 million pounds. Each engine utilizes liquid hydrogen for fuel and liquid oxygen as oxidizer and operates during the entire eight-and-a-half minute ride to orbit. Post-flight inspections and maintenance of each engine also are conducted in the SSME Processing Facility between shuttle missions. Photo credit: NASA_Jack Pfaller
KENNEDY SPACE CENTER, FLA. - On Launch Pad 17-B at Cape Canaveral Air Force Station in Florida, workers remove the protective covers from the engine nozzle on the second stage segment removed from the Delta II rocket. At the Boeing plant in Alabama, a leak was observed in the second-stage oxidizer tank for another Delta II that had been scheduled to launch in November; therefore, all identical tanks scheduled for launch in the near future are being checked. The second stage for the Delta II that will launch STEREO cannot be effectively tested while atop the first stage at Pad 17-B. STEREO stands for Solar Terrestrial Relations Observatory and comprises two spacecraft. The STEREO mission is the first to take measurements of the sun and solar wind in 3-dimension. This new view will improve our understanding of space weather and its impact on the Earth. STEREO is expected to lift off in late August 2006. Photo credit: NASA/Jim Grossmann
This image shows partially exposed bedrock within the Koval'sky impact basin, which is on the outskirts of the extensive lava field of Daedalia Planum. Daedalia Planum is located southwest of Arsia Mons, which may be the source responsible for filling the crater with lava flows and ash deposits. On one side, bright bedrock with scattered dark blue spots are seen. The dark blue spots are boulders shedding from the outcrops. The color range of the bedrock provides some information on its composition. The blue color is indicative of the presence of iron-rich minerals that are generally not oxidized (i.e., rusted), unlike most of the ruddy Martian surface. Volcanic rocks are common on Mars. Possible candidate minerals for the bluish materials are often consistent with iron-rich minerals, such as pyroxene and olivine. The ridges may represent remnants of the original surface of the lava flows that filled the Koval'sky impact basin. NB: The region is named for M. A. Koval'sky, a Russian astronomer. https://photojournal.jpl.nasa.gov/catalog/PIA21765