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NASA's Image and Video Library is one of the most comprehensive public archives of space imagery in the world, containing over 140,000 images, videos, and audio recordings spanning more than six decades of space exploration. From the earliest Mercury and Gemini missions through the Apollo Moon landings, the Space Shuttle era, and today's cutting-edge observations from the James Webb Space Telescope, this collection documents humanity's journey into the cosmos.

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Use the search bar above to find specific subjects — try queries like "Apollo 11," "Hubble Deep Field," "Mars surface," or "astronaut EVA." You can also filter by media type (image, video, or audio). For a daily curated experience, visit the Astronomy Picture of the Day.

Showing results for "Carbon-Carbon"

2,471 results found - Page 14 of 103

NASA image: 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.
Image
Sep 9, 2003

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, United Space Alliance worker Dan Kenna (right)...

KSC
NASA image: 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.
Image
Sep 9, 2003

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, United Space Alliance workers share the task of...

NASA image: 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.
Image
Sep 9, 2003

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 Landy, NDE specialist with United Space...

NASA image: 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.
Image
Sep 9, 2003

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 Landy (left), NDE specialist with United Space...

NASA image: 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.
Image
Sep 9, 2003

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, United Space Alliance workers (left to right) Jim...

NASA image: 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.
Image
Sep 9, 2003

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, United Space Alliance workers Jim Landy (front),...

NASA image: 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.
Image
Sep 9, 2003

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, United Space Alliance workers (left to right) Jim...

NASA image: 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.
Image
Sep 5, 2003

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, United Space Alliance workers Mike Hyatt (left)...

NASA image: 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.
Image
Dec 8, 2003

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, astronaut Scott E. Parazynski points to the...

NASA image: 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.
Image
Sep 8, 2003

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, United Space Alliance workers Mike Hyatt (above)...

KSC
NASA image: 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.
Image
Sep 8, 2003

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, United Space Alliance workers Mike Hyatt (above),...

KSC
NASA image: 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.
Image
Sep 5, 2003

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, United Space Alliance worker Mike Hyatt attaches a...

KSC
NASA image: 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.
Image
Sep 9, 2003

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, United Space Alliance workers Dan Kenna and Jim...

KSC
NASA image: 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.
Image
Sep 5, 2003

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, United Space Alliance worker Mike Hyatt (right)...

KSC
NASA image: Carbon Monoxide in Mid-Troposphere over Indonesia Fires, October 2015
Image
Oct 30, 2015

Carbon Monoxide in Mid-Troposphere over Indonesia Fires, October 2015

Widespread forest fires across Indonesia have burned tens of thousands of acres over three months, causing high...

JPL
NASA image: Imaging Spectrometer Vibration Test
Image
Sep 14, 2023

Imaging Spectrometer Vibration Test

Engineers and technicians prepare the Carbon Mapper imaging spectrometer, which will measure the greenhouse gases...

JPL
NASA image: Spring Frost on a Cold World
Image
Nov 27, 2018

Spring Frost on a Cold World

Winter on Mars comes with a blanket of carbon dioxide snow. During the spring "thaw," this snow evaporates into the...

JPL
NASA image: Amazon Canopy Comes to Life through Laser Data
Video
Jun 12, 2018

Amazon Canopy Comes to Life through Laser Data

Flying over the Brazilian Amazon with an instrument firing 300,000 laser pulses per second, NASA scientists have...

GSFC
NASA image: Imaging Spectrometer Vacuum Chamber Test
Image
Sep 14, 2023

Imaging Spectrometer Vacuum Chamber Test

An engineer prepares the Carbon Mapper imaging spectrometer, which will measure the greenhouse gases methane and...

JPL
NASA image: 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.
Image
Sep 4, 2003

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 Hyatt (above) and Saul Ngy (below), with...

KSC
NASA image: 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.
Image
Sep 5, 2003

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 as he examines the spar installation (behind...

KSC
NASA image: KENNEDY SPACE CENTER, FLA. - NASA Vehicle Manager Scott Thurston (left) talks to a phalanx of media in the Orbiter Processing Facility. The media was invited to see the orbiter Atlantis as it is being prepared for Return to Flight. Both local and national reporters representing print and TV networks were able to see work in progress on Atlantis, including the reinstallation of the Reinforced Carbon-Carbon panels on the orbiter’s wing leading edge; wiring inspections; and checks of the engines in the Orbital Maneuvering System.
Image
Sep 26, 2003

KENNEDY SPACE CENTER, FLA. - NASA Vehicle Manager Scott Thurston (left) talks to a phalanx of media in the Orbiter Processing Facility. The media was invited to see the orbiter Atlantis as it is being prepared for Return to Flight. Both local and national reporters representing print and TV networks were able to see work in progress on Atlantis, including the reinstallation of the Reinforced Carbon-Carbon panels on the orbiter’s wing leading edge; wiring inspections; and checks of the engines in the Orbital Maneuvering System.

KENNEDY SPACE CENTER, FLA. - NASA Vehicle Manager Scott Thurston (left) talks to a phalanx of media in the Orbiter...

KSC
NASA image: KENNEDY SPACE CENTER, FLA. - NASA Vehicle Manager Scott Thurston (right) talks to the media in the Orbiter Processing Facility . The media was invited to see the orbiter Atlantis as it is being prepared for Return to Flight. Both local and national reporters representing print and TV networks were able to see work in progress on Atlantis, including the reinstallation of the Reinforced Carbon-Carbon panels on the orbiter’s wing leading edge; wiring inspections; and checks of the engines in the Orbital Maneuvering System.
Image
Sep 26, 2003

KENNEDY SPACE CENTER, FLA. - NASA Vehicle Manager Scott Thurston (right) talks to the media in the Orbiter Processing Facility . The media was invited to see the orbiter Atlantis as it is being prepared for Return to Flight. Both local and national reporters representing print and TV networks were able to see work in progress on Atlantis, including the reinstallation of the Reinforced Carbon-Carbon panels on the orbiter’s wing leading edge; wiring inspections; and checks of the engines in the Orbital Maneuvering System.

KENNEDY SPACE CENTER, FLA. - NASA Vehicle Manager Scott Thurston (right) talks to the media in the Orbiter...

KSC
NASA image: 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.
Image
Sep 3, 2003

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), a United Space Alliance technician examines...

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