NASA Media Archive
KENNEDY SPACE CENTER, FLA. - In the Vehicle Assembly Building, Jim Landy, NDE specialist, performs flash thermography on flight crew lockers. He is screening the lockers for hidden damage underneath dings and dents that might occur during handling.
KSC-03pd2548
KSC | 2003-09-04
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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.
KSC-03pd2531
KSC | 2003-09-04
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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.
KSC-03pd2533
KSC | 2003-09-04
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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.
KSC-03pd2532
KSC | 2003-09-04
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KENNEDY SPACE CENTER, FLA. - In the Vehicle Assembly Building, Jim Landy, NDE specialist, sets up a flight crew lockers for flash thermography. He is screening the lockers for hidden damage underneath dings and dents that might occur during handling.
KSC-03pd2550
KSC | 2003-09-04
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Expedition Seven Malenchenko and Lu wearing Sokol pressure suit in Destiny laboratory
iss007e14437
JSC | 2003-09-04
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KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, while Greg Harlow, with United Space Alliance (USA), (above) threads a camera under the tiles of the orbiter Endeavour, Peggy Ritchie, with USA, (behind the stand) and NASA’s Richard Parker watch the images on a monitor to inspect for corrosion.
KSC-03pd2541
KSC | 2003-09-04
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KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, while Greg Harlow, with United Space Alliance (USA) (above) threads a camera under the tiles of the orbiter Endeavour, Peggy Ritchie, USA, (behind the stand) and NASA’s Richard Parker (seated) watch the images on a monitor to inspect for corrosion.
KSC-03pd2538
KSC | 2003-09-04
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KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Richard Parker, with NASA, watches a monitor showing images from a camera inserted beneath tiles of the orbiter Endeavour to inspect for corrosion.
KSC-03pd2540
KSC | 2003-09-04
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Expedition Seven Lu wearing Sokol pressure suit in Destiny laboratory
iss007e14440
JSC | 2003-09-04
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Expedition Seven Malenchenko wearing Sokol pressure suit in Destiny laboratory
iss007e14441
JSC | 2003-09-04
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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.
KSC-03pd2535
KSC | 2003-09-04
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KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Greg Harlow, with United Space Alliance (USA), threads a camera under the tiles of the orbiter Endeavour to inspect for corrosion.
KSC-03pd2539
KSC | 2003-09-04
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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.
KSC-03pd2534
KSC | 2003-09-04
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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.
KSC-03pd2491
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - This bird's-eye view of a high bay in the Orbiter Processing Facility (OPF) shows Space Shuttle Atlantis surrounded by the standard platforms and equipment required to process a Space Shuttle orbiter for flight. The high bay is 197 feet (60 meters) long, 150 feet (46 meters) wide, 95 feet (29 meters) high, and encompasses a 29,000-square-foot (2,694-meter) area. Platforms, a main access bridge, and two rolling bridges with trucks provide access to various parts of the orbiter. The next mission scheduled for Atlantis is STS-114, a utilization and logistics flight to the International Space Station.
KSC-03pd2487
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - John Macke (standing, center), with Boeing St. Louis, Alden Pitard (seated, left) and Dan Clark (right), with KSC Boeing, check results after 3D digital scanning of actuators in the Orbiter Processing Facility. There are two actuators per engine on the Shuttle, one for pitch motion and one for yaw motion. The Space Shuttle Main Engine hydraulic servoactuators are used to gimbal the main engine.
KSC-03pd2510
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - Astronaut Soichi Noguchi, with the National Space Development Agency of Japan (NASDA), rests inside the Japanese Experiment Module (JEM), undergoing a Multi-Element Integrated Test (MEIT) in the Space Station Processing Facility. Noguchi is assigned to mission STS-114 as a mission specialist. Node 2 attaches to the end of the U.S. Lab on the ISS and provides attach locations for the Japanese laboratory, European laboratory, the Centrifuge Accommodation Module and, eventually, Multipurpose Logistics Modules. It will provide the primary docking location for the Shuttle when a pressurized mating adapter is attached to Node 2. Installation of the module will complete the U.S. Core of the ISS. The JEM, developed by NASDA, is Japan's primary contribution to the Station. It will enhance the unique research capabilities of the orbiting complex by providing an additional environment for astronauts to conduct science experiments.
KSC-03pd2525
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - Astronaut Soichi Noguchi (left), with the National Space Development Agency of Japan (NASDA), points to data on the console during a Multi-Element Integrated Test (MEIT) of the U.S. Node 2 and the Japanese Experiment Module (JEM) in the Space Station Processing Facility. The JEM, developed by NASDA, is Japan's primary contribution to the Station. It will enhance the unique research capabilities of the orbiting complex by providing an additional environment for astronauts to conduct science experiments. Noguchi is assigned to mission STS-114 as a mission specialist. Node 2 provides attach locations for the Japanese laboratory, as well as European laboratory, the Centrifuge Accommodation Module and, eventually, Multipurpose Logistics Modules. Installation of the module will complete the U.S. Core of the ISS.
KSC-03pd2546
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - Astronaut Soichi Noguchi, with the National Space Development Agency of Japan (NASDA), signals success during a Multi-Element Integrated Test (MEIT ) of the Japanese Experiment Module (JEM) in the Space Station Processing Facility. Noguchi is assigned to mission STS-114 as a mission specialist. Node 2 attaches to the end of the U.S. Lab on the ISS and provides attach locations for the Japanese laboratory, European laboratory, the Centrifuge Accommodation Module and, eventually, Multipurpose Logistics Modules. It will provide the primary docking location for the Shuttle when a pressurized mating adapter is attached to Node 2. Installation of the module will complete the U.S. Core of the ISS. The JEM, developed by NASDA, is Japan's primary contribution to the Station. It will enhance the unique research capabilities of the orbiting complex by providing an additional environment for astronauts to conduct science experiments.
KSC-03pd2526
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - Workers in the Space Station Processing Facility observe consoles during a Multi-Element Integrated Test (MEIT) of the U.S. Node 2 and the Japanese Experiment Module (JEM). Node 2 attaches to the end of the U.S. Lab on the ISS and provides attach locations for the Japanese laboratory, European laboratory, the Centrifuge Accommodation Module and, eventually, Multipurpose Logistics Modules. It will provide the primary docking location for the Shuttle when a pressurized mating adapter is attached to Node 2. Installation of the module will complete the U.S. Core of the ISS. The JEM, developed by the National Space Development Agency of Japan (NASDA), is Japan's primary contribution to the Station. It will enhance the unique research capabilities of the orbiting complex by providing an additional environment for astronauts to conduct science experiments.
KSC-03pd2518
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - Various elements intended for the International Space Station are lined up in the Space Station Processing Facility. The newest to arrive at KSC are in the rear: at left, the U.S. Node 2, and next to it at right, the Japanese Experiment Module (JEM). The two elements are undergoing a Multi-Element Integrated Test (MEIT). Node 2 attaches to the end of the U.S. Lab on the ISS and provides attach locations for the Japanese laboratory, European laboratory, the Centrifuge Accommodation Module and, eventually, Multipurpose Logistics Modules. It will provide the primary docking location for the Shuttle when a pressurized mating adapter is attached to Node 2. Installation of the module will complete the U.S. Core of the ISS. Developed by the National Space Development Agency of Japan (NASDA), the JEM is Japan's primary contribution to the Station. It will enhance the unique research capabilities of the orbiting complex by providing an additional environment for astronauts to conduct science experiments.
KSC-03pd2528
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - Workers in the Space Station Processing Facility are lined up at consoles during a Multi-Element Integrated Test (MEIT ) of the Japanese Experiment Module (JEM) and U.S. Node 2. Node 2 attaches to the end of the U.S. Lab on the ISS and provides attach locations for the Japanese laboratory, European laboratory, the Centrifuge Accommodation Module and, eventually, Multipurpose Logistics Modules. It will provide the primary docking location for the Shuttle when a pressurized mating adapter is attached to Node 2. Installation of the module will complete the U.S. Core of the ISS. The JEM, developed by NASDA, is Japan's primary contribution to the Station. It will enhance the unique research capabilities of the orbiting complex by providing an additional environment for astronauts to conduct science experiments.
KSC-03pd2527
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - A tracking telescope, part of the Distant Object Attitude Measurement System (DOAMS), is being calibrated. The telescope, which is located in Cocoa Beach, Fla., provides optical support for launches from KSC and Cape Canaveral.
KSC-03pd2503
KSC | 2003-09-03
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KENNEDY SPACE CENTER, FLA. - John Macke (standing, left), with Boeing St. Louis, Alden Pitard (seated, left) and Dan Clark (right), with KSC Boeing, look at a monitor after 3D digital scanning of actuators in the Orbiter Processing Facility. There are two actuators per engine on the Shuttle, one for pitch motion and one for yaw motion. The Space Shuttle Main Engine hydraulic servoactuators are used to gimbal the main engine.
KSC-03pd2509
KSC | 2003-09-03
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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.
KSC-03pd2489
KSC | 2003-09-03
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