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Ceremonial Skirt - needlework visual works

Ceremonial Skirt - needlework visual works

Picryl description: Public domain image of a 19th-century fashion, Asian costume design, free to use, no copyright restrictions.

map from "The Story of Atlantis. A geographical, historical, and ethnological sketch. Illustrated by four maps of the world's configuration at different periods ... With a preface by A. P. Sinnett"

map from "The Story of Atlantis. A geographical, historical, and ethno...

This image has been taken from scan 000089 from "The Story of Atlantis. A geographical, historical, and ethnological sketch. Illustrated by four maps of the world's configuration at different periods ... With a... More

world from "The Story of Atlantis. A geographical, historical, and ethnological sketch. Illustrated by four maps of the world's configuration at different periods ... With a preface by A. P. Sinnett"

world from "The Story of Atlantis. A geographical, historical, and eth...

This image has been taken from scan 000091 from "The Story of Atlantis. A geographical, historical, and ethnological sketch. Illustrated by four maps of the world's configuration at different periods ... With a... More

Mercury Project, NASA history collection

Mercury Project, NASA history collection

A Mercury-Redstone launch vehicle awaits test-firing in the Redstone Test Stand during the late 1950s. Between 1953 and 1960, the rocket team at Redstone Arsenal in Huntsville, Alabama performed hundreds of tes... More

Under the goals of the Vision for Space Exploration, Ares I is a chief component of the cost-effective space transportation infrastructure being developed by NASA's Constellation Program. This transportation system will safely and reliably carry human explorers back to the moon, and then onward to Mars and other destinations in the solar system. The Ares I effort includes multiple project element teams at NASA centers and contract organizations around the nation, and is managed by the Exploration Launch Projects Office at NASA's Marshall Space Flight Center (MFSC). ATK Launch Systems near Brigham City, Utah, is the prime contractor for the first stage booster. ATK's subcontractor, United Space Alliance of Houston, is designing, developing and testing the parachutes at its facilities at NASA's Kennedy Space Center in Florida. NASA's Johnson Space Center in Houston hosts the Constellation Program and Orion Crew Capsule Project Office and provides test instrumentation and support personnel. Together, these teams are developing vehicle hardware, evolving proven technologies, and testing components and systems. Their work builds on powerful, reliable space shuttle propulsion elements and nearly a half-century of NASA space flight experience and technological advances. Ares I is an inline, two-stage rocket configuration topped by the Crew Exploration Vehicle, its service module, and a launch abort system. This HD video image depicts friction stir welding used in manufacturing aluminum panels that will fabricate the Ares I upper stage barrel. The aluminum panels are subjected to confidence panel tests during which the bent aluminum is stressed to breaking point and thoroughly examined. The panels are manufactured by AMRO Manufacturing located in El Monte, California. (Highest resolution available) n/a

Under the goals of the Vision for Space Exploration, Ares I is a chief...

Under the goals of the Vision for Space Exploration, Ares I is a chief component of the cost-effective space transportation infrastructure being developed by NASA's Constellation Program. This transportation sy... More

CAPE CANAVERAL, Fla. -- At NASA's Kennedy Space Center in Florida, this overhead image shows the Space Shuttle Program's last external fuel tank, ET-122, after it was delivered to the transfer aisle of the Vehicle Assembly Building (VAB). The tank traveled 900 miles by sea, carried in the Pegasus Barge, from NASA's Michoud Assembly Facility in New Orleans. Once inside the VAB, it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station targeted to launch Feb. 2011. STS-134 currently is scheduled to be the last mission in the shuttle program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Kevin O'Connell KSC-2010-4912

CAPE CANAVERAL, Fla. -- At NASA's Kennedy Space Center in Florida, thi...

CAPE CANAVERAL, Fla. -- At NASA's Kennedy Space Center in Florida, this overhead image shows the Space Shuttle Program's last external fuel tank, ET-122, after it was delivered to the transfer aisle of the Vehi... More

CAPE CANAVERAL, Fla. -- A tugboat pulls the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122, toward NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea from NASA's Michoud Assembly Facility in New Orleans. After reaching the Turn Basin at Kennedy, the tank will be offloaded and moved to the Vehicle Assembly Building where it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station. STS-134, targeted to launch in Feb. 2011, currently is scheduled to be the last mission in the Space Shuttle Program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Jim Grossmann KSC-2010-4867

CAPE CANAVERAL, Fla. -- A tugboat pulls the Pegasus Barge carrying the...

CAPE CANAVERAL, Fla. -- A tugboat pulls the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122, toward NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea ... More

KENNEDY SPACE CENTER, FLA. - After rollback of the rotating service structure (RSS) on Launch Pad 39B, Space Shuttle Discovery stands bathed in lights from the RSS and fixed service structure. The rollback was in preparation for launch July 1 on mission STS-121. Extending toward the cockpit of the shuttle is the orbiter access arm with the White Room extended. The White Room provides access into the orbiter for the astronauts. The RSS provides protected access to the orbiter for changeout and servicing of payloads at the pad. The structure is supported by a rotating bridge that pivots about a vertical axis on the west side of the pad's flame trench. The hinge column rests on the pad surface and is braced to the fixed service structure. Support for the outer end of the bridge is provided by two eight-wheel, motor-driven trucks that move along circular twin rails installed flush with the pad surface. The track crosses the flame trench on a permanent bridge. The RSS is 102 feet long, 50 feet wide and 130 feet high. The structure has orbiter access platforms at five levels to provide access to the payload bay while the orbiter is being serviced in the RSS. Each platform has independent extendable planks that can be arranged to conform to a payload's configuration. This mission is the 115th shuttle flight and the 18th U.S. flight to the International Space Station. Photo credit: NASA/Kim Shiflett KSC-06pd1308

KENNEDY SPACE CENTER, FLA. - After rollback of the rotating service ...

KENNEDY SPACE CENTER, FLA. - After rollback of the rotating service structure (RSS) on Launch Pad 39B, Space Shuttle Discovery stands bathed in lights from the RSS and fixed service structure. The rollback w... More

JOHNSON SPACE CENTER, HOUSTON -- STS123-S-001-- STS-123 continues assembly of the International Space Station (ISS). The primary mission objectives include rotating an expedition crew member and installing both the first component of the Japanese Experimental Module (the Experimental Logistics Module - Pressurized Section [ELM-PS]) and the Canadian Special Purpose Dexterous Manipulator (SPDM). In addition, STS-123 will deliver various spare ISS components and leave behind the sensor boom used for inspecting the shuttle's thermal protection system. A follow-on mission to ISS will utilize and then return home with this sensor boom. A total of four spacewalks are planned to accomplish these tasks. The mission will also require the use of both the shuttle and ISS robotic arms. STS-123 will utilize the Station-Shuttle Power Transfer System to extend the docked portion of the mission to 11 days, with a total planned duration of 15 days. The crew patch depicts the space shuttle in orbit with the crew names trailing behind. STS-123's major additions to ISS (the ELM-PS installation with the shuttle robotic arm and the fully constructed SPDM) are both illustrated. The ISS is shown in the configuration that the STS-123 crew will encounter when they arrive. The NASA insignia design for shuttle flights is reserved for use by the astronauts and for other official use as the NASA Administrator may authorize. Public availability has been approved only in the form of illustrations by the various news media. When and if there is any change in this policy, which is not anticipated, it will be publicly announced. KSC-08pd0363

JOHNSON SPACE CENTER, HOUSTON -- STS123-S-001-- STS-123 continues asse...

JOHNSON SPACE CENTER, HOUSTON -- STS123-S-001-- STS-123 continues assembly of the International Space Station (ISS). The primary mission objectives include rotating an expedition crew member and installing bot... More

CAPE CANAVERAL, Fla. -- Workers unload a container holding the cruise stage, one of the first three elements for NASA's Mars Science Laboratory (MSL) that arrived at NASA Kennedy Space Center's Shuttle Landing Facility aboard an Air Force C-17 cargo plane. The cruise stage, back shell and heat shield, the first flight elements to arrive for the MSL mission, were taken to the Payload Hazardous Servicing Facility (PHSF) located in the KSC Industrial Area to begin processing. The Curiosity rover will arrive next month. A United Launch Alliance Atlas V-541 configuration will be used to loft MSL into space. Curiosity’s 10 science instruments are designed to search for evidence on whether Mars has had environments favorable to microbial life, including chemical ingredients for life. The unique rover will use a laser to look inside rocks and release its gasses so that the rover’s spectrometer can analyze and send the data back to Earth. MSL is scheduled to launch from Cape Canaveral Air Force Station in Florida Nov. 25 with a window extending to Dec. 18 and arrival at Mars Aug. 2012. For more information, visit http://www.nasa.gov/msl. Photo credit: NASA/Troy Cryder KSC-2011-3510

CAPE CANAVERAL, Fla. -- Workers unload a container holding the cruise ...

CAPE CANAVERAL, Fla. -- Workers unload a container holding the cruise stage, one of the first three elements for NASA's Mars Science Laboratory (MSL) that arrived at NASA Kennedy Space Center's Shuttle Landing ... More

KENNEDY SPACE CENTER, FLA. - After rollback of the rotating service structure (RSS) on Launch Pad 39B, Space Shuttle Discovery stands bathed in lights from the RSS and fixed service structure. The rollback was in preparation for launch July 1 on mission STS-121. Extending toward the cockpit of the shuttle is the orbiter access arm with the White Room extended. The White Room provides access into the orbiter for the astronauts. The RSS provides protected access to the orbiter for changeout and servicing of payloads at the pad. The structure is supported by a rotating bridge that pivots about a vertical axis on the west side of the pad's flame trench. The hinge column rests on the pad surface and is braced to the fixed service structure. Support for the outer end of the bridge is provided by two eight-wheel, motor-driven trucks that move along circular twin rails installed flush with the pad surface. The track crosses the flame trench on a permanent bridge. The RSS is 102 feet long, 50 feet wide and 130 feet high. The structure has orbiter access platforms at five levels to provide access to the payload bay while the orbiter is being serviced in the RSS. Each platform has independent extendable planks that can be arranged to conform to a payload's configuration. This mission is the 115th shuttle flight and the 18th U.S. flight to the International Space Station. Photo credit: NASA/Kim Shiflett KSC-06pd1307

KENNEDY SPACE CENTER, FLA. - After rollback of the rotating service ...

KENNEDY SPACE CENTER, FLA. - After rollback of the rotating service structure (RSS) on Launch Pad 39B, Space Shuttle Discovery stands bathed in lights from the RSS and fixed service structure. The rollback w... More

KENNEDY SPACE CENTER, FLA. -- Cameras are prepared to record the launch of Space Shuttle Atlantis from Launch Pad 39A following sunrise on a cloudy Florida day. Rollback of the pad's rotating service structure, or RSS, is one of the milestones in preparation for the launch of mission STS-117 on June 8. Rollback started at 10:56 p.m. EDT June 7 and was complete at 11:34 p.m. The RSS, the massive structure to the left of the shuttle, provides protected access to the orbiter for changeout and servicing of payloads at the pad. The structure is supported by a rotating bridge that pivots about a vertical axis on the side of the pad's flame trench. The hinge column rests on the pad surface and is braced to the fixed service structure. Support for the outer end of the bridge is provided by two eight-wheel, motor-driven trucks that move along circular twin rails installed flush with the pad surface. The track crosses the flame trench on a permanent bridge. The RSS is 102 feet long, 50 feet wide and 130 feet high. The structure has orbiter access platforms at five levels to provide access to the payload bay while the orbiter is being serviced in the RSS. Each platform has independent extendable planks that can be arranged to conform to a payload's configuration. This mission is the 118th shuttle flight and the 21st U.S. flight to the International Space Station and will deliver and install the S3/S4 truss segment, deploy a set of solar arrays and prepare them for operation. Photo credit: NASA/Ken Thornsley KSC-07pd1399

KENNEDY SPACE CENTER, FLA. -- Cameras are prepared to record the launc...

KENNEDY SPACE CENTER, FLA. -- Cameras are prepared to record the launch of Space Shuttle Atlantis from Launch Pad 39A following sunrise on a cloudy Florida day. Rollback of the pad's rotating service structure,... More

CAPE CANAVERAL, Fla. -- This sunrise view from the stern of Freedom Star, one of NASA's solid rocket booster retrieval ships, shows the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122. The tank will travel 900 miles by sea to NASA's Kennedy Space Center in Florida before being offloaded and moved to Kennedy's Vehicle Assembly Building. There it will be integrated to space shuttle Endeavour for the STS-134 mission to the International Space Station. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. STS-134, targeted to launch Feb. 2011, currently is scheduled to be the last mission in the Space Shuttle Program. Photo credit: NASA/Kim Shiflett KSC-2010-4819

CAPE CANAVERAL, Fla. -- This sunrise view from the stern of Freedom St...

CAPE CANAVERAL, Fla. -- This sunrise view from the stern of Freedom Star, one of NASA's solid rocket booster retrieval ships, shows the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank... More

CAPE CANAVERAL, Fla. -- This panoramic image shows tug boats maneuvering the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122, through the Turn Basin at NASA's Kennedy Space Center in Florida. Once docked, the tank will be offloaded from the barge and transported to the Vehicle Assembly Building (VAB). NASA's Liberty Star solid rocket booster retrieval ship is also seen (left) docked at the Turn Basin. The tank traveled 900 miles by sea, carried in the barge, from NASA's Michoud Assembly Facility in New Orleans. Once inside the VAB, it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station targeted to launch Feb. 2011. STS-134 currently is scheduled to be the last mission in the shuttle program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Frankie Martin KSC-2010-4903

CAPE CANAVERAL, Fla. -- This panoramic image shows tug boats maneuveri...

CAPE CANAVERAL, Fla. -- This panoramic image shows tug boats maneuvering the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122, through the Turn Basin at NASA's Kennedy Space Ce... More

KENNEDY SPACE CENTER, FLA. -- In the Vehicle Assembly Building at NASA's Kennedy Space Center, United Space Alliance technicians get ready to lower the external tank to be mated with the solid rocket boosters on the mobile launcher platform. The boosters-tank configuration will be used on space shuttle Atlantis for mission STS-122, which is targeted for launch on Dec. 6. Photo credit: Kim Shiflett KSC-07pd2872

KENNEDY SPACE CENTER, FLA. -- In the Vehicle Assembly Building at NASA...

KENNEDY SPACE CENTER, FLA. -- In the Vehicle Assembly Building at NASA's Kennedy Space Center, United Space Alliance technicians get ready to lower the external tank to be mated with the solid rocket boosters o... More

CAPE CANAVERAL, Fla. -- A United Space Alliance technician monitors the Space Shuttle Program's last external fuel tank, ET-122, as it moves from the Turn Basin to the Vehicle Assembly Building at NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea from NASA's Michoud Assembly Facility in New Orleans aboard the Pegasus Barge. Once inside the Vehicle Assembly Building, it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station. STS-134, targeted to launch in Feb. 2011, currently is scheduled to be the last mission in the shuttle program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Jack Pfaller KSC-2010-4893

CAPE CANAVERAL, Fla. -- A United Space Alliance technician monitors th...

CAPE CANAVERAL, Fla. -- A United Space Alliance technician monitors the Space Shuttle Program's last external fuel tank, ET-122, as it moves from the Turn Basin to the Vehicle Assembly Building at NASA's Kenned... More

CAPE CANAVERAL, Fla. -- This overhead view shows the Space Shuttle Program's last external fuel tank, ET-122 (right), as it is being transported to the Vehicle Assembly Building (VAB) at NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea, carried in the Pegasus Barge, from NASA's Michoud Assembly Facility in New Orleans. Once inside the VAB, it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station targeted to launch Feb. 2011. STS-134 currently is scheduled to be the last mission in the shuttle program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Kevin O'Connell KSC-2010-4907

CAPE CANAVERAL, Fla. -- This overhead view shows the Space Shuttle Pro...

CAPE CANAVERAL, Fla. -- This overhead view shows the Space Shuttle Program's last external fuel tank, ET-122 (right), as it is being transported to the Vehicle Assembly Building (VAB) at NASA's Kennedy Space Ce... More

CAPE CANAVERAL, Fla. -- This panoramic image shows the Launch Complex 39 area at NASA's Kennedy Space Center in Florida. In the far background is the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122, into Kennedy's Turn Basin. Once docked, the tank will be offloaded from the barge and transported to the Vehicle Assembly Building (VAB). NASA's Liberty Star solid rocket booster retrieval ship also is docked at the Turn Basin. The tank traveled 900 miles by sea, carried in the barge, from NASA's Michoud Assembly Facility in New Orleans. Once inside the VAB, it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station targeted to launch Feb. 2011. STS-134 currently is scheduled to be the last mission in the shuttle program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Frankie Martin KSC-2010-4900

CAPE CANAVERAL, Fla. -- This panoramic image shows the Launch Complex ...

CAPE CANAVERAL, Fla. -- This panoramic image shows the Launch Complex 39 area at NASA's Kennedy Space Center in Florida. In the far background is the Pegasus Barge carrying the Space Shuttle Program's last exte... More

KENNEDY SPACE CENTER, FLA. - Leaders from space agencies around the world take a moment from the International Space Station Heads of Agency meeting being held at Kennedy Space Center for a group portrait, framed by the space shuttle launch pads in Launch Complex 39. From left are Canadian Space Agency Vice-President Space Science, Technology and Programs Virendra Jha; Russian Federal Space Agency Head Anatolii Perminov; European Space Agency Director-General Jean-Jacques Dordain; NASA Administrator Michael Griffin; and Japan Aerospace Exploration Agency President Keiji Tachikawa. The purpose of the meeting is to review International Space Station cooperation and endorse a revision to the station configuration and assembly sequence. KSC-06pd0414

KENNEDY SPACE CENTER, FLA. - Leaders from space agencies around the w...

KENNEDY SPACE CENTER, FLA. - Leaders from space agencies around the world take a moment from the International Space Station Heads of Agency meeting being held at Kennedy Space Center for a group portrait, fra... More

NEW ORLEANS -- Workers escort the Space Shuttle Program's last external fuel tank, ET-122, from NASA's Michoud Assembly Facility in New Orleans for transportation to NASA's Kennedy Space Center in Florida. The tank will travel 900 miles by sea secured aboard the Pegasus Barge, offloaded and moved to Kennedy's Vehicle Assembly Building where it will be integrated to space shuttle Endeavour for the STS-134 mission to the International Space Station. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. STS-134, targeted to launch Feb. 2011, currently is scheduled to be the last mission in the Space Shuttle Program. Photo credit: NASA/Kim Shiflett KSC-2010-4792

NEW ORLEANS -- Workers escort the Space Shuttle Program's last externa...

NEW ORLEANS -- Workers escort the Space Shuttle Program's last external fuel tank, ET-122, from NASA's Michoud Assembly Facility in New Orleans for transportation to NASA's Kennedy Space Center in Florida. The ... More

Module Nova concept - Solid C-3 Basis - Early Program Development

Module Nova concept - Solid C-3 Basis - Early Program Development

This artist's concept illustrates the Module Nova concept - Solid C-3 Basis. From 1960 to 1962, the Marshall Space Flight Center considered the Nova launch vehicle as a means to achieve a marned lunar landing w... More

Early Program Development Module Nova concept

Early Program Development Module Nova concept

This artist's concept illustrates the Module Nova concept - Solid C-3 Basis. From 1960 to 1962, the Marshall Space Flight Center considered the Nova launch vehicle as a means to achieve a marned lunar landing w... 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...

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...

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

Supersonic Transport Configuration in Large scale (40x80 foot) Wind Tunnel Investigation at Ames Research Center

Supersonic Transport Configuration in Large scale (40x80 foot) Wind Tu...

3/4 front view (low sweep) Francis Mallerick shown in picture. Don Richey

David Reese and Alvin Seiff interpret the results from tests designed to study spacecraft configuration and performance in a particular atmosphere ARC-1964-A-33672

David Reese and Alvin Seiff interpret the results from tests designed ...

David Reese and Alvin Seiff interpret the results from tests designed to study spacecraft configuration and performance in a particular atmosphere

Saturn V chart - Saturn Apollo Program

Saturn V chart - Saturn Apollo Program

This chart illustrates the testing vehicle and flight vehicle configurations, in addition to the approximate dimensions of the stages of the Saturn V launch vehicle.

Aerodynamic Characteristics of Rotary Entry Vehicle configuration REV-1 model schlieren. Testing being done at the NASA Ames Research Center, California ARC-1966-A-39240

Aerodynamic Characteristics of Rotary Entry Vehicle configuration REV-...

Aerodynamic Characteristics of Rotary Entry Vehicle configuration REV-1 model schlieren. Testing being done at the NASA Ames Research Center, California

Aerodynamic Characteristics of Rotary Entry Vehicle configuration REV-1 model schlieren Testing being done at the NASA Ames Research Center, California ARC-1966-A-39238

Aerodynamic Characteristics of Rotary Entry Vehicle configuration REV-...

Aerodynamic Characteristics of Rotary Entry Vehicle configuration REV-1 model schlieren Testing being done at the NASA Ames Research Center, California

Saturn Apollo Program - Lunar Module (LM) configuration

Saturn Apollo Program - Lunar Module (LM) configuration

This illustration is the Lunar Module (LM) configuration. The LM was a two part spacecraft. Its lower or descent stage had the landing gear, engines, and fuel needed for the landing. When the LM blasted off the... More

Saturn V - in inches and meters by the Boeing Company

Saturn V - in inches and meters by the Boeing Company

The Saturn V configuration is shown in inches and meters as illustrated by the Boeing Company. The Saturn V vehicle consisted of three stages: the S-IC (first) stage powered by five F-1 engines, the S-II (secon... More

Apollo 9 Lunar Module in lunar landing configuration

Apollo 9 Lunar Module in lunar landing configuration

AS09-21-3181 (7 March 1969) --- A View of the Apollo 9 Lunar Module (LM), "Spider," in a lunar lading configuration, as photographed from the Command and Service Modules (CSM) on the fifth day of the Apollo 9 E... More

Apollo 9 Lunar Module in lunar landing configuration

Apollo 9 Lunar Module in lunar landing configuration

AS09-21-3212 (7 March 1969) --- A view of the Apollo 9 Lunar Module (LM), "Spider", in a lunar landing configuration, as photographed from the Command and Service Modules (CSM) on the fifth day of the Apollo 9 ... More

Apollo 9 Lunar Module in lunar landing configuration

Apollo 9 Lunar Module in lunar landing configuration

AS09-21-3199 (7 March 1969) --- Excellent view of the Apollo 9 Lunar Module, "Spider," in a lunar landing configuration, as photographed from the Command and Service Modules on the fifth day of the Apollo 9 Ear... More

Apollo 12 Lunar Module, in landing configuration, photographed in lunar orbit

Apollo 12 Lunar Module, in landing configuration, photographed in luna...

AS12-51-7507 (19 Nov. 1969) --- The Apollo 12 Lunar Module (LM), in a lunar landing configuration, is photographed in lunar orbit from the Command and Service Modules (CSM). The coordinates of the center of the... More

LOUISIANA -- A tug boat pulls the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122, from NASA's Michoud Assembly Facility in New Orleans toward Gulfport, La. The barge will meet up with Freedom Star, NASA's solid rocket booster retrieval ship, which will escort it to NASA's Kennedy Space Center in Florida. The tank will travel 900 miles by sea before being offloaded and moved to Kennedy's Vehicle Assembly Building. There it will be integrated to space shuttle Endeavour for the STS-134 mission to the International Space Station. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. STS-134, targeted to launch Feb. 2011, currently is scheduled to be the last mission in the Space Shuttle Program. Photo credit: NASA/Kim Shiflett KSC-2010-4808

LOUISIANA -- A tug boat pulls the Pegasus Barge carrying the Space Shu...

LOUISIANA -- A tug boat pulls the Pegasus Barge carrying the Space Shuttle Program's last external fuel tank, ET-122, from NASA's Michoud Assembly Facility in New Orleans toward Gulfport, La. The barge will mee... More

CAPE CANAVERAL, Fla. -- A tug boat pulls the Space Shuttle Program's last external fuel tank, ET-122, to the Turn Basin at NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea from NASA's Michoud Assembly Facility in New Orleans aboard the Pegasus Barge. Next, the tank will be offloaded and moved to Kennedy's Vehicle Assembly Building where it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station. STS-134, targeted to launch in Feb. 2011, currently is scheduled to be the last mission in the Space Shuttle Program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Frankie Martin KSC-2010-4841

CAPE CANAVERAL, Fla. -- A tug boat pulls the Space Shuttle Program's l...

CAPE CANAVERAL, Fla. -- A tug boat pulls the Space Shuttle Program's last external fuel tank, ET-122, to the Turn Basin at NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea from NASA's ... More

KENNEDY SPACE CENTER, FLA. -- On a cloudy Florida day, Space Shuttle Atlantis awaits launch atop a mobile launch platform at Launch Pad 39A. At the right of the pad is the 290-foot tall, 300,000-gallon water tank that is part of the sound suppression system during launches. In the foreground is the crawlerway. a 130-foot-wide roadway with a 5-percent grade leading to the top of the launch pad. Rollback of the pad's rotating service structure, or RSS, is one of the milestones in preparation for the launch of mission STS-117 on June 8. Rollback started at 10:56 p.m. EDT June 7 and was complete at 11:34 p.m. The RSS, the massive structure to the left of the shuttle, provides protected access to the orbiter for changeout and servicing of payloads at the pad. The structure is supported by a rotating bridge that pivots about a vertical axis on the side of the pad's flame trench. The hinge column rests on the pad surface and is braced to the fixed service structure. Support for the outer end of the bridge is provided by two eight-wheel, motor-driven trucks that move along circular twin rails installed flush with the pad surface. The track crosses the flame trench on a permanent bridge. The RSS is 102 feet long, 50 feet wide and 130 feet high. The structure has orbiter access platforms at five levels to provide access to the payload bay while the orbiter is being serviced in the RSS. Each platform has independent extendable planks that can be arranged to conform to a payload's configuration. This mission is the 118th shuttle flight and the 21st U.S. flight to the International Space Station and will deliver and install the S3/S4 truss segment, deploy a set of solar arrays and prepare them for operation. Photo credit: NASA/Ken Thornsley KSC-07pd1403

KENNEDY SPACE CENTER, FLA. -- On a cloudy Florida day, Space Shuttle A...

KENNEDY SPACE CENTER, FLA. -- On a cloudy Florida day, Space Shuttle Atlantis awaits launch atop a mobile launch platform at Launch Pad 39A. At the right of the pad is the 290-foot tall, 300,000-gallon water ta... More

KENNEDY SPACE CENTER, FLA. - In preparation for the July 1 launch of Space Shuttle Discovery on mission STS-121, the Launch Pad 39B rotating service structure (RSS) enclosing the shuttle rolls away. Above the golden external tank is the vent hood (known as the "beanie cap") at the end of the gaseous oxygen vent arm. Vapors are created as the liquid oxygen in the external tank boil off. The hood vents the gaseous oxygen vapors away from the space shuttle vehicle. The RSS provides protected access to the orbiter for changeout and servicing of payloads at the pad. The structure is supported by a rotating bridge that pivots about a vertical axis on the west side of the pad's flame trench. The hinge column rests on the pad surface and is braced to the fixed service structure. Support for the outer end of the bridge is provided by two eight-wheel, motor-driven trucks that move along circular twin rails installed flush with the pad surface. The track crosses the flame trench on a permanent bridge. The RSS is 102 feet long, 50 feet wide and 130 feet high. The structure has orbiter access platforms at five levels to provide access to the payload bay while the orbiter is being serviced in the RSS. Each platform has independent extendable planks that can be arranged to conform to a payload's configuration. This mission is the 115th shuttle flight and the 18th U.S. flight to the International Space Station. Photo credit: NASA/Kim Shiflett KSC-06pd1302

KENNEDY SPACE CENTER, FLA. - In preparation for the July 1 launch of ...

KENNEDY SPACE CENTER, FLA. - In preparation for the July 1 launch of Space Shuttle Discovery on mission STS-121, the Launch Pad 39B rotating service structure (RSS) enclosing the shuttle rolls away. Above the... More

CAPE CANAVERAL, Fla. -- A tug boat pulls the Space Shuttle Program's last external fuel tank, ET-122, toward the Turn Basin at NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea from NASA's Michoud Assembly Facility in New Orleans aboard the Pegasus Barge. Next, the tank will be offloaded and moved to Kennedy's Vehicle Assembly Building where it eventually will be attached to space shuttle Endeavour for the STS-134 mission to the International Space Station. STS-134, targeted to launch in Feb. 2011, currently is scheduled to be the last mission in the Space Shuttle Program. The tank, which is the largest element of the space shuttle stack, was damaged during Hurricane Katrina in August 2005 and restored to flight configuration by Lockheed Martin Space Systems Company employees. Photo credit: NASA/Frankie Martin KSC-2010-4835

CAPE CANAVERAL, Fla. -- A tug boat pulls the Space Shuttle Program's l...

CAPE CANAVERAL, Fla. -- A tug boat pulls the Space Shuttle Program's last external fuel tank, ET-122, toward the Turn Basin at NASA's Kennedy Space Center in Florida. The tank traveled 900 miles by sea from NAS... More

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRAIGHT WING CONFIGURATION ARC-1970-A70-04625

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRA...

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRAIGHT WING CONFIGURATION

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRAIGHT WING CONFIGURATION ARC-1970-A70-04623

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRA...

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRAIGHT WING CONFIGURATION

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRAIGHT WING CONFIGURATION ARC-1970-A70-04624

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRAI...

OBLIQUE WING TRANSONIC TRANSPORT MODEL: DR. R. T. JONES' CONCEPT-STRAIGHT WING CONFIGURATION

Lunar Roving Vehicle (LRV) - Saturn Apollo Program

Lunar Roving Vehicle (LRV) - Saturn Apollo Program

This photograph shows a front view of a folded configuration of the Lunar Roving Vehicle (LRV) No. 2. The LRV was built to give Apollo astronauts a greater range of mobility during lunar exploration. It was an ... More

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission simulations and is adaptable to two configurations. Configuration 1: The cab will accommodate a three-man crew for space mission research. The accelerations and rates are intended to be smoothly applicable at very low value so the navigation and guidance procedures using a high-accuracy, out-the window display may be simulated. Configuration 2: The simulator can use a one-man cab for human tolerance studies and performance testing. Atmosphere and tempertaure can be varied as stress inducements. This simlator is operated closed-loop with digital or analog computation. It is currently man-rated for 3.5g maximum. ARC-1971-AC71-6490

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission s...

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission simulations and is adaptable to two configurations. Configuration 1: The cab will accommodate a three-man crew for space mission research. T... More

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission simulations and is adaptable to two configurations. Configuration 1: The cab will accommodate a three-man crew for space mission research. The accelerations and rates are intended to be smoothly applicable at very low value so the navigation and guidance procedures using a high-accuracy, out-the window display may be simulated. Configuration 2: The simulator can use a one-man cab for human tolerance studies and performance testing. Atmosphere and tempertaure can be varied as stress inducements. This simlator is operated closed-loop with digital or analog computation. It is currently man-rated for 3.5g maximum. ARC-1971-AC71-6486

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission s...

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission simulations and is adaptable to two configurations. Configuration 1: The cab will accommodate a three-man crew for space mission research. T... More

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission simulations and is adaptable to two configurations. Configuration 1: The cab will accommodate a three-man crew for space mission research. The accelerations and rates are intended to be smoothly applicable at very low value so the navigation and guidance procedures using a high-accuracy, out-the window display may be simulated. Configuration 2: The simulator can use a one-man cab for human tolerance studies and performance testing. Atmosphere and tempertaure can be varied as stress inducements. This simlator is operated closed-loop with digital or analog computation. It is currently man-rated for 3.5g maximum. ARC-1971-AC71-6488

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission s...

N-243 Flight and Guidance Centrifuge: Is used for spacecraft mission simulations and is adaptable to two configurations. Configuration 1: The cab will accommodate a three-man crew for space mission research. T... More

AS16-113-18347 - Apollo 16 - Apollo 16 Mission image - A partial view of the Apollo 16 Apollo Lunar Surface Experiments Package (ALSEP) in deployed configuration on the lunar surface as photographed during the mission's first extravehicular activity (EVA-1), on April 21, 1972

AS16-113-18347 - Apollo 16 - Apollo 16 Mission image - A partial view ...

The original database describes this as: Description: A partial view of the Apollo 16 Apollo Lunar Surface Experiments Package (ALSEP) in deployed configuration on the lunar surface as photographed during the ... More

MSC 040A Space Shuttle: 11ft. W.T. Test of Acoustic Environment (Configuration #5) ARC-1972-A72-1341

MSC 040A Space Shuttle: 11ft. W.T. Test of Acoustic Environment (Confi...

MSC 040A Space Shuttle: 11ft. W.T. Test of Acoustic Environment (Configuration #5)

MSC 040A Space Shuttle: 11ft. W.T. Tests pf Acoustic Environment (Configuration 5 with James M. Peterson ARC-1972-AC72-1344

MSC 040A Space Shuttle: 11ft. W.T. Tests pf Acoustic Environment (Conf...

MSC 040A Space Shuttle: 11ft. W.T. Tests pf Acoustic Environment (Configuration 5 with James M. Peterson

R.T. Jones Oblique Wing model: landing configuration ARC-1972-A72-1961

R.T. Jones Oblique Wing model: landing configuration ARC-1972-A72-1961

R.T. Jones Oblique Wing model: landing configuration Public domain photograph of NASA experimental aircraft, free to use, no copyright restrictions image - Picryl description

R.T. Jones Oblique Wing model: flight configuration ARC-1972-A72-1962

R.T. Jones Oblique Wing model: flight configuration ARC-1972-A72-1962

R.T. Jones Oblique Wing model: flight configuration Public domain photograph of NASA experimental aircraft, free to use, no copyright restrictions image - Picryl description

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION INST SCOOP AND MICROPHONE BOOM ARRAY

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION INST SCOOP AND MICROPH...

The original finding aid described this as: Capture Date: 12/19/1973 Photographer: PAUL RIEDEL Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION NO. 3

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION NO. 3

The original finding aid described this as: Capture Date: 12/14/1973 Photographer: PAUL RIEDEL Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION INST SCOOP AND MICROPHONE BOOM ARRAY

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION INST SCOOP AND MICROPH...

The original finding aid described this as: Capture Date: 12/19/1973 Photographer: PAUL RIEDEL Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION INST SCOOP AND MICROPHONE BOOM ARRAY

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION INST SCOOP AND MICROPH...

The original finding aid described this as: Capture Date: 12/19/1973 Photographer: PAUL RIEDEL Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION NO. 3

GENERAL ELECTRIC GE AND BB&N TEST CONFIGURATION NO. 3

The original finding aid described this as: Capture Date: 12/14/1973 Photographer: PAUL RIEDEL Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

GENERAL ELECTRIC GE AND BBN TEST CONFIGURATION

GENERAL ELECTRIC GE AND BBN TEST CONFIGURATION

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

GENERAL ELECTRIC GE AND BBN TEST CONFIGURATION

GENERAL ELECTRIC GE AND BBN TEST CONFIGURATION

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

GENERAL ELECTRIC GE AND BBN TEST CONFIGURATION

GENERAL ELECTRIC GE AND BBN TEST CONFIGURATION

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

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR APRON QUIET ENGINE SITE

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR...

The original finding aid described this as: Capture Date: 10/7/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 4 Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

TITAN CENTAUR 6-2 CONFIGURATION AND DISTORTION BARS

TITAN CENTAUR 6-2 CONFIGURATION AND DISTORTION BARS

The original finding aid described this as: Capture Date: 2/20/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

TITAN CENTAUR VENT TEST CONFIGURATION 3-2

TITAN CENTAUR VENT TEST CONFIGURATION 3-2

The original finding aid described this as: Capture Date: 1/24/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

The original finding aid described this as: Capture Date: 4/12/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR APRON QUIET ENGINE SITE

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR...

The original finding aid described this as: Capture Date: 10/7/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 4 Photographs Relating to Agency Activities, Facilities and Personnel

TITAN CENTAUR VENT TEST CONFIGURATION 3-2

TITAN CENTAUR VENT TEST CONFIGURATION 3-2

The original finding aid described this as: Capture Date: 1/24/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

The original finding aid described this as: Capture Date: 4/12/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

TITAN CENTAUR VENT CONFIGURATION 4-2 IN THE 8X6 FOOT WIND TUNNEL

TITAN CENTAUR VENT CONFIGURATION 4-2 IN THE 8X6 FOOT WIND TUNNEL

The original finding aid described this as: Capture Date: 1/22/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET - 60-40 TAKEOFF CONFIGURATION

J-85 F-106 AIRPLANE SPIKE INLET - 60-40 TAKEOFF CONFIGURATION

The original finding aid described this as: Capture Date: 9/27/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

FORWARD THRUST CONFIGURATION OF THRUST REVERSER AIRPLANE MODEL

FORWARD THRUST CONFIGURATION OF THRUST REVERSER AIRPLANE MODEL

The original finding aid described this as: Capture Date: 4/8/1974 Photographer: PAUL RIEDEL Keywords: c1974_01100s 1974_01195.jpg Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

TITAN CENTAUR 6-2 CONFIGURATION AND DISTORTION BARS

TITAN CENTAUR 6-2 CONFIGURATION AND DISTORTION BARS

The original finding aid described this as: Capture Date: 2/20/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

The original finding aid described this as: Capture Date: 4/12/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

POSITIVE PITCH LOUVER CONFIGURATION OF TRAMP CASCADE ASSEMBLY

POSITIVE PITCH LOUVER CONFIGURATION OF TRAMP CASCADE ASSEMBLY

The original finding aid described this as: Capture Date: 3/28/1974 Photographer: PAUL RIEDEL Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

UTW FLAP REVERSER CONFIGURATION WITH AIR SUPPLY LINES REMOVED

The original finding aid described this as: Capture Date: 4/12/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR APRON QUIET ENGINE SITE

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR...

The original finding aid described this as: Capture Date: 10/7/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 4 Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR APRON QUIET ENGINE SITE

J-85 F-106 AIRPLANE SPIKE INLET 40-60 TAKE OFF CONFIGURATION AT HANGAR...

The original finding aid described this as: Capture Date: 10/7/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 4 Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET 40-60 APPROACH CONFIGURATION AT THE HANGAR APRON

J-85 F-106 AIRPLANE SPIKE INLET 40-60 APPROACH CONFIGURATION AT THE HA...

The original finding aid described this as: Capture Date: 10/3/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 4 Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

TITAN CENTAUR VENT TEST CONFIGURATION 3-2

TITAN CENTAUR VENT TEST CONFIGURATION 3-2

The original finding aid described this as: Capture Date: 1/24/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET 40-60 APPROACH CONFIGURATION AT THE HANGAR APRON

J-85 F-106 AIRPLANE SPIKE INLET 40-60 APPROACH CONFIGURATION AT THE HA...

The original finding aid described this as: Capture Date: 10/3/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Location Building No: 4 Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOOT WIND TUNNEL

CONFIGURATION AND INSTALLATION OF 5.5 INCH SONIC INLET IN THE 9X15 FOO...

The original finding aid described this as: Capture Date: 2/28/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 39 Photographs Relating to Agency Activities, Facilities and Personnel

POSITIVE PITCH LOUVER CONFIGURATION OF TRAMP CASCADE ASSEMBLY

POSITIVE PITCH LOUVER CONFIGURATION OF TRAMP CASCADE ASSEMBLY

The original finding aid described this as: Capture Date: 3/28/1974 Photographer: PAUL RIEDEL Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

JP-2 COMBUSTOR FUEL STRUT CONFIGURATION

JP-2 COMBUSTOR FUEL STRUT CONFIGURATION

The original finding aid described this as: Capture Date: 6/24/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET - 60-40 TAKEOFF CONFIGURATION

J-85 F-106 AIRPLANE SPIKE INLET - 60-40 TAKEOFF CONFIGURATION

The original finding aid described this as: Capture Date: 9/27/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

J-85 F-106 AIRPLANE SPIKE INLET - 60-40 TAKEOFF CONFIGURATION

J-85 F-106 AIRPLANE SPIKE INLET - 60-40 TAKEOFF CONFIGURATION

The original finding aid described this as: Capture Date: 9/27/1974 Photographer: DONALD HUEBLER Keywords: Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

POSITIVE PITCH LOUVER CONFIGURATION OF TRAMP CASCADE ASSEMBLY

POSITIVE PITCH LOUVER CONFIGURATION OF TRAMP CASCADE ASSEMBLY

The original finding aid described this as: Capture Date: 3/28/1974 Photographer: PAUL RIEDEL Keywords: c1974_01000s 1974_01088.jpg Larsen Scan Photographs Relating to Agency Activities, Facilities and Personnel

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR NOZZLE AT THE 8X6 FOOT WIND TUNNEL

MODEL NOZZLE CONFIGURATION OF GENERAL ELECTRIC GE FLUIDYNE SUPPRESSOR ...

The original finding aid described this as: Capture Date: 5/29/1974 Photographer: MARTIN BROWN Keywords: Larsen Scan Location Building No: 54 Photographs Relating to Agency Activities, Facilities and Personnel

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