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Showing results for "RCC"

269 results found - Page 4 of 12

NASA image: KSC-2010-1247
Image
Jan 14, 2010

KSC-2010-1247

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility 1 at NASA's Kennedy Space Center in Florida, United Space...

KSC
NASA image: KSC-2010-1249
Image
Jan 14, 2010

KSC-2010-1249

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility 1 at NASA's Kennedy Space Center in Florida, United Space...

KSC
NASA image: KSC-2010-1244
Image
Jan 14, 2010

KSC-2010-1244

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility 1 at NASA's Kennedy Space Center in Florida, United Space...

KSC
NASA image: KSC-2010-1248
Image
Jan 14, 2010

KSC-2010-1248

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility 1 at NASA's Kennedy Space Center in Florida, a team of United...

KSC
NASA image: KSC-2010-1246
Image
Jan 14, 2010

KSC-2010-1246

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility 1 at NASA's Kennedy Space Center in Florida, United Space...

KSC
NASA image: 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.
Image
Mar 10, 2004

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.

NASA image: 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.
Image
Mar 10, 2004

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.

NASA image: 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.
Image
Mar 10, 2004

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.

NASA image: 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.
Image
Mar 10, 2004

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.

NASA image: 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.
Image
Mar 10, 2004

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.

NASA image: KSC-05pd-0118
Image
Jan 10, 2005

KSC-05pd-0118

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Matt Scott and Mel Romans (left and right), with...

KSC
NASA image: KSC-05pd-0121
Image
Jan 10, 2005

KSC-05pd-0121

KENNEDY SPACE CENTER, FLA. - Matt Scott, with United Space Alliance, lifts the final Reinforced Carbon-Carbon (RCC)...

KSC
NASA image: KSC-05pd-0120
Image
Jan 10, 2005

KSC-05pd-0120

KENNEDY SPACE CENTER, FLA. - In the Orbiter Processing Facility, Mel Romans, with United Space Alliance, prepares...

KSC
NASA image: KSC-04pd1426
Image
Jul 7, 2004

KSC-04pd1426

KENNEDY SPACE CENTER, FLA. - Workers in the Orbiter Processing Facility check the placement of the Reinforced...

KSC
NASA image: KSC-04pd1425
Image
Jul 7, 2004

KSC-04pd1425

KENNEDY SPACE CENTER, FLA. - Workers in the Orbiter Processing Facility lift the Reinforced Carbon-Carbon (RCC) chin...

KSC
NASA image: Camarada on middeck
Image
Aug 4, 2005

Camarada on middeck

S114-E-7003 (4 August 2005) --- Astronaut Charles J. Camarda, STS-114 mission specialist, performs a middeck...

JSC
NASA image: KSC-04pd1424
Image
Jul 7, 2004

KSC-04pd1424

KENNEDY SPACE CENTER, FLA. - Workers in the Orbiter Processing Facility lift the Reinforced Carbon-Carbon (RCC) chin...

KSC
NASA image: Camarada and Thomas on middeck
Image
Aug 7, 2005

Camarada and Thomas on middeck

S114-E-7001 (4 August 2005) --- Astronaut Andrew S. W. Thomas, STS-114 mission specialist, photographs a middeck...

JSC
NASA image: KSC-04pd1423
Image
Jul 7, 2004

KSC-04pd1423

KENNEDY SPACE CENTER, FLA. - Workers in the Orbiter Processing Facility prepare the Reinforced Carbon-Carbon (RCC)...

KSC
NASA image: Thomas and Camarda on middeck
Image
Aug 4, 2005

Thomas and Camarda on middeck

S114-E-7005 (4 August 2005) --- Astronaut Andrew S. W. Thomas, STS-114 mission specialist, photographs a middeck...

JSC
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. - 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...

NASA image: 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.
Image
Aug 22, 2003

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 Alliance, prepares to install a spar on the wing...

KSC
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KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Space Alliance (USA), examines a Reinforced...

KSC

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with USA, points to an area of a Reinforced Carbon Carbon...

KSC

KENNEDY SPACE CENTER, FLA. - Dan Phillips (left) and Donald Nielen, with United Space Alliance, watch a monitor as...

KSC

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Space Alliance, sets up equipment to examine a...

KSC

KENNEDY SPACE CENTER, FLA. - Jim Landy, NDE specialist with United Space Alliance (USA), prepares equipment to...

KSC
KSC