carbon, kennedy space center

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CAPE CANAVERAL, Fla. – A closeup of the wing leading edge on space shuttle Atlantis where a reinforced-carbon carbon, or RCC, panel has been removed. The structural edge of the wing (area of red and green behind the panels) will undergo spar corrosion inspection to verify the structural integrity of the wing.  The RCC panels will be placed in protective coverings until the inspection is complete.  Atlantis will make the 31st flight to the International Space Station for the STS-129 mission, targeted for launch on Nov. 12. Photo credit: NASA/Tim Jacobs KSC-2009-3832

CAPE CANAVERAL, Fla. – A closeup of the wing leading edge on space shu...

CAPE CANAVERAL, Fla. – A closeup of the wing leading edge on space shuttle Atlantis where a reinforced-carbon carbon, or RCC, panel has been removed. The structural edge of the wing (area of red and green behin... More

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center in Florida, a crane is attached to the Cosmic Origins Spectrograph, or COS, still in its shipping container.  The crane will remove the COS and place it on a test stand. The COS is part of the payload on space shuttle Atlantis for the Hubble servicing mission, targeted to launch in mid-May.  Installing the COS during the mission will effectively restore spectroscopy to Hubble’s scientific arsenal, and at the same time provide the telescope with unique capabilities. COS is designed to study the large-scale structure of the universe and how galaxies, stars and planets formed and evolved. It will help determine how elements needed for life such as carbon and iron first formed and how their abundances have increased over the lifetime of the universe.   Photo credit: NASA/Jack Pfaller KSC-2009-2148

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at ...

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center in Florida, a crane is attached to the Cosmic Origins Spectrograph, or COS, still in its shipping container. Th... More

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center in Florida, technicians oversee the lifting of the Cosmic Origins Spectrograph, or COS, from a stand.  The COS will be moved to and placed on the Orbital Replacement Unit Carrier that will be installed in space shuttle Atlantis' payload bay.  The COS is part of the payload for the Hubble servicing mission, STS-125, targeted to launch in mid-May. Installing the COS during the mission will effectively restore spectroscopy to Hubble’s scientific arsenal, and at the same time provide the telescope with unique capabilities. COS is designed to study the large-scale structure of the universe and how galaxies, stars and planets formed and evolved. It will help determine how elements needed for life such as carbon and iron first formed and how their abundances have increased over the lifetime of the universe.  Photo credit: NASA/Kim Shiflett KSC-2009-2162

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at ...

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center in Florida, technicians oversee the lifting of the Cosmic Origins Spectrograph, or COS, from a stand. The COS w... More

CAPE CANAVERAL, Fla. - In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a technician works to replace the protective cover on the Super Lightweight Interchangeable Carrier, or SLIC.  The cover was removed to clean  the carrier of contaminants found Sept. 17 during preparations to deliver NASA's Hubble Space Telescope servicing payload to Launch Pad 39A. Cleanliness is extremely important for space shuttle Atlantis’ STS-125 mission to Hubble, and the teams have insured that the SLIC  is ready to fly.  The SLIC, which holds battery module assemblies, is built with state-of-the-art, lightweight, composite materials - carbon fiber with a cyanate ester resin and a titanium metal matrix composite. These composites have greater strength-to-mass ratios than the metals typically used in spacecraft design. The carrier is one of four being transferred to Launch Pad 39A. At the pad, the carriers will be loaded into Atlantis’ payload bay.  Launch of Atlantis is targeted for Oct. 10.   Photo credit: NASA/Jack Pfaller KSC-08pd2655

CAPE CANAVERAL, Fla. - In the Payload Hazardous Servicing Facility at ...

CAPE CANAVERAL, Fla. - In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a technician works to replace the protective cover on the Super Lightweight Interchangeable Carrier, or SLIC. ... More

CAPE CANAVERAL, Fla. -- In the high bay of the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a worker from NASA's Goddard Space Flight Center documents the installation of a pallet support strut on the Super Lightweight Interchangeable Carrier for the Hubble Space Telescope.  The Super Lightweight Interchangeable Carrier, or SLIC, is one of four carriers supporting hardware for space shuttle Atlantis' STS-125 mission to service the telescope. SLIC is built with state-of-the-art, lightweight, composite materials - carbon fiber with a cyanate ester resin and a titanium metal matrix composite. These composites have greater strength-to-mass ratios than the metals typically used in spacecraft design. The Orbital Replacement Unit Carrier, or ORUC, and the Flight Support System, or FSS, have also arrived at Kennedy.     The Multi-Use Lightweight Equipment carrier will be delivered in early August. The carriers will be prepared for the integration of telescope science instruments, both internal and external replacement components, as well as the flight support equipment to be used by the astronauts during the Hubble servicing mission, targeted for launch Oct. 8.  Photo credit: NASA/Jack Pfaller KSC-08pd2095

CAPE CANAVERAL, Fla. -- In the high bay of the Payload Hazardous Servi...

CAPE CANAVERAL, Fla. -- In the high bay of the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a worker from NASA's Goddard Space Flight Center documents the installation of a pallet suppor... More

CAPE CANAVERAL, Fla. -  In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a technician uncovers the Super Lightweight Interchangeable Carrier, or SLIC.  Contamination discovered Sept. 17 during preparations to deliver NASA's Hubble Space Telescope servicing payload to Launch Pad 39A will be removed. Cleanliness is extremely important for space shuttle Atlantis’ STS-125 mission to Hubble, and the teams have insured that the SLIC is ready to fly. The SLIC, which holds battery module assemblies for servicing of the Hubble Space Telescope on the STS-125 mission, is built with state-of-the-art, lightweight, composite materials - carbon fiber with a cyanate ester resin and a titanium metal matrix composite. These composites have greater strength-to-mass ratios than the metals typically used in spacecraft design. The carrier is one of four being transferred to Launch Pad 39A. At the pad, the carriers will be loaded into Atlantis’ payload bay.  Launch of Atlantis is targeted for Oct. 10.   Photo credit: NASA/Jack Pfaller KSC-08pd2643

CAPE CANAVERAL, Fla. - In the Payload Hazardous Servicing Facility at...

CAPE CANAVERAL, Fla. - In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center, a technician uncovers the Super Lightweight Interchangeable Carrier, or SLIC. Contamination discovered Sept. ... More

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center in Florida, a crane places the Cosmic Origins Spectrograph, or COS, on the Orbital Replacement Unit Carrier where it will be installed.  The carrier will be placed in space shuttle Atlantis' payload bay for the Hubble servicing mission, STS-125, targeted to launch in mid-May.  Installing the COS during the mission will effectively restore spectroscopy to Hubble’s scientific arsenal, and at the same time provide the telescope with unique capabilities. COS is designed to study the large-scale structure of the universe and how galaxies, stars and planets formed and evolved. It will help determine how elements needed for life such as carbon and iron first formed and how their abundances have increased over the lifetime of the universe.  Photo credit: NASA/Kim Shiflett KSC-2009-2167

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at ...

CAPE CANAVERAL, Fla. – In the Payload Hazardous Servicing Facility at NASA's Kennedy Space Center in Florida, a crane places the Cosmic Origins Spectrograph, or COS, on the Orbital Replacement Unit Carrier wher... More

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experiment features a four-acre site just north of the Launch Complex 39 area. Increased amoounts of carbon dioxide are piped into 16 open-top chambers that house pristine Florida scrub vegetation, chosen because it is small and woody and fits in the chambers and can be controlled, yet has the attributes of much larger forests. Experts predict a doubling of the carbon dioxide in the Earth's atmosphere during the next century, and the three-year KSC project being conducted by the Smithsonian-led team hopes that by simulating the increase, they can determine how natural ecosystems and vegetation will respond. Also participating in the effort are KSC, academic and international organizations. The study is being funded by a Department of energy grant KSC-96pc632

Researchers from the Smithsonian Institution hope their experiment in ...

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experimen... More

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experiment features a four-acre site just north of the Launch Complex 39 area. Increased amoounts of carbon dioxide are piped into 16 open-top chambers that house pristine Florida scrub vegetation, chosen because it is small and woody and fits in the chambers and can be controlled, yet has the attributes of much larger forests. Experts predict a doubling of the carbon dioxide in the Earth's atmosphere during the next century, and the three-year KSC project being conducted by the Smithsonian-led team hopes that by simulating the increase, they can determine how natural ecosystems and vegetation will respond. Also participating in the effort are KSC, academic and international organizations. The study is being funded by a Department of energy grant KSC-96pc635

Researchers from the Smithsonian Institution hope their experiment in ...

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experimen... More

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experiment features a four-acre site just north of the Launch Complex 39 area. Increased amoounts of carbon dioxide are piped into 16 open-top chambers that house pristine Florida scrub vegetation, chosen because it is small and woody and fits in the chambers and can be controlled, yet has the attributes of much larger forests. Experts predict a doubling of the carbon dioxide in the Earth's atmosphere during the next century, and the three-year KSC project being conducted by the Smithsonian-led team hopes that by simulating the increase, they can determine how natural ecosystems and vegetation will respond. Also participating in the effort are KSC, academic and international organizations. The study is being funded by a Department of energy grant KSC-96pc634

Researchers from the Smithsonian Institution hope their experiment in ...

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experimen... More

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experiment features a four-acre site just north of the Launch Complex 39 area. Increased amoounts of carbon dioxide are piped into 16 open-top chambers that house pristine Florida scrub vegetation, chosen because it is small and woody and fits in the chambers and can be controlled, yet has the attributes of much larger forests. Experts predict a doubling of the carbon dioxide in the Earth's atmosphere during the next century, and the three-year KSC project being conducted by the Smithsonian-led team hopes that by simulating the increase, they can determine how natural ecosystems and vegetation will respond. Also participating in the effort are KSC, academic and international organizations. The study is being funded by a Department of energy grant KSC-96pc633

Researchers from the Smithsonian Institution hope their experiment in ...

Researchers from the Smithsonian Institution hope their experiment in a local scrub oak community at KSC will yield new insights into the effects of increased carbon dioxide on natural vegetation. The experimen... More

KENNEDY SPACE CENTER, FLA. -- A Boeing Delta II expendable launch vehicle lifts off with NASA's Mars Polar Lander into a cloud-covered sky at 3:21:10 p.m. EST from Launch Complex 17B, Cape Canaveral Air Station. The lander is a solar-powered spacecraft designed to touch down on the Martian surface near the northern-most boundary of the south polar cap, which consists of carbon dioxide ice. The lander will study the polar water cycle, frosts, water vapor, condensates and dust in the Martian atmosphere. It is equipped with a robotic arm to dig beneath the layered terrain at the polar cap. In addition, Deep Space 2 microprobes, developed by NASA's New Millennium Program, are installed on the lander's cruise stage. After crashing into the planet's surface, they will conduct two days of soil and water experiments up to 1 meter (3 feet) below the Martian surface, testing new technologies for future planetary descent probes. The lander is the second spacecraft to be launched in a pair of Mars Surveyor '98 missions. The first is the Mars Climate Orbiter, which was launched aboard a Delta II rocket from Launch Complex 17A on Dec. 11, 1998. KSC-99pc03

KENNEDY SPACE CENTER, FLA. -- A Boeing Delta II expendable launch vehi...

KENNEDY SPACE CENTER, FLA. -- A Boeing Delta II expendable launch vehicle lifts off with NASA's Mars Polar Lander into a cloud-covered sky at 3:21:10 p.m. EST from Launch Complex 17B, Cape Canaveral Air Station... More

KENNEDY SPACE CENTER, FLA. -- Amid clouds of exhaust, a Boeing Delta II expendable launch vehicle with NASA's Mars Polar Lander clears Launch Complex 17B, Cape Canaveral Air Station, after launch at 3:21:10 p.m. EST. The lander is a solar-powered spacecraft designed to touch down on the Martian surface near the northern-most boundary of the south polar cap, which consists of carbon dioxide ice. The lander will study the polar water cycle, frosts, water vapor, condensates and dust in the Martian atmosphere. It is equipped with a robotic arm to dig beneath the layered terrain at the polar cap. In addition, Deep Space 2 microprobes, developed by NASA's New Millennium Program, are installed on the lander's cruise stage. After crashing into the planet's surface, they will conduct two days of soil and water experiments up to 1 meter (3 feet) below the Martian surface, testing new technologies for future planetary descent probes. The lander is the second spacecraft to be launched in a pair of Mars Surveyor '98 missions. The first is the Mars Climate Orbiter, which was launched aboard a Delta II rocket from Launch Complex 17A on Dec. 11, 1998. KSC-99pc05

KENNEDY SPACE CENTER, FLA. -- Amid clouds of exhaust, a Boeing Delta I...

KENNEDY SPACE CENTER, FLA. -- Amid clouds of exhaust, a Boeing Delta II expendable launch vehicle with NASA's Mars Polar Lander clears Launch Complex 17B, Cape Canaveral Air Station, after launch at 3:21:10 p.m... More

KENNEDY SPACE CENTER, FLA. -- Amid clouds of exhaust and into a gray-clouded sky , a Boeing Delta II expendable launch vehicle lifts off with NASA's Mars Polar Lander at 3:21:10 p.m. EST from Launch Complex 17B, Cape Canaveral Air Station. The lander is a solar-powered spacecraft designed to touch down on the Martian surface near the northern-most boundary of the south polar cap, which consists of carbon dioxide ice. The lander will study the polar water cycle, frosts, water vapor, condensates and dust in the Martian atmosphere. It is equipped with a robotic arm to dig beneath the layered terrain at the polar cap. In addition, Deep Space 2 microprobes, developed by NASA's New Millennium Program, are installed on the lander's cruise stage. After crashing into the planet's surface, they will conduct two days of soil and water experiments up to 1 meter (3 feet) below the Martian surface, testing new technologies for future planetary descent probes. The lander is the second spacecraft to be launched in a pair of Mars Surveyor '98 missions. The first is the Mars Climate Orbiter, which was launched aboard a Delta II rocket from Launch Complex 17A on Dec. 11, 1998. KSC-99pc04

KENNEDY SPACE CENTER, FLA. -- Amid clouds of exhaust and into a gray-c...

KENNEDY SPACE CENTER, FLA. -- Amid clouds of exhaust and into a gray-clouded sky , a Boeing Delta II expendable launch vehicle lifts off with NASA's Mars Polar Lander at 3:21:10 p.m. EST from Launch Complex 17B... More

KENNEDY SPACE CENTER, FLA. -- Looking like a Roman candle, the exhaust from the Boeing Delta II rocket with the Mars Polar Lander aboard lights up the clouds as it hurtles skyward. The rocket was launched at 3:21:10 p.m. EST from Launch Complex 17B, Cape Canaveral Air Station. The lander is a solar-powered spacecraft designed to touch down on the Martian surface near the northern-most boundary of the south polar cap, which consists of carbon dioxide ice. The lander will study the polar water cycle, frosts, water vapor, condensates and dust in the Martian atmosphere. It is equipped with a robotic arm to dig beneath the layered terrain. In addition, Deep Space 2 microprobes, developed by NASA's New Millennium Program, are installed on the lander's cruise stage. After crashing into the planet's surface, they will conduct two days of soil and water experiments up to 1 meter (3 feet) below the Martian surface, testing new technologies for future planetary descent probes. The lander is the second spacecraft to be launched in a pair of Mars Surveyor '98 missions. The first is the Mars Climate Orbiter, which was launched aboard a Delta II rocket from Launch Complex 17A on Dec. 11, 1998. KSC-99pc07

KENNEDY SPACE CENTER, FLA. -- Looking like a Roman candle, the exhaust...

KENNEDY SPACE CENTER, FLA. -- Looking like a Roman candle, the exhaust from the Boeing Delta II rocket with the Mars Polar Lander aboard lights up the clouds as it hurtles skyward. The rocket was launched at 3:... More

KENNEDY SPACE CENTER, FLA. -- Silhouetted against the gray sky, a Boeing Delta II expendable launch vehicle with NASA's Mars Polar Lander lifts off from Launch Complex 17B, Cape Canaveral Air Station, at 3:21:10 p.m. EST. The lander is a solar-powered spacecraft designed to touch down on the Martian surface near the northern-most boundary of the south polar cap, which consists of carbon dioxide ice. The lander will study the polar water cycle, frosts, water vapor, condensates and dust in the Martian atmosphere. It is equipped with a robotic arm to dig beneath the layered terrain at the polar cap. In addition, Deep Space 2 microprobes, developed by NASA's New Millennium Program, are installed on the lander's cruise stage. After crashing into the planet's surface, they will conduct two days of soil and water experiments up to 1 meter (3 feet) below the Martian surface, testing new technologies for future planetary descent probes. The lander is the second spacecraft to be launched in a pair of Mars Surveyor '98 missions. The first is the Mars Climate Orbiter, which was launched aboard a Delta II rocket from Launch Complex 17A on Dec. 11, 1998. KSC-99pc06

KENNEDY SPACE CENTER, FLA. -- Silhouetted against the gray sky, a Boei...

KENNEDY SPACE CENTER, FLA. -- Silhouetted against the gray sky, a Boeing Delta II expendable launch vehicle with NASA's Mars Polar Lander lifts off from Launch Complex 17B, Cape Canaveral Air Station, at 3:21:1... More

VANDENBERG AIR FORCE BASE, Calif. --  NASA’s Orbiting Carbon Observatory and its Taurus booster lift off Feb. 24 from Vandenberg Air Force Base in California at 4:55 a.m. EST. A contingency was declared a few minutes later and the satellite failed to reach orbit after liftoff.  Preliminary indications are that the fairing on the Taurus XL launch vehicle failed to separate. The fairing is a clamshell structure that encapsulates the satellite as it travels through the atmosphere. A Mishap Investigation Board is being set up to determine the cause of the launch failure.  Photo courtesy of Orbital Sciences KSC-2009-1827

VANDENBERG AIR FORCE BASE, Calif. -- NASA’s Orbiting Carbon Observato...

VANDENBERG AIR FORCE BASE, Calif. -- NASA’s Orbiting Carbon Observatory and its Taurus booster lift off Feb. 24 from Vandenberg Air Force Base in California at 4:55 a.m. EST. A contingency was declared a few m... More

Original photo and caption dated August 14, 1995: <i>"KSC plant physiologist Dr. Gary Stutte (right) and Cheryl Mackowiak harvest potatoes grown in the Biomass Production Chamber of the Controlled Enviornment Life Support System (CELSS in Hangar L at Cape Canaveral Air Station. During a 418-day "human rated" experiment, potato crops grown in the chamber provided the equivalent of a continuous supply of the oxygen for one astronaut, along with 55 percent of that long-duration space flight crew member's caloric food requirements and enough purified water for four astronauts while absorbing their expelled carbon dioxide. The experiment provided data that will help demonstarte the feasibility of the CELSS operating as a bioregenerative life support system for lunar and deep-space missions that can operate independently without the need to carry consumables such as air, water and food, while not requiring the expendable air and water system filters necessary on today's human-piloted spacecraft."</i KSC-95pc1196

Original photo and caption dated August 14, 1995: <i>"KSC plant physio...

Original photo and caption dated August 14, 1995: <i>"KSC plant physiologist Dr. Gary Stutte (right) and Cheryl Mackowiak harvest potatoes grown in the Biomass Production Chamber of the Controlled Enviornment L... More

Original photo and caption dated August 14, 1995: <i>"KSC plant physiologist Dr. Gary Stutte harvests a potato grown in the Biomass Production Chamber of the Controlled environment Life Support system (CELSS) in Hangar L at Cape Canaveral Air Station. During a 418-day "human rated" experiment, potato crops grown in the chamber provided the equivalent of a continuous supply of the oxygen for one astronaut, along with 55 percent of that long-duration space flight crew member's caloric food requirements and enough purified water for four astronauts while absorbing their expelled carbon dioxide. The experiment provided data that will help demonstarte the feasibility of the CELSS operating as a bioregenerative life support system for lunar and deep-space missions that can operate independently without the need to carry consumables such as air, water and food, while not requiring the expendable air and water system filters necessary on today's human-piloted spacecraft."</i KSC-95pc1197

Original photo and caption dated August 14, 1995: <i>"KSC plant physio...

Original photo and caption dated August 14, 1995: <i>"KSC plant physiologist Dr. Gary Stutte harvests a potato grown in the Biomass Production Chamber of the Controlled environment Life Support system (CELSS) i... More

Original photo and caption dated June 22, 1988: "A dwarf wheat variety known as Yecoro Rojo flourishes in KSC's Biomass Production Chamber. Researchers are gathering information on the crop's ability to produce food, water and oxygen, and then remove carbon dioxide. The confined quarters associated with space travel require researchers to focus on smaller plants that yield proportionately large amounts of biomass. This wheat crop takes about 85 days to grow before harvest." KSC-388c2096-08

Original photo and caption dated June 22, 1988: "A dwarf wheat variety...

Original photo and caption dated June 22, 1988: "A dwarf wheat variety known as Yecoro Rojo flourishes in KSC's Biomass Production Chamber. Researchers are gathering information on the crop's ability to produce... More

CO2 study site manager and plant physiologist Graham Hymus (left) examines scrub oak foliage while project engineer David Johnson (right) looks on. The life sciences study is showing that rising levels of carbon dioxide in our atmosphere, caused by the burning of fossil fuels, could spur plant growth globally. The site of KSC's study is a natural scrub oak area near the Vehicle Assembly Building. Twelve-foot areas of scrub oak have been enclosed in 16 open-top test chambers into which CO2 has been blown. Five scientists from NASA and the Smithsonian Environmental Research Center in Edgewater, Md., work at the site to monitor experiments and keep the site running. Scientists hope to continue the study another five to 10 years. More information on this study can be found in Release No. 57-00. Additional photos can be found at: www-pao.ksc.nasa.gov/captions/subjects/co2study.htm KSC00pp0920

CO2 study site manager and plant physiologist Graham Hymus (left) exam...

CO2 study site manager and plant physiologist Graham Hymus (left) examines scrub oak foliage while project engineer David Johnson (right) looks on. The life sciences study is showing that rising levels of carbo... More

CO2 study site manager and plant physiologist Graham Hymus (left) examines scrub oak foliage while project engineer David Johnson (right) looks on. The life sciences study is showing that rising levels of carbon dioxide in our atmosphere, caused by the burning of fossil fuels, could spur plant growth globally. The site of KSC's study is a natural scrub oak area near the Vehicle Assembly Building. Twelve-foot areas of scrub oak have been enclosed in 16 open-top test chambers into which CO2 has been blown. Five scientists from NASA and the Smithsonian Environmental Research Center in Edgewater, Md., work at the site to monitor experiments and keep the site running. Scientists hope to continue the study another five to 10 years. More information on this study can be found in Release No. 57-00. Additional photos can be found at: www-pao.ksc.nasa.gov/captions/subjects/co2study.htm KSC-00pp0920

CO2 study site manager and plant physiologist Graham Hymus (left) exam...

CO2 study site manager and plant physiologist Graham Hymus (left) examines scrub oak foliage while project engineer David Johnson (right) looks on. The life sciences study is showing that rising levels of carbo... More

KENNEDY SPACE CENTER, FLA.  -  Members of the  Stafford-Covey Return to Flight Task Group (SCTG) look over equipment in the Orbiter Processing Facility.  At left (back to camera), Fernando Santos, with NASA, and Paul Ogletree (at monitor), with United Space Alliance, describe how flash thermography is used to inspect the structure of Reinforced Carbon Carbon panels and establish a baseline on panels before flight.  Chairing the task group are Richard O. Covey (far right), former Space Shuttle commander, and Thomas P. Stafford, Apollo commander.  Chartered by NASA Administrator Sean O’Keefe, the task group will perform an independent assessment of NASA’s implementation of the final recommendations by the Columbia Accident Investigation Board.

KENNEDY SPACE CENTER, FLA. - Members of the Stafford-Covey Return t...

KENNEDY SPACE CENTER, FLA. - Members of the Stafford-Covey Return to Flight Task Group (SCTG) look over equipment in the Orbiter Processing Facility. At left (back to camera), Fernando Santos, with NASA, an... More

KENNEDY SPACE CENTER, FLA. -  Mike Hyatt (left) and Saul Ngy, technicians with United Space Alliance, install a spar on the wing of the orbiter Atlantis.  The Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Mike Hyatt (left) and Saul Ngy, technici...

KENNEDY SPACE CENTER, FLA. - Mike Hyatt (left) and Saul Ngy, technicians with United Space Alliance, install a spar on the wing of the orbiter Atlantis. The Reinforced Carbon Carbon (RCC) panels are mechanica... More

KENNEDY SPACE CENTER, FLA. -  Mike Hyatt (left) and Saul Ngy, technicians with United Space Alliance, prepare to install a spar on the wing of the orbiter Atlantis.  The Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Mike Hyatt (left) and Saul Ngy, technici...

KENNEDY SPACE CENTER, FLA. - Mike Hyatt (left) and Saul Ngy, technicians with United Space Alliance, prepare to install a spar on the wing of the orbiter Atlantis. The Reinforced Carbon Carbon (RCC) panels ar... More

KENNEDY SPACE CENTER, FLA. - Technician Saul Ngy, with United Space Alliance, prepares to install a spar on the wing of the orbiter Atlantis.  The Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Technician Saul Ngy, with United Space Al...

KENNEDY SPACE CENTER, FLA. - Technician Saul Ngy, with United Space Alliance, prepares to install a spar on the wing of the orbiter Atlantis. The Reinforced Carbon Carbon (RCC) panels are mechanically attached... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects the wing of the orbiter Atlantis before installing a spar. Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects the wing of the orbiter Atlantis before installing a spar. Reinforced Carbon Carbon (RCC) pane... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, Mike Hyatt, with United Space Alliance, installs a spar on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike Hyatt, with United Space Alliance, installs a spar on the wing of the orbiter Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanic... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects spar installation on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects spar installation on the wing of the orbiter Atlantis. Reinforced Carbon Carbon (RCC) panels ... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects a spar to be installed on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects a spar to be installed on the wing of the orbiter Atlantis. Reinforced Carbon Carbon (RCC) pa... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike Hyatt (above) and Saul Ngy (below), with United Space Alliance, install a spar on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike Hyatt (above) and Saul Ngy (below), with United Space Alliance, install a spar on the wing of the orbiter Atlantis. Reinforced Carbon Carbo... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike Hyatt (left) and Saul Ngy (right), with United Space Alliance, finish installing a spar on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mike Hyatt (left) and Saul Ngy (right), with United Space Alliance, finish installing a spar on the wing of the orbiter Atlantis. Reinforced Car... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects a piece of equipment for spar installation on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, John Newport, with United Space Alliance, inspects a piece of equipment for spar installation on the wing of the orbiter Atlantis. Reinforced Ca... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (above) attaches a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unit...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (above) attaches a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the wing of the orbiter... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (left) Saul Ngy (center) and Jerry Belt (right) lift a Reinforced Carbon Carbon (RCC) panel to attach onto the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (left) Saul Ngy (center) and Jerry Belt (right) lift a Reinforced Carbon Carbon (RCC) panel to attach on... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (left) Jerry Belt (center), and Saul Ngy (right), lift a Reinforced Carbon Carbon (RCC) panel they will attach to the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (left) Jerry Belt (center), and Saul Ngy (right), lift a Reinforced Carbon Carbon (RCC) panel they will ... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers, from center, left to right, Saul Ngy, Jerry Belt and Mike Hyatt, prepare to attach a Reinforced Carbon Carbon (RCC) panel (on the table) to the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers, from center, left to right, Saul Ngy, Jerry Belt and Mike Hyatt, prepare to attach a Reinforced Carbon Carbon (RCC... More

KENNEDY SPACE CENTER, FLA. -  William Gaetjens (background), with the Vehicle Integration Test Team (VITT) directs Japanese astronaut Koichi Wakata’s attention to the spars installed on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing via the spars - a series of floating joints - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - William Gaetjens (background), with the ...

KENNEDY SPACE CENTER, FLA. - William Gaetjens (background), with the Vehicle Integration Test Team (VITT) directs Japanese astronaut Koichi Wakata’s attention to the spars installed on the wing of the orbiter ... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (above) completes installation of a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (above) completes installation of a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the win... More

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata (right) listens to William Gaetjens, with the Vehicle Integration Test Team (VITT), who is providing details about the spar installation (left) on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing via the spars - a series of floating joints - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata (right) ...

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata (right) listens to William Gaetjens, with the Vehicle Integration Test Team (VITT), who is providing details about the spar installation (left) on t... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt attaches a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unit...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt attaches a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the wing of the orbiter Atlanti... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (right) attaches a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot. The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unit...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (right) attaches a Reinforced Carbon Carbon (RCC) panel onto the leading edge of the wing of the orbiter... More

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata looks at the spars installed on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing via the spars - a series of floating joints - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata looks at...

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata looks at the spars installed on the wing of the orbiter Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing via t... More

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata gestures as he examines the spar installation (behind him) on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing via the spars - a series of floating joints - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata gestures...

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata gestures as he examines the spar installation (behind him) on the wing of the orbiter Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanica... More

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata gestures as he examines the spar installation (behind him) on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing via the spars - a series of floating joints - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata gestures...

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata gestures as he examines the spar installation (behind him) on the wing of the orbiter Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanica... More

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata (front) listens to William Gaetjens, with the Vehicle Integration Test Team (VITT), who is providing details about the spar installation (left) on the wing of the orbiter Atlantis.  Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing via the spars - a series of floating joints - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata (front) ...

KENNEDY SPACE CENTER, FLA. - Japanese astronaut Koichi Wakata (front) listens to William Gaetjens, with the Vehicle Integration Test Team (VITT), who is providing details about the spar installation (left) on t... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Jerry Belt, with United Space Alliance, checks a spar attachment on the wing of the orbiter Atlantis before installing Reinforced Carbon Carbon (RCC) panels on the wing.  The spars - floating joints - reduce loading on the panels caused by wing deflections.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Jerry...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Jerry Belt, with United Space Alliance, checks a spar attachment on the wing of the orbiter Atlantis before installing Reinforced Carbon Carbon (... More

KENNEDY SPACE CENTER, FLA. -   Billy Witt, a midbody shop mechanic with United Space Alliance, checks a part used for installation of a Reinforced Carbon Carbon (RCC) panel to the leading edge of the wing of an orbiter.  Above him is an RCC panel just installed on Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - Billy Witt, a midbody shop mechanic wit...

KENNEDY SPACE CENTER, FLA. - Billy Witt, a midbody shop mechanic with United Space Alliance, checks a part used for installation of a Reinforced Carbon Carbon (RCC) panel to the leading edge of the wing of an... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (above) and Saul Ngy (below right) finish installing a Reinforced Carbon Carbon (RCC) panel to the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (above) and Saul Ngy (below right) finish installing a Reinforced Carbon Carbon (RCC) panel to the leadi... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (above) finishes installing a Reinforced Carbon Carbon (RCC) panel to the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt (above) finishes installing a Reinforced Carbon Carbon (RCC) panel to the leading edge of the wing of the... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, United Space Alliance workers  Mike Hyatt (above),  Saul Ngy (right) and Jerry Belt (below) install a Reinforced Carbon Carbon (RCC) panel to the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unit...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (above), Saul Ngy (right) and Jerry Belt (below) install a Reinforced Carbon Carbon (RCC) panel to th... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt looks over a Reinforced Carbon Carbon (RCC) panel that will be attached to the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unit...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Mike Hyatt looks over a Reinforced Carbon Carbon (RCC) panel that will be attached to the leading edge of the wing ... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (left), Saul Ngy (center) and Jerry Belt (right) prepare to install a Reinforced Carbon Carbon (RCC) panel to the leading edge of the wing of the orbiter Atlantis.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unit...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Mike Hyatt (left), Saul Ngy (center) and Jerry Belt (right) prepare to install a Reinforced Carbon Carbon (RCC) pa... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility,  Jim Landy, NDE specialist with United Space Alliance (USA), watches a monitor off-screen to examine a Reinforced Carbon Carbon panel using flash thermography.  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Jim ...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Jim Landy, NDE specialist with United Space Alliance (USA), watches a monitor off-screen to examine a Reinforced Carbon Carbon panel using flash... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, United Space Alliance worker Dan Kenna (right) positions a Reinforced Carbon Carbon panel on the table to perform flash thermography.  In the background, Paul Ogletree observes the monitor.  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unit...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance worker Dan Kenna (right) positions a Reinforced Carbon Carbon panel on the table to perform flash thermography. In the ba... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Jim Landy (front), Dan Phillips and Dan Kenna watch a monitor showing results of flash thermography on the Reinforced Carbon Carbon panel on the table (foreground).  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Jim Landy (front), Dan Phillips and Dan Kenna watch a monitor showing results of flash thermography on the Reinforc... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Dan Kenna and Jim Landy prepare to examine a Reinforced Carbon Carbon panel using flash thermography.  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers Dan Kenna and Jim Landy prepare to examine a Reinforced Carbon Carbon panel using flash thermography. Attached to ... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers share the task of examining  a Reinforced Carbon Carbon panel using flash thermography.  From left are Paul Ogletree, Jim Landy (kneeling), Dan Phillips and Dan Kenna.  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers share the task of examining a Reinforced Carbon Carbon panel using flash thermography. From left are Paul Ogletre... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers (left to right) Jim Landy, Dan Phillips, Paul Ogletree and Dan Kenna check results of flash thermography on the Reinforced Carbon Carbon panel on the table (foreground).  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers (left to right) Jim Landy, Dan Phillips, Paul Ogletree and Dan Kenna check results of flash thermography on the Rei... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility,  Jim Landy (left), NDE specialist with United Space Alliance (USA), prepares to examine a Reinforced Carbon Carbon panel using flash thermography.  Helping out, at right, is Dan Phillips, also with USA.  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Jim...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Jim Landy (left), NDE specialist with United Space Alliance (USA), prepares to examine a Reinforced Carbon Carbon panel using flash thermograph... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers (left to right) Jim Landy, Paul Ogletree, Dan Kenna and Dan Phillips check results of flash thermography on the Reinforced Carbon Carbon panel on the table (foreground).  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers (left to right) Jim Landy, Paul Ogletree, Dan Kenna and Dan Phillips check results of flash thermography on the Rei... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers share the task of examining  a Reinforced Carbon Carbon panel using flash thermography.  From left are Dan Kenna, Jim Landy, Paul Ogletree and Dan Phillips.  Attached to the leading edge of the wing of the orbiters,  the gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Unite...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, United Space Alliance workers share the task of examining a Reinforced Carbon Carbon panel using flash thermography. From left are Dan Kenna, J... More

KENNEDY SPACE CENTER, FLA. -  United Space Alliance employee Anthony Simmons prepares to electroweld a crack formed in the insulator inside a Reinforced Carbon Carbon panel.   The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony S...

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons prepares to electroweld a crack formed in the insulator inside a Reinforced Carbon Carbon panel. The gray carbon composite RCC pane... More

KENNEDY SPACE CENTER, FLA. -   United Space Alliance employee Anthony Simmons continues electrowelding on an insulator inside a Reinforced Carbon Carbon panel.   The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony ...

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons continues electrowelding on an insulator inside a Reinforced Carbon Carbon panel. The gray carbon composite RCC panels are attache... More

KENNEDY SPACE CENTER, FLA. -  United Space Alliance employee Anthony Simmons electrowelds a crack formed in the insulator inside a Reinforced Carbon Carbon panel.   The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony S...

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons electrowelds a crack formed in the insulator inside a Reinforced Carbon Carbon panel. The gray carbon composite RCC panels are atta... More

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons checks the electroweld he performed on an insulator inside a Reinforced Carbon Carbon panel.   The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Si...

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons checks the electroweld he performed on an insulator inside a Reinforced Carbon Carbon panel. The gray carbon composite RCC panels ar... More

KENNEDY SPACE CENTER, FLA. -  United Space Alliance employee Anthony Simmons electrowelds a crack formed in the insulator inside a Reinforced Carbon Carbon panel.   The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony S...

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons electrowelds a crack formed in the insulator inside a Reinforced Carbon Carbon panel. The gray carbon composite RCC panels are atta... More

KENNEDY SPACE CENTER, FLA. -   United Space Alliance employee Anthony Simmons prepares to electroweld a crack found on an insulator inside a Reinforced Carbon Carbon panel.   The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony ...

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons prepares to electroweld a crack found on an insulator inside a Reinforced Carbon Carbon panel. The gray carbon composite RCC panel... More

KENNEDY SPACE CENTER, FLA. -   United Space Alliance employee Anthony Simmons continues electrowelding on an insulator inside a Reinforced Carbon Carbon panel.   The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony ...

KENNEDY SPACE CENTER, FLA. - United Space Alliance employee Anthony Simmons continues electrowelding on an insulator inside a Reinforced Carbon Carbon panel. The gray carbon composite RCC panels are attache... More

KENNEDY SPACE CENTER, FLA. -  - In the Orbiter Processing Facility astronaut Danny Olivas listens to Greg Grantham (left) talking about the Reinforced Carbon Carbon panels used on the leading edge of the wing of the orbiters.  Behind Olivas are engineers from around the Agency who are working on improving the RCC panels used on the wing leading edge. The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - - In the Orbiter Processing Facility ast...

KENNEDY SPACE CENTER, FLA. - - In the Orbiter Processing Facility astronaut Danny Olivas listens to Greg Grantham (left) talking about the Reinforced Carbon Carbon panels used on the leading edge of the wing o... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, astronaut Michael E. Lopez-Alegria looks at the Reinforced Carbon Carbon panels used on the leading edge of the wing of the orbiters. He and engineers from around the Agency are on a fact-finding tour for improving the RCC panels used on the wing leading edge.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, astro...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, astronaut Michael E. Lopez-Alegria looks at the Reinforced Carbon Carbon panels used on the leading edge of the wing of the orbiters. He and engi... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, astronaut Scott E. Parazynski points to the Reinforced Carbon Carbon panels used on the leading edge of the wing of the orbiters. With Parazynski are engineers from around the Agency who are working on improving the RCC panels used on the wing leading edge.  The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, astr...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, astronaut Scott E. Parazynski points to the Reinforced Carbon Carbon panels used on the leading edge of the wing of the orbiters. With Parazynsk... More

KENNEDY SPACE CENTER, FLA. -  In the Orbiter Processing Facility, astronaut Scott E. Parazynski discusses the Reinforced Carbon Carbon panels used on the leading edge of the wing of the orbiters.  With him are engineers from around the Agency who are working on improving the RCC panels used on the wing leading edge. The gray carbon composite RCC panels have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, astr...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, astronaut Scott E. Parazynski discusses the Reinforced Carbon Carbon panels used on the leading edge of the wing of the orbiters. With him are ... More

KENNEDY SPACE CENTER, FLA. -- In the Space Life Sciences (SLS) Lab, Jan Bauer, with Dynamac Corp., weighs samples of onion tissue for processing in the elemental analyzer behind it.  The equipment analyzes for carbon, hydrogen, nitrogen and sulfur. The 100,000 square-foot SLS houses labs for NASA’s ongoing research efforts, microbiology/microbial ecology studies and analytical chemistry labs. Also calling the new lab home are facilities for space flight-experiment and flight-hardware development, new plant growth chambers, and an Orbiter Environment Simulator that will be used to conduct ground control experiments in simulated flight conditions for space flight experiments.  The SLS Lab, formerly known as the Space Experiment Research and Processing Laboratory or SERPL, provides space for NASA’s Life Sciences Services contractor Dynamac Corporation, Bionetics Corporation, and researchers from the University of Florida. NASA’s Office of Biological and Physical Research will use the facility for processing life sciences experiments that will be conducted on the International Space Station. The SLS Lab is the magnet facility for the International Space Research Park at KSC being developed in partnership with Florida Space Authority.

KENNEDY SPACE CENTER, FLA. -- In the Space Life Sciences (SLS) Lab, Ja...

KENNEDY SPACE CENTER, FLA. -- In the Space Life Sciences (SLS) Lab, Jan Bauer, with Dynamac Corp., weighs samples of onion tissue for processing in the elemental analyzer behind it. The equipment analyzes for ... More

KENNEDY SPACE CENTER, FLA. -- In the Space Life Sciences (SLS) Lab, Jan Bauer, with Dynamac Corp., places samples of onion tissue in the elemental analyzer, which analyzes for carbon, hydrogen, nitrogen and sulfur. The 100,000 square-foot SLS houses labs for NASA’s ongoing research efforts, microbiology/microbial ecology studies and analytical chemistry labs. Also calling the new lab home are facilities for space flight-experiment and flight-hardware development, new plant growth chambers, and an Orbiter Environment Simulator that will be used to conduct ground control experiments in simulated flight conditions for space flight experiments.  The SLS Lab, formerly known as the Space Experiment Research and Processing Laboratory or SERPL, provides space for NASA’s Life Sciences Services contractor Dynamac Corporation, Bionetics Corporation, and researchers from the University of Florida. NASA’s Office of Biological and Physical Research will use the facility for processing life sciences experiments that will be conducted on the International Space Station. The SLS Lab is the magnet facility for the International Space Research Park at KSC being developed in partnership with Florida Space Authority.

KENNEDY SPACE CENTER, FLA. -- In the Space Life Sciences (SLS) Lab, Ja...

KENNEDY SPACE CENTER, FLA. -- In the Space Life Sciences (SLS) Lab, Jan Bauer, with Dynamac Corp., places samples of onion tissue in the elemental analyzer, which analyzes for carbon, hydrogen, nitrogen and sul... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis. KSC-04pd0333

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, worke...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis. KSC-04pd0331

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, worke...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis. KSC-04pd0329

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, worke...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis.

KENNEDY SPACE CENTER, FLA. - - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis. KSC-04pd0332

KENNEDY SPACE CENTER, FLA. - - In the Orbiter Processing Facility, wor...

KENNEDY SPACE CENTER, FLA. - - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis. KSC-04pd0334

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, worke...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers install C-shaped T-seals, which fit between each Reinforced Carbon Carbon panel, on the left-side wing leading edge of the orbiter Atlantis.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers wipe down the Reinforced Carbon Carbon panels on Atlantis’ left-side wing leading edge in preparation for installing the C-shaped T-seals, which fit between each panel. KSC-04pd0330

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, worke...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, workers wipe down the Reinforced Carbon Carbon panels on Atlantis’ left-side wing leading edge in preparation for installing the C-shaped T-seals... More

KENNEDY SPACE CENTER, FLA. -  In the middeck of Endeavour, in the Orbiter Processing Facility, Center Director Jim Kennedy (far left) watches as a technician gets ready to lower himself through the LiOH door into the Environmental Control and Life Support System (ECLSS) bay. LiOH refers to lithium hydroxide, canisters of which are stored in the ECLSS bay under the middeck floor. During flight, cabin air from the cabin fan is ducted to two LiOH canisters, where carbon dioxide is removed and activated charcoal removes odors and trace contaminants.  Kennedy is taking an opportunity to learn first-hand what workers are doing to enable Return to Flight.  Endeavour is in an Orbiter Major Modification period. KSC-04pd0545

KENNEDY SPACE CENTER, FLA. - In the middeck of Endeavour, in the Orbi...

KENNEDY SPACE CENTER, FLA. - In the middeck of Endeavour, in the Orbiter Processing Facility, Center Director Jim Kennedy (far left) watches as a technician gets ready to lower himself through the LiOH door in... More

KENNEDY SPACE CENTER, FLA. -  Jim Landy, NDE specialist with United Space Alliance (USA), examines a Reinforced Carbon Carbon panel using flash thermography.  A relatively new procedure at KSC, thermography uses high intensity light to heat areas of the panels. The panels are then immediately scanned with an infrared camera. As the panels cool, any internal flaws are revealed. The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters.  They have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.  The panels will be installed on the orbiter Discovery, designated for the first Return to Flight mission, STS-114.

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Sp...

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Space Alliance (USA), examines a Reinforced Carbon Carbon panel using flash thermography. A relatively new procedure at KSC, thermography use... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF), a United Space Alliance technician examines the attachment points for the spars on the exterior of a wing of Space Shuttle Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.  The next launch of Atlantis will be on mission STS-114, a utilization and logistics flight to the International Space Station.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF),...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF), a United Space Alliance technician examines the attachment points for the spars on the exterior of a wing of Space Shuttle Atlantis. Reinfo... More

KENNEDY SPACE CENTER, FLA. -  Dan Phillips (left) and Donald Nielen, with United Space Alliance, watch a monitor as  Jim Landy, NDE specialist with USA, prepares to examine a Reinforced Carbon Carbon panel (on the table, center) using flash thermography.  A relatively new procedure at KSC, thermography uses high intensity light to heat areas of the panels. The panels are then immediately scanned with an infrared camera. As the panels cool, any internal flaws are revealed. The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters.  They have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.  The panels will be installed on the orbiter Discovery, designated  for the first Return to Flight mission, STS-114.

KENNEDY SPACE CENTER, FLA. - Dan Phillips (left) and Donald Nielen, w...

KENNEDY SPACE CENTER, FLA. - Dan Phillips (left) and Donald Nielen, with United Space Alliance, watch a monitor as Jim Landy, NDE specialist with USA, prepares to examine a Reinforced Carbon Carbon panel (on ... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF), United Space Alliance technicians replace the attachment points for the spars on the interior of a wing of Space Shuttle Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.  The next launch of Atlantis will be on mission STS-114, a utilization and logistics flight to the International Space Station.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF),...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF), United Space Alliance technicians replace the attachment points for the spars on the interior of a wing of Space Shuttle Atlantis. Reinforc... More

KENNEDY SPACE CENTER, FLA. -  Jim Landy, NDE specialist with United Space Alliance, sets up equipment to examine a Reinforced Carbon Carbon panel using flash thermography.  A relatively new procedure at KSC, thermography uses high intensity light to heat areas of the panels. The panels are then immediately scanned with an infrared camera. As the panels cool, any internal flaws are revealed. The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters.  They have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.  The panels will be installed on the orbiter Discovery, designated  for the first Return to Flight mission, STS-114.

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Sp...

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Space Alliance, sets up equipment to examine a Reinforced Carbon Carbon panel using flash thermography. A relatively new procedure at KSC, th... More

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, technicians Jake Jacobson (left) and Billy Barecka install a reinforced carbon carbon panel on the right wing of Space Shuttle Discovery.  The next flight planned for Discovery is the STS-114 mission on Logistics Flight 1 to deliver supplies and equipment, as well as the external stowage platform, to the International Space Station. STS-114 will be the mission that returns the Space Shuttle to flight status and is scheduled for no earlier than March 2005. KSC-04pd1131

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, tech...

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, technicians Jake Jacobson (left) and Billy Barecka install a reinforced carbon carbon panel on the right wing of Space Shuttle Discovery. The n... More

KENNEDY SPACE CENTER, FLA. -In the Orbiter Processing Facility (OPF), a United Space Alliance technician examines the attachment points for the spars on the exterior of a wing of Space Shuttle Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.  The next launch of Atlantis will be on mission STS-114, a utilization and logistics flight to the International Space Station.

KENNEDY SPACE CENTER, FLA. -In the Orbiter Processing Facility (OPF), ...

KENNEDY SPACE CENTER, FLA. -In the Orbiter Processing Facility (OPF), a United Space Alliance technician examines the attachment points for the spars on the exterior of a wing of Space Shuttle Atlantis. Reinfor... More

KENNEDY SPACE CENTER, FLA. -  Jim Landy, NDE specialist with United Space Alliance (USA), prepares equipment to examine a Reinforced Carbon Carbon panel using flash thermography.  A relatively new procedure at KSC, thermography uses high intensity light to heat areas of the panels. The panels are then immediately scanned with an infrared camera. As the panels cool, any internal flaws are revealed. The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters.  They have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry. The panels will be installed on the orbiter Discovery, designated for the first Return to Flight mission, STS-114.

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Sp...

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Space Alliance (USA), prepares equipment to examine a Reinforced Carbon Carbon panel using flash thermography. A relatively new procedure at ... More

KENNEDY SPACE CENTER, FLA. -  Jim Landy, NDE specialist with USA, points to   an area of a Reinforced Carbon Carbon panel just examined using flash thermography. A relatively new procedure at KSC, thermography uses high intensity light to heat areas of the panels. The panels are then immediately scanned with an infrared camera. As the panels cool, any internal flaws are revealed. The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters.  They have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.  The panels will be installed on the orbiter Discovery, designated  for the first Return to Flight mission, STS-114.

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with USA, poin...

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with USA, points to an area of a Reinforced Carbon Carbon panel just examined using flash thermography. A relatively new procedure at KSC, thermography ... More

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, technicians Mike McCall (left) and Jake Jacobson install a reinforced carbon carbon panel on the right wing of Space Shuttle Discovery. The next flight planned for Discovery is the STS-114 mission on Logistics Flight 1 to deliver supplies and equipment, as well as the external stowage platform, to the International Space Station. STS-114 will be the mission that returns the Space Shuttle to flight status and is scheduled for no earlier than March 2005. KSC-04pd1129

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, tech...

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, technicians Mike McCall (left) and Jake Jacobson install a reinforced carbon carbon panel on the right wing of Space Shuttle Discovery. The next... More

KENNEDY SPACE CENTER, FLA. -  Jim Landy, NDE specialist with USA, looks closely at an area of a Reinforced Carbon Carbon panel just examined using flash thermography. A relatively new procedure at KSC, thermography uses high intensity light to heat areas of the panels. The panels are then immediately scanned with an infrared camera. As the panels cool, any internal flaws are revealed. The gray carbon composite RCC panels are attached to the leading edge of the wing of the orbiters.  They have sufficient strength to withstand the aerodynamic forces experienced during launch and reentry, which can reach as high as 800 pounds per square foot.  The operating range of RCC is from minus 250º F to about 3,000º F, the temperature produced by friction with the atmosphere during reentry.  The panels will be installed on the orbiter Discovery, designated for the first Return to Flight mission, STS-114. KSC-04pd0450

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with USA, look...

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with USA, looks closely at an area of a Reinforced Carbon Carbon panel just examined using flash thermography. A relatively new procedure at KSC, thermogr... More

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF), a United Space Alliance technician examines the attachment points for the spars on the exterior of a wing of Space Shuttle Atlantis. Reinforced Carbon Carbon (RCC) panels are mechanically attached to the wing with a series of floating joints - spars - to reduce loading on the panels caused by wing deflections. The aluminum and the metallic attachments are protected from exceeding temperature limits by internal insulation.  The next launch of Atlantis will be on mission STS-114, a utilization and logistics flight to the International Space Station.

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF),...

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility (OPF), a United Space Alliance technician examines the attachment points for the spars on the exterior of a wing of Space Shuttle Atlantis. Reinfo... More

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, technician Mike McCall installs a reinforced carbon carbon panel on the right wing of Space Shuttle Discovery. The next flight planned for Discovery is the STS-114 mission on Logistics Flight 1 to deliver supplies and equipment, as well as the external stowage platform, to the International Space Station. STS-114 will be the mission that returns the Space Shuttle to flight status and is scheduled for no earlier than March 2005. KSC-04pd1130

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, tech...

KENNEDY SPACE CENTER, FLA. -- In the Orbiter Processing Facility, technician Mike McCall installs a reinforced carbon carbon panel on the right wing of Space Shuttle Discovery. The next flight planned for Disco... More

VANDENBERG AIR FORCE BASE, Calif. --  At Vandenberg AFB, the first stage of the Taurus rocket is being moved into Building 1555's west bay.  The Taurus will launch the Orbiting Carbon Observatory, or OCO, in 2009.  The OCO is a new Earth-orbiting mission sponsored by NASA's Earth System Science Pathfinder Program.  Photo credit: NASA/Randy Beaudoin KSC-08pd1883

VANDENBERG AIR FORCE BASE, Calif. -- At Vandenberg AFB, the first sta...

VANDENBERG AIR FORCE BASE, Calif. -- At Vandenberg AFB, the first stage of the Taurus rocket is being moved into Building 1555's west bay. The Taurus will launch the Orbiting Carbon Observatory, or OCO, in 20... More

VANDENBERG AIR FORCE BASE, Calif. --   In Building 1555's west bay at Vandenberg AFB, workers secure the strapping holding the third stage of the Taurus rocket on the assembly integration trailer.  The Taurus will launch the Orbiting Carbon Observatory, or OCO, in 2009.  The OCO is a new Earth-orbiting mission sponsored by NASA's Earth System Science Pathfinder Program.  Photo credit: NASA/Randy Beaudoin KSC-08pd1874

VANDENBERG AIR FORCE BASE, Calif. -- In Building 1555's west bay at ...

VANDENBERG AIR FORCE BASE, Calif. -- In Building 1555's west bay at Vandenberg AFB, workers secure the strapping holding the third stage of the Taurus rocket on the assembly integration trailer. The Taurus w... More

VANDENBERG AIR FORCE BASE, Calif. --  In Building 1555's west bay at Vandenberg AFB, the third and second stages of the Taurus rocket rest on the stationary rails. The Taurus will launch the Orbiting Carbon Observatory, or OCO, in 2009.  The OCO is a new Earth-orbiting mission sponsored by NASA's Earth System Science Pathfinder Program.  Photo credit: NASA/Randy Beaudoin KSC-08pd1880

VANDENBERG AIR FORCE BASE, Calif. -- In Building 1555's west bay at V...

VANDENBERG AIR FORCE BASE, Calif. -- In Building 1555's west bay at Vandenberg AFB, the third and second stages of the Taurus rocket rest on the stationary rails. The Taurus will launch the Orbiting Carbon Obs... More

VANDENBERG AIR FORCE BASE, Calif. --  At Vandenberg AFB, the first stage of the Taurus rocket is being moved onto the stationary rails in Building 1555's west bay. The Taurus will launch the Orbiting Carbon Observatory, or OCO, in 2009.  The OCO is a new Earth-orbiting mission sponsored by NASA's Earth System Science Pathfinder Program.  Photo credit: NASA/Randy Beaudoin KSC-08pd1884

VANDENBERG AIR FORCE BASE, Calif. -- At Vandenberg AFB, the first sta...

VANDENBERG AIR FORCE BASE, Calif. -- At Vandenberg AFB, the first stage of the Taurus rocket is being moved onto the stationary rails in Building 1555's west bay. The Taurus will launch the Orbiting Carbon Obs... More

VANDENBERG AIR FORCE BASE, Calif. --  At Vandenberg AFB, the first stage of the Taurus rocket is moved out of the transportation trailer onto the assembly integration trailer.  The Taurus will launch the Orbiting Carbon Observatory, or OCO, in 2009.  The OCO is a new Earth-orbiting mission sponsored by NASA's Earth System Science Pathfinder Program.  Photo credit: NASA/Randy Beaudoin KSC-08pd1881

VANDENBERG AIR FORCE BASE, Calif. -- At Vandenberg AFB, the first sta...

VANDENBERG AIR FORCE BASE, Calif. -- At Vandenberg AFB, the first stage of the Taurus rocket is moved out of the transportation trailer onto the assembly integration trailer. The Taurus will launch the Orbiti... More

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