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CAPE CANAVERAL, Fla. – At the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, hardware that will be used in the launch of the Ares I-X rocket is being offloaded from the C-5 aircraft. The hardware consists of a precisely machined, full-scale simulator crew module and launch abort system to form the tip of NASA's Ares I-X rocket. The launch of the 321-foot-tall, full-scale Ares I-X, targeted for July 2009, will be the first in a series of unpiloted rocket launches from Kennedy. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for the astronauts, while their launch abort system will provide safe evacuation if a launch vehicle failure occurs. Photo credit: NASA/Jack Pfaller KSC-2009-1405

CAPE CANAVERAL, Fla. – At the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, hardware that will be used in the launch of the Ares I-X rocket is being offloaded from the C-5 aircraft. The ha More

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility bay 3 at NASA's Kennedy Space Center in Florida, (at left) one of three space shuttle main engines is being prepared for installation in space shuttle Discovery. Each engine is 14 feet long, weighs about 6,700 pounds, and is 7.5 feet in diameter at the end of the nozzle. Discovery is being processed for its next mission, STS-119, targeted for launch on Feb. 12, 2009. Discovery and its crew will deliver integrated truss structure 6 (S6) and solar arrays to the International Space Station. Photo credit: NASA/Dimitri Gerondidakis KSC-08pd2943

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility bay 3 at NASA's Kennedy Space Center in Florida, (at left) one of three space shuttle main engines is being prepared for installation in space shuttle Disco More

CAPE CANAVERAL, Fla. -- In Orbiter Processing Facility-1 at NASA's Kennedy Space Center in Florida, engine #2, the last of three space shuttle main engines is installed in shuttle Atlantis. Each engine is 14 feet long, weighs about 6,700 pounds, and is 7.5 feet in diameter at the end of the nozzle. This is the final planned engine installation for the Space Shuttle Program. Atlantis is being prepared for the "launch on need," or potential rescue mission, for the final planned shuttle flight, Endeavour's STS-134 mission. For more information, visit www.nasa.gov/shuttle. Photo credit: NASA/Kim Shiflett KSC-2010-5828

CAPE CANAVERAL, Fla. -- In Orbiter Processing Facility-1 at NASA's Kennedy Space Center in Florida, engine #2, the last of three space shuttle main engines is installed in shuttle Atlantis. Each engine is More

In the Space Station Processing Facility, workers help guide the Multi-Purpose Logistics Module Leonardo as it moves toward the weight and balance scale. The Italian-built MPLM is one of three such pressurized modules that will serve as the International Space Station's "moving vans," carrying laboratory racks filled with equipment, experiments and supplies to and from the station aboard the Space Shuttle. The cylindrical module is approximately 21 feet long and 15 feet in diameter, weighing almost 4.1 metric tons. It can carry up to 9.1 metric tons of cargo packed into 16 standard space station equipment racks. The Leonardo will be launched on mission STS-102 March 8. On that flight, Leonardo will be filled with equipment and supplies to outfit the U.S. laboratory module, to be carried to the ISS on the Feb. 7 launch of STS-98 KSC-01pp0253

In the Space Station Processing Facility, workers help guide the Multi-Purpose Logistics Module Leonardo as it moves toward the weight and balance scale. The Italian-built MPLM is one of three such pressurized More

KENNEDY SPACE CENTER, FLA. -- The nose of NASA's Super Guppy aircraft opens to reveal the /2000/78-00.htm">Joint Airlock Module</a> the gateway from which crew members aboard the International Space Station (ISS) will enter and exit the 470-ton orbiting research facility. The airlock was transported from NASA's Marshall Space Flight Center in Huntsville, Ala. The airlock will be transported to the Operations and Checkout Building in the KSC industrial area where it will undergo vacuum chamber testing. It will then be moved to the Space Station Processing Facility (SSPF) for further prelaunch preparation and checkout. The massive, spindle-shaped airlock is 20 feet long, has a diameter of 13 feet at its widest point, and weighs six and a half tons. It was manufactured at NASA's Marshall Space Flight Center by the Huntsville division of The Boeing Company. The Space Shuttle Atlantis will carry the airlock to orbit on mission STS-104, the tenth International Space Station flight, currently targeted for liftoff in May 2001 KSC00pp1344

KENNEDY SPACE CENTER, FLA. -- The nose of NASA's Super Guppy aircraft opens to reveal the kscpao/release/2000/78-00.htm">Joint Airlock Module</a> the gateway from which crew members aboard the International Spa More

CAPE CANAVERAL, Fla. – In the Space Station Processing Facility at NASA's Kennedy Space Center in Florida, Bernardo Patti, at left, head of International Space Station, Program Department, European Space Agency, and Michael Suffredini, program manager, International Space Station, NASA, sign documents transferring the ownership of node 3 for the International Space Station from the European Space Agency, or ESA, to NASA. Node 3 is named "Tranquility" after the Sea of Tranquility, the lunar landing site of Apollo 11. The payload for the STS-130 mission, Tranquility is a pressurized module that will provide room for many of the International Space Station's life support systems. The module was built for ESA by Thales Alenia Space in Turin, Italy. Attached to one end of Tranquility is a cupola, a unique work station with six windows on its sides and one on top. The cupola resembles a circular bay window and will provide a vastly improved view of the station's exterior. Just under 10 feet in diameter, the module will accommodate two crew members and portable workstations that can control station and robotic activities. The multi-directional view will allow the crew to monitor spacewalks and docking operations, as well as provide a spectacular view of Earth and other celestial objects. Space shuttle Endeavour's STS-130 mission is targeted to launch Feb. 4, 2010. Photo credit: NASA/Kim Shiflett KSC-2009-6511

CAPE CANAVERAL, Fla. – In the Space Station Processing Facility at NASA's Kennedy Space Center in Florida, Bernardo Patti, at left, head of International Space Station, Program Department, European Space Agency More

CAPE CANAVERAL, Fla. – At the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, hardware that will be used in the launch of the Ares I-X rocket is being offloaded from the C-5 aircraft. The hardware consists of a precisely machined, full-scale simulator crew module and launch abort system to form the tip of NASA's Ares I-X rocket. The launch of the 321-foot-tall, full-scale Ares I-X, targeted for July 2009, will be the first in a series of unpiloted rocket launches from Kennedy. When fully developed, the 16-foot diameter crew module will furnish living space and reentry protection for the astronauts, while their launch abort system will provide safe evacuation if a launch vehicle failure occurs. Photo credit: NASA/Jack Pfaller KSC-2009-1406

CAPE CANAVERAL, Fla. – At the Shuttle Landing Facility at NASA's Kennedy Space Center in Florida, hardware that will be used in the launch of the Ares I-X rocket is being offloaded from the C-5 aircraft. The ha More

Photograph of Measuring Diameter of a Tree Tallied at the Forest Inventory Sample Point

Original caption: Measuring diameter of tree tallied at the forest inventory sample point. Horace La Bumbard, Watersmeet R.D. Historic Photographs

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. Construction of the S-IC test stand came to a halt at the end of September as the determination was made that the Saturn booster size had to be increased. As a result, the stand had to be modified. With construction delayed, and pumps turned off, this photo, taken December 11, 1961, shows the abandoned site with floods above the 18 ft mark. The flooding was caused by the disturbance of a natural spring months prior during the excavation of the site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the S-IC test stand, related facilities were built during this time. Built to the north of the massive S-IC test stand, was the F-1 Engine test stand. The F-1 test stand, a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, was designed to assist in the development of the F-1 Engine. Capability was provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This photo, taken October 26, 1962, depicts the excavation process of the single engine F-1 stand. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the S-IC test stand, related facilities were built during this time. Built to the north of the massive S-IC test stand, was the F-1 Engine test stand. The F-1 test stand, a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, was designed to assist in the development of the F-1 Engine. Capability was provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This photo, taken November 15, 1962, depicts the excavation process of the single engine F-1 stand site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th More

Saturn I - Saturn Apollo Program

The Saturn I (SA-3) flight lifted off from Kennedy Space Center launch Complex 34, November 16, 1962. The third launch of Saturn launch vehicles, developed at the Marshall Space Flight Center (MSFC) under the d More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the stand itself, related facilities were constructed during this time. Built directly east of the test stand was the Block House, which served as the control center for the test stand. The two were connected by a narrow access tunnel which housed the cables for the controls. The F-1 Engine test stand was built north of the massive S-IC test stand. The F-1 test stand is a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, and was designed to assist in the development of the F-1 Engine. Capability is provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This aerial photograph, taken January 15, 1963 gives an overall view of the construction progress of the newly developed test complex. The large white building located in the center is the Block House. Just below and to the right of it is the S-IC test stand. The large hole to the left of the S-IC stand is the F-1 test stand site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th More

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, the existing stands were remodeled and a sizable new test area was developed. The new comprehensive test complex for propulsion and structural dynamics was unique within the nation and the free world, and they remain so today because they were constructed with foresight to meet the future as well as on going needs. Construction of the S-IC Static test stand complex began in 1961 in the west test area of MSFC, and was completed in 1964. The S-IC static test stand was designed to develop and test the 138-ft long and 33-ft diameter Saturn V S-IC first stage, or booster stage, weighing in at 280,000 pounds. Required to hold down the brute force of a 7,500,000-pound thrust produced by 5 F-1 engines, the S-IC static test stand was designed and constructed with the strength of hundreds of tons of steel and 12,000,000 pounds of cement, planted down to bedrock 40 feet below ground level. The foundation walls, constructed with concrete and steel, are 4 feet thick. The base structure consists of four towers with 40-foot-thick walls extending upward 144 feet above ground level. The structure was topped by a crane with a 135-foot boom. With the boom in the upright position, the stand was given an overall height of 405 feet, placing it among the highest structures in Alabama at the time. In addition to the stand itself, related facilities were constructed during this time. Built directly east of the test stand was the Block House, which served as the control center for the test stand. The two were connected by a narrow access tunnel which housed the cables for the controls. The F-1 Engine test stand was built north of the massive S-IC test stand. The F-1 test stand is a vertical engine firing test stand, 239 feet in elevation and 4,600 square feet in area at the base, and was designed to assist in the development of the F-1 Engine. Capability is provided for static firing of 1.5 million pounds of thrust using liquid oxygen and kerosene. Like the S-IC stand, the foundation of the F-1 stand is keyed into the bedrock approximately 40 feet below grade. This aerial photograph, taken January 15, 1963, gives a close overall view of the newly developed test complex. Depicted in the forefront center is the S-IC test stand with towers prominent, the Block House is seen in the center just above the S-IC test stand, and the large hole to the left, located midway between the two is the F-1 test stand site. n/a

At its founding, the Marshall Space Flight Center (MSFC) inherited the Army’s Jupiter and Redstone test stands, but much larger facilities were needed for the giant stages of the Saturn V. From 1960 to 1964, th More

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles, developed at the Marshall Space Flight Center (MSFC) under the direction of Dr. Wernher von Braun, incorporated a Saturn I, Block I engine. The typical height of a Block I vehicle was approximately 163 feet and had only one live stage. It consisted of eight tanks, each 70 inches in diameter, clustered around a central tank, 105 inches in diameter. Four of the external tanks were fuel tanks for the RP-1 (kerosene) fuel. The other four, spaced alternately with the fuel tanks, were liquid oxygen tanks as was the large center tank. All fuel tanks and liquid oxygen tanks drained at the same rates respectively. The thrust for the stage came from eight H-1 engines, each producing a thrust of 165,000 pounds, for a total thrust of over 1,300,000 pounds. The engines were arranged in a double pattern. Four engines, located inboard, were fixed in a square pattern around the stage axis and canted outward slightly, while the remaining four engines were located outboard in a larger square pattern offset 40 degrees from the inner pattern. Unlike the inner engines, each outer engine was gimbaled. That is, each could be swung through an arc. They were gimbaled as a means of steering the rocket, by letting the instrumentation of the rocket correct any deviations of its powered trajectory. The block I required engine gimabling as the only method of guiding and stabilizing the rocket through the lower atmosphere. The upper stages of the Block I rocket reflected the three-stage configuration of the Saturn I vehicle. Like SA-3, the SA-4 flight’s upper stage ejected 113,560 liters (30,000 gallons) of ballast water in the upper atmosphere for "Project Highwater" physics experiment. Release of this vast quantity of water in a near-space environment marked the second purely scientific large-scale experiment. The SA-4 was the last Block I rocket launch. n/a

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles, developed at the Marshall Space Flight Center (MSFC) under the dir More

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles developed at the Marshall Space Flight Center (MSFC), under the direction of Dr. Wernher von Braun, incorporated a Saturn I, Block I engine. The typical height of a Block I vehicle was approximately 163 feet and had only one live stage. It consisted of eight tanks, each 70 inches in diameter, clustered around a central tank, 105 inches in diameter. Four of the external tanks were fuel tanks for the RP-1 (kerosene) fuel. The other four, spaced alternately with the fuel tanks, were liquid oxygen tanks as was the large center tank. All fuel tanks and liquid oxygen tanks drained at the same rates respectively. The thrust for the stage came from eight H-1 engines, each producing a thrust of 165,000 pounds, for a total thrust of over 1,300,000 pounds. The engines were arranged in a double pattern. Four engines, located inboard, were fixed in a square pattern around the stage axis and canted outward slightly, while the remaining four engines were located outboard in a larger square pattern offset 40 degrees from the inner pattern. Unlike the inner engines, each outer engine was gimbaled. That is, each could be swung through an arc. They were gimbaled as a means of steering the rocket, by letting the instrumentation of the rocket correct any deviations of its powered trajectory. The block I required engine gimabling as the only method of guiding and stabilizing the rocket through the lower atmosphere. The upper stages of the Block I rocket reflected the three-stage configuration of the Saturn I vehicle. Like SA-3, the SA-4 flight’s upper stage ejected 113,560 liters (30,000 gallons) of ballast water in the upper atmosphere for "Project Highwater" physics experiment. Release of this vast quantity of water in a near-space environment marked the second purely scientific large-scale experiment. The SA-4 was the last Block I rocket launch. n/a

The Saturn I (SA-4) flight lifted off from Kennedy Space Center launch Complex 34, March 28, 1963. The fourth launch of Saturn launch vehicles developed at the Marshall Space Flight Center (MSFC), under the dir More

Dome Added to the Space Power Chambers for the Centaur Rocket

This 22.5-foot-diameter domed lid was added to the Space Power Chambers to allow the vertical installation of a Centaur second-stage rocket into the vacuum tank at the National Aeronautics and Space Administrat More

8/65. Valdez - Water storage tank - 690,000 gal. capacity insulated by cellular glass 50 feet in diameter - elevation 190 feet

Valdez Public domain photograph of a storage tank, free to use, no copyright restrictions image - Picryl description

13-Foot Diameter Hydrogen Tank Tested in the K-Site Test Chamber

A 13-foot diameter mounted inside the large test chamber at the Cryogenic Propellant Tank, or K-Site, at National Aeronautics and Space Administration’s (NASA) Plum Brook Station. The 25-foot test chamber and 2 More

Clean Room in the Zero Gravity Research Facility

A technician prepares a test sample in the Zero Gravity Research Facility clean room at the National Aeronautics and Space Administration (NASA) Lewis Research Center. The Zero Gravity Research Facility contain More

Near vertical view of lunar farside taken from Apollo 8 spacecraft

AS8-17-2704 (21-27 Dec. 1968) --- Near vertical view of the lunar farside as photographed from the Apollo 8 spacecraft. This crater, which is about 22 statute miles in diameter, is located at 167 degrees east l More

Rectangular Drop Vehicle in the Zero Gravity Research Facility

A rectangular drop test vehicle perched above 450-foot shaft at the Zero Gravity Research Facility at NASA Lewis Research Center. The drop tower was designed to provide five seconds of microgravity during a nor More

Oblique view of crater Theophilus at northwest edge of Sea of Nectar

AS11-42-6237 (20 July 1969) --- An Apollo 11 oblique view of the large crater Theophilus located at the northwest edge of the Sea of Nectar on the lunar nearside. Theophilus is about 60 statute miles in diamete More

Construction of Cooler for New Propulsion Systems Laboratory Test Cells

The 50-foot diameter primary cooler for the new Propulsion Systems Laboratory No. 3 and 4 facility constructed at the National Aeronautics and Space Administration (NASA) Lewis Research Center. In 1968, 20 year More

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility bay 3 at NASA's Kennedy Space Center in Florida, space shuttle main engine No. 1 is installed in space shuttle Discovery. Each engine is 14 feet long, weighs about 6,700 pounds, and is 7.5 feet in diameter at the end of the nozzle. Discovery is being processed for its next mission, STS-119, targeted for launch on Feb. 12, 2009. Discovery and its crew will deliver integrated truss structure 6 (S6) and solar arrays to the International Space Station. Photo credit: NASA/Dimitri Gerondidakis KSC-08pd2949

CAPE CANAVERAL, Fla. - In Orbiter Processing Facility bay 3 at NASA's Kennedy Space Center in Florida, space shuttle main engine No. 1 is installed in space shuttle Discovery. Each engine is 14 feet long, weig More

Mariner 9 views Olympus Mons standing above the Martian Dust Storm

(November 27, 1971) In pictures taken early in the Mariner 9 mission, this region, shows a dark mountain standing above the Martian dust storm. This higher resolution photograph shows that the area contains a c More

AS15-84-11324 - Apollo 15 - Apollo 15 Mission image - View of Station 6 and North Complex

The original database describes this as: Description: On the far side of Hadley Delta at station 6A, Astronaut David R. Scott, mission commander, took a series of photographs with the 500mm telephoto lens. The More

View of Hadley-Apennine area, looking north, photographed by Apollo 15

S71-44667 (31 July-2 Aug. 1971) --- An oblique view of the Hadley-Apennine area, looking north, as photographed by the Fairchild metric camera in the Scientific Instrumentation Module (SIM) bay of the Apollo 15 More

Space shuttle Space Station. NASA public domain image colelction.

This is an artist's concept of a modular space station. In 1970 the Marshall Space Flight Center arnounced the completion of a study concerning a modular space station that could be launched by the planned-for More

Rigid Tilt Rotor Research: Boeing 26-ft. diameter proprotor on semi-span wing in Ames Research Center 40x80ft w.t. (Photo by Ames photographer Lee Jones; composite of test results by Ames Graphics) ARC-1972-AC72-5255

Rigid Tilt Rotor Research: Boeing 26-ft. diameter proprotor on semi-span wing in Ames Research Center 40x80ft w.t. (Photo by Ames photographer Lee Jones; composite of test results by Ames Graphics)

6 FOOT DIAMETER SOLAR COLLECTOR

The original finding aid described this as: Capture Date: 12/7/1973 Photographer: MARTIN BROWN Keywords: 1973_04247.jpg c1973_04200s Larsen Scan Geographic Location: Cleveland, Ohio Photographs Relating to More

Applications Technology Satellite Test, NASA history, Goddard space flight center

A test model of the Applications Technology Satellite (ATS) is seen during checkout activity in Chamber A of the Space Environment Simulation Laboratory at the Johnson Space Center (JSC) to see if the satellite More

6 FOOT DIAMETER SOLAR COLLECTOR

The original finding aid described this as: Capture Date: 12/7/1973 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

DAMAGED INNER DIAMETER ID LINER ON JP-2 COMBUSTOR

The original finding aid described this as: Capture Date: 10/15/1974 Photographer: STEVE LOOMIS Keywords: Larsen Scan Location Building No: 38 Photographs Relating to Agency Activities, Facilities and Personnel

DAMAGED JP-2 COMBUSTOR INNER DIAMETER ID LINER

The original finding aid described this as: Capture Date: 10/30/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

4 19 INCH DIAMETER COPPER DISKS SHOWING MACRO ETCHED SURFACE

The original finding aid described this as: Capture Date: 9/18/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

18 FOOT DIAMETER WORK PLATFORM IN THE 8X6 FOOT WIND TUNNEL FACILITY

The original finding aid described this as: Capture Date: 10/22/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

4 19 INCH DIAMETER COPPER DISKS SHOWING MACRO ETCHED SURFACE

The original finding aid described this as: Capture Date: 9/18/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

JT-8D 20 INCH DIAMETER ROTOR AND BYPASS STATORS

The original finding aid described this as: Capture Date: 2/6/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 23 Location Room: W-8 Photographs Relating to Agency Activities, More

18 FOOT DIAMETER WORK PLATFORM IN THE 8X6 FOOT WIND TUNNEL FACILITY

The original finding aid described this as: Capture Date: 10/22/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

DAMAGED JP-2 COMBUSTOR INNER DIAMETER ID LINER

The original finding aid described this as: Capture Date: 10/30/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

DAMAGED INNER DIAMETER ID COMBUSTOR LINER

The original finding aid described this as: Capture Date: 1/31/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

20 INCH OUTER DIAMETER OD BY 1.5 INCH THICK COPPER FORGINGS

The original finding aid described this as: Capture Date: 5/15/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

DAMAGED AREA ON INNER DIAMETER ID COMBUSTOR LINER

The original finding aid described this as: Capture Date: 9/4/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

18 FOOT DIAMETER WORK PLATFORM IN THE 8X6 FOOT WIND TUNNEL FACILITY

The original finding aid described this as: Capture Date: 10/22/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

6 FOOT DIAMETER SOLAR COLLECTOR

The original finding aid described this as: Capture Date: 5/2/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

6 FOOT DIAMETER SOLAR COLLECTOR

The original finding aid described this as: Capture Date: 5/2/1974 Photographer: MARTIN BROWN Keywords: c1974_01500s 1974_01578.jpg Larsen Scan Geographic Location: Cleveland, Ohio Photographs Relating to A More

16 FOOT DIAMETER ANTENNA FOR COMMUNICATION TECHNOLOGY SATELLITE CTS SPACECRAFT IN THE 8X6 FOOT WIND TUNNEL

The original finding aid described this as: Capture Date: 8/6/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

4 19 INCH DIAMETER COPPER DISKS SHOWING MACRO ETCHED SURFACE

The original finding aid described this as: Capture Date: 9/18/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

6 FOOT DIAMETER SOLAR COLLECTOR

The original finding aid described this as: Capture Date: 5/2/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

JT-8D 20 INCH DIAMETER ROTOR AND BYPASS STATORS

The original finding aid described this as: Capture Date: 2/6/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 23 Location Room: W-8 Photographs Relating to Agency Activities, More

6 FOOT DIAMETER SOLAR COLLECTOR

The original finding aid described this as: Capture Date: 5/2/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

16 FOOT DIAMETER ANTENNA FOR COMMUNICATION TECHNOLOGY SATELLITE CTS SPACECRAFT IN THE 8X6 FOOT WIND TUNNEL

The original finding aid described this as: Capture Date: 8/6/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

4 19 INCH DIAMETER COPPER DISKS SHOWING MACRO ETCHED SURFACE

The original finding aid described this as: Capture Date: 9/18/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

16 FOOT DIAMETER ANTENNA FOR COMMUNICATION TECHNOLOGY SATELLITE CTS SPACECRAFT IN THE 8X6 FOOT WIND TUNNEL

The original finding aid described this as: Capture Date: 8/6/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

JT-8D 20 INCH DIAMETER ROTOR AND BYPASS STATORS

The original finding aid described this as: Capture Date: 2/6/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 23 Location Room: W-8 Photographs Relating to Agency Activities, More

DAMAGED AREA ON INNER DIAMETER ID COMBUSTOR LINER

The original finding aid described this as: Capture Date: 9/4/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

OPENING OF THE JET TEST NOZZLE - 2 INCH DIAMETER

The original finding aid described this as: Capture Date: 2/25/1975 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

ISS031-E-143143 (19 June 2012) --- Al Jubayl, Saudi Arabia at night is featured in this image photographed by an Expedition 31 crew member on the International Space Station. The city of Al Jubayl (or Jubail) is located on the Saudi Arabian coastline of the Persian Gulf. The city has a history extending back more than 7,000 years, but since 1975 it has been associated with the heavy industries of petrochemical refining and production, fertilizer production and steel works. At night, these industrial areas form a brightly lit region (center) to the south of the residential and commercial center of Al Jubayl (characterized by green-gray lighting). An artificial peninsula extending into the Persian Gulf to the northeast hosts supertanker docks and petroleum storage facilities. The Persian Gulf to the north and northeast is devoid of lights; likewise, the open desert to the south-southeast provides a stark contrast to the well-lit urban and industrial areas. A bright circle of light located within the heavy industrial area (center) cannot be resolved in this photograph, but is likely a concentration of lights associated with ongoing processing or construction activities. The approximate scale of the feature ? hundreds of meters in diameter ? is consistent with multiple stationary light sources, particularly if the light from those sources is accentuated due to the camera?s low light settings. iss031e143143

ISS031-E-143143 (19 June 2012) --- Al Jubayl, Saudi Arabia at night is featured in this image photographed by an Expedition 31 crew member on the International Space Station. The city of Al Jubayl (or Jubail) i More

5 INCH DIAMETER TEFLON SPUTTERING TARGET

The original finding aid described this as: Capture Date: 5/29/1975 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

25 INCH DIAMETER SPLENICAL TANK

The original finding aid described this as: Capture Date: 2/13/1975 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

JET TEST NOZZLE - 2 INCH DIAMETER

The original finding aid described this as: Capture Date: 2/20/1975 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 23 Location Room: W-2 Photographs Relating to Agency Activities, F More

25 INCH DIAMETER SPLENICAL TANK

The original finding aid described this as: Capture Date: 2/13/1975 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

42 INCH DIAMETER ZERO GRAVITY VEHICLE - CODE NAME C - SHOWING DAMAGE

The original finding aid described this as: Capture Date: 3/4/1976 Photographer: J DAVID CLINTON Keywords: Larsen Scan Location Building No: 110 Photographs Relating to Agency Activities, Facilities and Personnel

42 INCH DIAMETER ZERO GRAVITY VEHICLE - CODE NAME C - SHOWING DAMAGE

The original finding aid described this as: Capture Date: 3/4/1976 Photographer: J DAVID CLINTON Keywords: Larsen Scan Location Building No: 110 Photographs Relating to Agency Activities, Facilities and Personnel