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Space Shuttle Orbiter and Earth of Johnson Space Center (JSC)
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X-38
One of NASA's three X-38 Cre
11/4/09
| Description |
One of NASA's three X-38 Crew Return Vehicle technology demonstrators that flew at NASA's Dryden Flight Research Center at Edwards Air Force Base, Calif., a decade ago has found a new home in America's heartland. In this image from test flights in 1999, the X-38 research vehicle drops away from NASA's B-52 mothership immediately after being released from the B-52's wing pylon. More than 30 years earlier, this same B-52 launched the original lifting-body vehicles flight tested by NASA and the Air Force at what is now called the Dryden Flight Research Center and the Air Force Flight Test Center. The wingless lifting body craft was transferred this past weekend from NASA's Johnson Space Center in Houston to the Strategic Air and Space Museum, located just off Interstate 80 at Ashland, Neb., about 20 miles southeast of Omaha. The X-38 adds to the museum's growing collection of aerospace vehicles and other historical artifacts. The move of the second X-38 built to the museum has a fitting connection, as the X-38 vehicles were air-launched from NASA's famous B-52B 008 mothership. The B-52 bomber served as the backbone of the Air Force's Strategic Air Command during the command's history. Prior to cancellation, the X-38 program was developing the technology for proposed vehicles that could return up to seven International Space Station crewmembers to Earth in case of an emergency. These vehicles would have been carried to the space station in the cargo bay of a space shuttle and attached to station docking ports. If an emergency arose that forced the ISS crew to leave the space station, a Crew Return Vehicle would have undocked and returned them to Earth much like the space shuttle, although the vehicle would have deployed a parafoil for the final descent and landing. Photo Credit: NASA/Carla Thomas |
| Date |
11/4/09 |
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Houston, Texas L & C bands
This image of Houston, Texas
6/8/95
| Date |
6/8/95 |
| Description |
This image of Houston, Texas, shows the amount of detail that is possible to obtain using spaceborne radar imaging. Images such as this -- obtained by the Spaceborne Imaging Radar-C/X-band Synthetic Aperture Radar (SIR-C/X-SAR) flying aboard the space shuttle Endeavor last fall -- can become an effective tool for urban planners who map and monitor land use patterns in urban, agricultural and wetland areas. Central Houston appears pink and white in the upper portion of the image, outlined and crisscrossed by freeways. The image was obtained on October 10, 1994, during the space shuttle's 167th orbit. The area shown is 100 kilometers by 60 kilometers (62 miles by 38 miles) and is centered at 29.38 degrees north latitude, 95.1 degrees west longitude. North is toward the upper left. The pink areas designate urban development while the green- and blue-patterned areas are agricultural fields. Black areas are bodies of water, including Galveston Bay along the right edge and the Gulf of Mexico at the bottom of the image. Interstate 45 runs from top to bottom through the image. The narrow island at the bottom of the image is Galveston Island, with the city of Galveston at its northeast (right) end. The dark cross in the upper center of the image is Hobby Airport. Ellington Air Force Base is visible below Hobby on the other side of Interstate 45. Clear Lake is the dark body of water in the middle right of the image. The green square just north of Clear Lake is Johnson Space Center, home of Mission Control and the astronaut training facilities. The black rectangle with a white center that appears to the left of the city center is the Houston Astrodome. The colors in this image were obtained using the follow radar channels: red represents the L-band (horizontally transmitted, vertically received), green represents the C-band (horizontally transmitted, vertically received), blue represents the C-band (horizontally transmitted and received). ----- Spaceborne Imaging Radar-C/X-band Synthetic Aperture Radar(SIR- C/X-SAR) is part of NASA's Mission to Planet Earth. The radars illuminate Earth with microwaves, allowing detailed observations at any time, regardless of weather or sunlight conditions. SIR- C/X-SAR uses three microwave wavelengths: L-band (24 cm), C-band (6 cm) and X-band (3 cm). The multi-frequency data will be used by the international scientific community to better understand the global environment and how it is changing. The SIR-C/X-SAR data, complemented by aircraft and ground studies, will give scientists clearer insights into those environmental changes which are caused by nature and those changes which are induced by human activity. SIR-C was developed by NASA's Jet Propulsion Laboratory. X-SAR was developed by the Dornier and Alenia Spazio companies for the German space agency, Deutsche Agentur fuer Raumfahrtangelegenheiten (DARA), and the Italian space agency, Agenzia Spaziale Italiana (ASI) with the Deutsche Forschungsanstalt fuer luft und Raumfahrt e.V.(DLR), the major partner in science, operations and data processing of X-SAR. ##### |
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Moon Framed
| Title |
Moon Framed |
| Full Description |
The moon is framed between the Orbiter's OMS pod and the Earth limb over the Atlantic Ocean as seen from the aft windows onboard Discovery on mission STS-95. |
| Date |
11/06/1998 |
| NASA Center |
Johnson Space Center |
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Moon Set over Earth
| Title |
Moon Set over Earth |
| Full Description |
Moon set over the Earth limb taken from Space Shuttle Discovery during STS-70 mission. |
| Date |
07/14/1995 |
| NASA Center |
Johnson Space Center |
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Arm in Arm
| Title |
Arm in Arm |
| Full Description |
Backdropped against the blue and white Earth, Mission Specialist (MS) and Payload Commander (PLC) G. David Low and (MS) Peter J.K. Wisoff, wearing Extravehicular Mobility Units (EMUs), simulate handling of large components in space. Above Endeavour's Payload Bay (PLB), Low, anchored by a Portable Foot Restraint (PFR) Manipulator Foot Restraint (MFR) on the Remote Manipulator System (RMS) end effector, maneuvers Wisoff, representing the mass of a large space component. This particular task was rehearsed with eyes toward the servicing of the Hubble Space Telescope (HST) or the assembly and maintenance of Space Station. This Extravehicular Activity (EVA), Detailed Test Objective (DTO) was conducted both with and without intentional disturbances from Endeavour's thrusters and movements of the RMS. The SPACEHAB-01 Commercial Middeck Augmentation Module (CMAM)) is visible in the foreground with the Superfluid Helium On Orbit Transfer (SHOOT) payload liquid helium dewar assembly and the European Retrievable Carrier (EURECA) only partially visible in the aft PLB shadows. The vertical stabilizer and Orbital Maneuvering System (OMS) pods are silhouetted against the Earth's surface. |
| Date |
06/25/1993 |
| NASA Center |
Johnson Space Center |
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Assembling Structures in the
| Title |
Assembling Structures in the Payload Bay |
| Full Description |
STS-49 Mission Specialist (MS) Kathryn C. Thornton (foreground) releases a strut from the Multipurpose Experiment Support Structure (MPESS) strut dispenser during Assembly of Station by Extravehicular Activity Methods (ASEM) procedures in Endeavour's payload bay. MS Thomas D. Akers, positioned on the opposite side of the MPESS, waits for Thornton to hand him the final strut. The two astronauts are building the ASEM structure during the mission's fourth EVA. The ASEM structure, locked in at four corners to payload retention latch assemblies (PRLAs), rises above the payload bay. In the background are the Intelsat cradle, the vertical tail, and the orbital maneuvering system (OMS) pods. The pale blue and white Earth is visible below. |
| Date |
05/01/1992 |
| NASA Center |
Johnson Space Center |
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Orbital Sunrise
| Title |
Orbital Sunrise |
| Full Description |
The STS-68 crew aboard the Space Shuttle Endeavour told a post-flight audience at JSC that this sunrise was one of the most scenic sunrises/ sunsets witnessed during the week and a half long Space Radar Laboratory (SRL-2) mission. Jutting clouds, back-lit by the dawn colors, are sandwiched between the blue airglow and the silhouetted horizon of Earth. |
| Date |
10/11/1994 |
| NASA Center |
Johnson Space Center |
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Orbital Sunrise with Venus a
| Title |
Orbital Sunrise with Venus and Mars |
| Full Description |
View of Earth limb horizon during sunrise with Mars and Venus rising. |
| Date |
08/03/1995 |
| NASA Center |
Johnson Space Center |
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Astronaut U.S. Senator John
| Title |
Astronaut U.S. Senator John Glenn |
| Full Description |
STS-95 crewmember, astronaut and U.S. Senator John Glenn. Glenn was the first American to orbit the earth and returned to space in 1998 aboard a Space Shuttle flight. |
| Date |
04/14/1998 |
| NASA Center |
Johnson Space Center |
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Atlantis departing Mir
| Title |
Atlantis departing Mir |
| Full Description |
A view of the Space Shuttle Atlantis departing the Mir Russian Space Station. This image was taken during the STS-71 mission by cosmonauts aboard their Soyuz TM transport vehicle. The scene is backdropped by the Earth's limb. |
| Date |
07/04/1995 |
| NASA Center |
Johnson Space Center |
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Backpacking
| Title |
Backpacking |
| Full Description |
Mission Specialist Bruce McCandless II ventured further away from the confines and safety of his ship than any previous astronaut ever has. This space first was made possible by the Manned Manuevering Unit or MMU, a nitrogen jet propelled backpack. After a series of test maneuvers inside and above Challenger's payload bay, McCandless went "free-flying" to a distance of 320 feet away from the Orbiter. The MMU is controled by joy sticks positioned at the end of the arm rests. Moving the joy sticks left or right or by pulling them fires nitrogen jet thrusters propelling McCandless in any direction he chooses. A still camera is mounted on the upper right portion of the MMU. This stunning view shows McCandless with the MMU out there amongst the black and blue of Earth and space. |
| Date |
02/11/1984 |
| NASA Center |
Johnson Space Center |
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Challenger as seen from SPAS
| Title |
Challenger as seen from SPAS |
| Full Description |
Full view of Space Shuttle Orbiter Challenger in space, taken by the Space Pallet Satellite (SPAS). A heavily cloud-covered portion of the earth forms the backdrop for this scene of Challenger. Visible in the payload bay are the protective cradles for the Palapa-B and Telesat F communications satellites, the pallet for the NASA Office of Space and Terrestrial Applications (OSTA-2), the Remote Manipulator System (RMS) robot arm in the shape of the numeral seven and the KU- band antenna. A number of GetAway Special (GAS) canisters are also visible along the port side. |
| Date |
06/22/1983 |
| NASA Center |
Johnson Space Center |
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Clouds and Sunglint over Ind
| Title |
Clouds and Sunglint over Indian Ocean |
| Full Description |
Clouds and sunglint as seen during the STS-96 mission from the Space Shuttle Discovery. |
| Date |
06/01/1999 |
| NASA Center |
Johnson Space Center |
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Rick Hieb peers into the fli
| Title |
Rick Hieb peers into the flight deck |
| Full Description |
Rick Hieb, a Mission Specialist aboard STS-49, looks into the aft flight deck of the orbiter during his spacewalk. STS-49, which launched on May 7, 1992 and returned:to Earth on May 16, 1992, marked the first flight of Endeavour and the first shuttle mission to feature four EVAs. Hieb, along with fellow astronauts Pierre Thuot and Thomas Akers helped to recover INTELSAT VI, a communications satellite whose orbit had become unstable. |
| Date |
05/16/1992 |
| NASA Center |
Johnson Space Center |
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Robot Arm Over Earth with Su
| Title |
Robot Arm Over Earth with Sunburst |
| Full Description |
View of the Remote Manipulator System (RMS) end effector over an Earth limb with a solar starburst pattern behind it. |
| Date |
06/01/1996 |
| NASA Center |
Johnson Space Center |
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SAFER Rescue System Tested
| Title |
SAFER Rescue System Tested |
| Full Description |
Astronauts Carl J. Meade and Mark C. Lee (red strip on suit) test the new Simplified Aid for EVA Rescue (SAFER) system some 130 nautical miles above Earth. The pair was actually performing an in-space rehearsal or demonstration of a contingency rescue using never-before flown hardware. Meade, who here wears the small back-pack unit with its complementary chest-mounted control unit, and Lee anchored to the Space Shuttle Discovery's Remote Manipulator System (RMS) robot arm, took turns using the SAFER hardware during their shared space walk. |
| Date |
09/16/1994 |
| NASA Center |
Johnson Space Center |
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SAFER Tests by Meade and Lee
| Title |
SAFER Tests by Meade and Lee |
| Full Description |
Astronauts Carl J. Meade and Mark C. Lee (red stripe on suit) test the Simplified Aid for EVA Rescue (SAFER) system some 130 nautical miles from Earth. The pair were actually performing an in-space rehearsal or demonstration of a contingency rescue using the never- before flown hardware. Meade, who here wears the small back-pack unit with its complementary chest-mounted control unit, and Lee, anchored to Discovery's Remote Manipulator System (RMS) robot arm, took turns using the SAFER hardware during their shared space walk of September 16, 1994. |
| Date |
09/16/1994 |
| NASA Center |
Johnson Space Center |
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Sally Ride, First U.S. Woman
| Title |
Sally Ride, First U.S. Woman in Space |
| Full Description |
Sally Ride was the first American woman in space. Born on May 26, 1951 in Los Angeles, California, she received a Bachelor in Physics and English in 1973 from Stanford University and, later, a Master in Physics in 1975 and a Doctorate in Physics in 1978, also from Stanford. NASA selected Dr. Ride as an astronaut candidate in January 1978. She completed her training in August 1979, and began her astronaut career as a mission specialist on STS-7, which launched from Kennedy Space Center, Florida on June 18, 1983. The mission spent 147 hours in space before landing on a lakebed runway at Edwards Air Force Base, California on June 24, 1983. Dr. Ride also served as a mission specialist on STS-41-G, which launched from Kennedy Space Center, Florida on October 5, 1984 and landed 197 hours later at Kennedy Space Center, Florida on October 13, 1984. In June 1985, NASA assigned Dr. Ride to serve as mission specialist on STS-61-M. She discontinued mission training in January 1986 to serve as a member of the Presidential Commission on the Space Shuttle Challenger accident, also known as the Rogers Commission. Upon completing the investigation she returned to NASA Headquarters as Special Assistant to the Administrator for Long Range and Strategic Planning, where she lead a team that wrote NASA Leadership and America's Future in Space:A Report to the Administrator in August 1987. Dr. Ride has also written a children's book, To Space and Back, describing her experiences in space, has received the Jefferson Award for Public Service, and has twice been awarded the National Spaceflight Medal. Her latest books include Voyager: An Adventure to the Edge of the Solar System and The Third Planet: Exploring the Earth from Space. She was also a member of the Columbia Accident Investigation Board (CAIB), which investigated the February 1, 2003 loss of Space Shuttle Columbia. Dr. Ride is currently a physics professor and Director of the California Space Institute at the University of California, San Diego. |
| Date |
06/1984 |
| NASA Center |
Johnson Space Center |
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EVAtion
| Title |
EVAtion |
| Full Description |
Mission Specialist Bruce McCandless II, is seen further away from the confines and safety of his ship than any previous astronaut has ever been. This space first was made possible by the Manned Manuevering Unit or MMU, a nitrogen jet propelled backpack. After a series of test maneuvers inside and above Challenger's payload bay, McCandless went "free-flying" to a distance of 320 feet away from the Orbiter. This stunning orbital panorama view shows McCandless out there amongst the black and blue of Earth and space. |
| Date |
02/12/1984 |
| NASA Center |
Johnson Space Center |
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Standing on the Edge of the
| Title |
Standing on the Edge of the Bay |
| Full Description |
Mission Specialist James H. Newman conducts an in-space evaluation of the Portable Foot Restraint (PFR) which will be used operationally on the first Hubble Space Telescope (HST) servicing mission and future Shuttle missions. He is positioned on the edge of Discovery's payload bay. Behind him the starboard Orbital Maneuvering System (OMS) pod can be seen with the soft glow of an Earth limb. |
| Date |
09/16/1993 |
| NASA Center |
Johnson Space Center |
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Female Astronauts
| Title |
Female Astronauts |
| Full Description |
Astronauts Dr. N. Jan Davis (left) and Dr. Mae C. Jemison (right) were mission specialists on board the STS-47 mission. Born on November 1, 1953 in Cocoa Beach, Florida, Dr. N. Jan Davis received a Master degree in Mechanical Engineering in 1983 followed by a Doctorate in Engineering from the University of Alabama in Huntsville in 1985. In 1979 she joined NASA Marshall Space Flight Center as an aerospace engineer. A veteran of three space flights, Dr. Davis has logged over 678 hours in space since becoming an astronaut in 1987. She flew as a mission specialist on STS-47 in 1992 and STS-60 in 1994, and was the payload commander on STS-85 in 1997. In July 1999, she transferred to the Marshall Space Flight Center, where she became Director of Flight Projects. Dr. Mae C. Jemison, the first African-American woman in space, was born on October 17, 1956 in Decatur, Alabama but considers Chicago, Illinois her hometown. She received a Bachelor degree in Chemical Engineering (and completed the requirements for a Bachelor degree in African and Afro-American studies) at Stanford University in 1977, and a Doctorate degree in medicine from Cornell University in 1981. After receiving her doctorate, she worked as a General Practitioner while attending graduate engineering classes in Los Angeles. She was named an astronaut candidate in 1987, and flew her first flight as a science mission specialists on STS-47, Spacelab-J, in September 1992, logging 190 hours, 30 minutes, 23 seconds in space. In March 1993, Dr. Jemison resigned from NASA, thought she still resides in Houston, Texas. She went on to publish her memoirs, Find Where the Wind Goes: Moments from My Life, in 2001. The astronauts are shown preparing to deploy the lower body negative pressure (LBNP) apparatus in this 35mm frame taken in the science module aboard the Earth-orbiting Space Shuttle Endeavor. Fellow astronauts Robert L. Gibson (Commander), Curtis L. Brown (Junior Pilot), Mark C. Lee (Payload Commander), Jay Apt (Mission Specialist), and Mamoru Mohri (Payload Specialist) joined the two on their maiden space flight. The Spacelab-J mission was a joint effort between Japan and the United States. |
| Date |
09/15/1992 |
| NASA Center |
Johnson Space Center |
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First Class of Female Astron
| Title |
First Class of Female Astronauts |
| Full Description |
From left to right are Shannon W. Lucid, Margaret Rhea Seddon, Kathryn D. Sullivan, Judith A. Resnik, Anna L. Fisher, and Sally K. Ride. NASA selected all six women as their first female astronaut candidates in January 1978, allowing them to enroll in a training program that they completed in August 1979. Shannon W. Lucid was born on January 14, 1943 in Shanghai, China but considers Bethany, Oklahoma to be her hometown. She spent many years at the University of Oklahoma, receiving a Bachelor in chemistry in 1963, a Master in biochemistry in 1970, and a Doctorate in biochemistry in 1973. Dr. Lucid flew on the STS-51G Discovery, STS-34 Atlantis, STS-43 Atlantis, and STS-58 Columbia shuttle missions, setting the record for female astronauts by logging 838 hours and 54 minutes in space. She also currently holds the United States single mission space flight endurance record for her 188 days on the Russian Space Station Mir. From February 2002 to September 2003, she served as chief scientist at NASA Headquarters before returning to JSC to help with the Return to Flight program after the STS-107 accident. Born November 8, 1947, in Murfreesboro, Tennessee, Margaret Rhea Seddon received a Doctorate of Medicine in 1973 from the University of Tennessee. She flew on space missions STS-51 Discovery, STS-40 Columbia, and STS-58 Columbia for a total of over 722 hours in space. Dr. Seddon retired from NASA in November 1997, taking on a position as the Assistant Chief Medical Officer of the Vanderbilt Medical Group in Nashville, Tennessee. Kathryn Sullivan was born October 3, 1951 in Patterson, New Jersey but considers Woodland Hills, California to be her hometown. She received a Bachelor in Earth Sciences from the University of California, Santa Cruz in 1973 and a Doctorate in Geology from Dalhousie University in Halifax, Nova Scotia in 1978. She flew on space missions STS-41G, STS-31, and STS-45 and logged a total of 532 hours in space. Dr. Sullivan left NASA in August 1992 to assume the position of Chief Scientist of the National Oceanic and Atmospheric Administration (NOAA). She later went on to serve as President and CEO of the Center of Science and Industry in Columbus, Ohio. Dr. Judith Resnik was born April 5, 1949 in Akron, Ohio. She received a Bachelor of Science degree in Electrical Engineering from Carnegie-Mellon University in 1970, and a Doctorate in Electrical Engineering from University of Maryland in 1977. Dr. Resnik left a job as a senior systems engineer in product development with Xerox Corporation at El Segundo, California to work for NASA in 1978. She died on January 28, 1986 on her second mission, during the launch of Challenger STS-51-L. Anna Fisher was born August 24, 1949 in New York City, New York hometown. She received a Doctorate in Medicine in 1976 and a Master of Science in Chemistry in 1987, both from the University of California, Los Angeles. Dr. Fisher flew on STS-51A, the Space Shuttle Discovery's November 8, 1984, mission, and logged 192 hours in space, her second schedule mission was cancelled after the Space Shuttle Challenger STS-51L accident. She remains with NASA, where she has filled many positions over decades of service. Dr. Sally Ride was the first American woman in space. Born on May 26, 1951 in Los Angeles, California, she went on to receive a Bachelor in Physics and English in 1973 from Stanford University and, later, a Master in Physics in 1975 and a Doctorate in Physics in 1978, also from Stanford. She began her astronaut career as a mission specialist on STS-7, which launched from Kennedy Space Center, Florida on June 18, 1983, and later went on to fly on STS-41G. She withdrew from training for her third scheduled mission in order to serve on the investigative committee for the Space Shuttle Challenger accident and never returned to training, although she went on to work for headquarters and later to serve on the Columbia Accident Investigation Board before returning to the private sector as a physics professor. |
| Date |
02/28/1979 |
| NASA Center |
Johnson Space Center |
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Florida From Space
| Title |
Florida From Space |
| Full Description |
Taken during the STS-95 mission from a point over Cuba, this photo shows an oblique, foreshortened view of the Florida Peninsula, with the light blue, shallow seafloor of both the Florida Keys (curving across the bottom of the view) and the Bahama banks (right). "Popcorn" cumulus cloud covers Miami and the Southern Everglades, although the built-up area from Ft. Lauderdale to West Palm Beach can be discerned. Lake Okeechobee is the prominent waterbody in Florida. Cape Canaveral is shown well, half way up the peninsula. Orlando appears as the lighter patch West (left) of Cape Canaveral, near the middle of the peninsula. Cape Hatteras appears top right, with the North part of Chesapeake Bay also visible. This is a visibility of 16 degrees of latitude (23 degrees N over Cuba to 39 degrees at Baltimore), showing unusual atmospheric clarity. |
| Date |
10/31/1998 |
| NASA Center |
Johnson Space Center |
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Gernhardt on Robot Arm
| Title |
Gernhardt on Robot Arm |
| Full Description |
The pale blue Earth serves as backdrop for astronaut Michael Gernhardt during his Extravehicular Activity (EVA). He is standing on a Manipulator Foot Restraint (MFR) attached to the Remote Manipulator System (RMS). He is positioned over the Payload Bay and Endeavour's forward section is reflected in his visor. A thermal cube is attached to the RMS and records temperatures during spacesuit evaluations. Unlike earlier spacewalking astronauts, Gernhardt was able to use an electronic cuff checklist, a prototype developed for the assembly of the International Space Station (ISS). |
| Date |
09/16/1995 |
| NASA Center |
Johnson Space Center |
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Sullivan Views the Earth
| Title |
Sullivan Views the Earth |
| Full Description |
Astronaut Kathryn D. Sullivan, 41-G mission specialist, uses binoculars for a magnifed viewing of Earth through Challenger's forward cabin windows. |
| Date |
10/06/1984 |
| NASA Center |
Johnson Space Center |
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Hubble Space Telescope and E
| Title |
Hubble Space Telescope and Earth Limb |
| Full Description |
Flyaround of the Hubble Space Telescope (HST) after deployment on this second servicing mission (HST SM-02). Note the telescope's open aperature door. |
| Date |
02/19/1997 |
| NASA Center |
Johnson Space Center |
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Thornton Prepares to Release
| Title |
Thornton Prepares to Release Hubble Array |
| Full Description |
To run all their systems, satellites need a way to generate power for months, even years. Most Earth-orbiting spacecraft, like the Hubble Space Telescope, rely on solar cells to recharge their onboard batteries. But solar panels have their own set of problems. They must be lightweight and flexible to fit inside a relatively small launch vehicle. Consequently, they tend to be fragile, and several satellites have had to cope with damaged panels once in orbit. That is what happened to the Hubble Space Telescope. Fortunately, the telescope was designed for on-orbit repairs, and astronauts were able to remove the damaged panel and replace it with a new one. In this image, Astronaut Kathy Thornton releases the old panel into low-Earth orbit during the first Hubble Space Telescope Servicing Mission in 1993. Earth's gravitation pulled the jettisoned panel toward Earth's atmosphere, where it entered and ultimately burned up. |
| Date |
10/14/1994 |
| NASA Center |
Johnson Space Center |
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Throttling Upward
| Title |
Throttling Upward |
| Full Description |
Aerial views of the STS-2 launch from Pad 39A at Kennedy Space Center. This photograph of Columbia soaring toward earth orbit was captured by Mission- Specialist/Astronaut Kathryn D. Sullivan from the rear station of a T-38 jet aircraft. Part of the wing top of her aircraft can be seen in the lower left corner. Another T-38 jet can be seen at lower left corner near the smoke trails from the Shuttle. |
| Date |
11/12/1981 |
| NASA Center |
Johnson Space Center |
|
Wisoff on the Arm
| Title |
Wisoff on the Arm |
| Full Description |
Against the blackness of space, Mission Specialist Peter J.K. Wisoff, wearing an extravehicular mobility unit, stands on a Portable Foot Restraint (PFR), Manipulator Foot Restrait (MFR) attached to the End Effector of the Remote Manipulator System (RMS), colloquially known as the "robot arm". Wisoff is being maneuvered above Endeavour's payload bay as part of Detailed Test Objective (DTO) extravehicular activity procedures. DTO results will assist in refining several procedures being developed to service the Hubble Space Telescope on mission STS-61 in December 1993. The Earth's surface and Discovery's payload bay are reflected in Wisoff's helmet visor. |
| Date |
06/25/1993 |
| NASA Center |
Johnson Space Center |
|
X-38: Artist Concept of Re-E
| Photo Description |
This is an artist's depiction of NASA's proposed Crew Return Vehicle (CRV) re-entering the earth's atmosphere. A team of NASA researchers began free flight tests of the X-38, a technology demonstrator for the CRV, at NASA's Dryden Flight Research Center, Edwards, California, in 1998. The CRV is being designed as a "lifeboat" for the International Space Station |
| Project Description |
The X-38 Crew Return Vehicle (CRV) research project is designed to develop the technology for a prototype emergency crew return vehicle, or lifeboat, for the International Space Station. The project is also intended to develop a crew return vehicle design that could be modified for other uses, such as a joint U.S. and international human spacecraft that could be launched on the French Ariane-5 Booster. The X-38 project is using available technology and off-the-shelf equipment to significantly decrease development costs. Original estimates to develop a capsule-type crew return vehicle were estimated at more than $2 billion. X-38 project officials have estimated that development costs for the X-38 concept will be approximately one quarter of the original estimate. Off-the-shelf technology is not necessarily "old" technology. Many of the technologies being used in the X-38 project have never before been applied to a human-flight spacecraft. For example, the X-38 flight computer is commercial equipment currently used in aircraft and the flight software operating system is a commercial system already in use in many aerospace applications. The video equipment for the X-38 is existing equipment, some of which has already flown on the space shuttle for previous NASA experiments. The X-38's primary navigational equipment, the Inertial Navigation System/Global Positioning System, is a unit already in use on Navy fighters. The X-38 electromechanical actuators come from previous joint NASA, U.S. Air Force, and U.S. Navy research and development projects. Finally, an existing special coating developed by NASA will be used on the X-38 thermal tiles to make them more durable than those used on the space shuttles. The X-38 itself was an unpiloted lifting body designed at 80 percent of the size of a projected emergency crew return vehicle for the International Space Station, although two later versions were planned at 100 percent of the CRV size. The X-38 and the actual CRV are patterned after a lifting-body shape first employed in the Air Force-NASA X-24 lifting-body project in the early to mid-1970s. The current vehicle design is base lined with life support supplies for about nine hours of orbital free flight from the space station. ItÕs landing will be fully automated with backup systems which allow the crew to control orientation in orbit, select a deorbit site, and steer the parafoil, if necessary. The X-38 vehicles (designated V131, V132, and V-131R) are 28.5 feet long, 14.5 feet wide, and weigh approximately 16,000 pounds on average. The vehicles have a nitrogen-gas-operated attitude control system and a bank of batteries for internal power. The actual CRV to be flown in space was expected to be 30 feet long. The X-38 project is a joint effort between the Johnson Space Center, Houston, Texas (JSC), Langley Research Center, Hampton, Virginia (LaRC) and Dryden Flight Research Center, Edwards, California (DFRC) with the program office located at JSC. A, contract was awarded to Scaled Composites, Inc., Mojave, California, for construction of the X-38 test airframes. The first vehicle was delivered to the JSC in September 1996. The vehicle was fitted with avionics, computer systems and other hardware at Johnson. A second vehicle was delivered to JSC in December 1996. Flight research with the X-38 at Dryden began with an unpiloted captive-carry flight in which the vehicle remained attached to its future launch vehicle, DrydenÕs B-52 008. There were four captive flights in 1997 and three in 1998, plus the first drop test on March 12, 1998, using the parachutes and parafoil. Further captive and drop tests occurred in 1999. In March 2000 Vehicle 132 completed its third and final free flight in the highest, fastest, and longest X-38 flight to date. It was released at an altitude of 39,000 feet and flew freely for 45 seconds, reaching a speed of over 500 miles per hour before deploying its parachutes for a landing on Rogers Dry Lakebed. In the drop tests, the X-38 vehicles have been autonomous after airlaunch from the B-52. After they deploy the parafoil, they have remained autonomous, but there is also a manual mode with controls from the ground. |
| Photo Date |
1997 |
|
X-38 research aircraft remov
Research pilot Fred Haise
Research pilot Mark Pestana
| Photo Date |
April 16, 2001 |
|
X-38 Drop Model: Glides to E
| Photo Description |
A 4-foot-long model of NASA's X-38, an experimental crew return vehicle, glides to earth after being dropped from a Cessna aircraft in late 1995. The model was used to test the ram-air parafoil landing system, which could allow for accurate and controlled landings of an emergency Crew Return Vehicle spacecraft returning to Earth. |
| Project Description |
The X-38 Crew Return Vehicle (CRV) research project is designed to develop the technology for a prototype emergency crew return vehicle, or lifeboat, for the International Space Station. The project is also intended to develop a crew return vehicle design that could be modified for other uses, such as a joint U.S. and international human spacecraft that could be launched on the French Ariane-5 Booster. The X-38 project is using available technology and off-the-shelf equipment to significantly decrease development costs. Original estimates to develop a capsule-type crew return vehicle were estimated at more than $2 billion. X-38 project officials have estimated that development costs for the X-38 concept will be approximately one quarter of the original estimate. Off-the-shelf technology is not necessarily "old" technology. Many of the technologies being used in the X-38 project have never before been applied to a human-flight spacecraft. For example, the X-38 flight computer is commercial equipment currently used in aircraft and the flight software operating system is a commercial system already in use in many aerospace applications. The video equipment for the X-38 is existing equipment, some of which has already flown on the space shuttle for previous NASA experiments. The X-38's primary navigational equipment, the Inertial Navigation System/Global Positioning System, is a unit already in use on Navy fighters. The X-38 electromechanical actuators come from previous joint NASA, U.S. Air Force, and U.S. Navy research and development projects. Finally, an existing special coating developed by NASA will be used on the X-38 thermal tiles to make them more durable than those used on the space shuttles. The X-38 itself was an unpiloted lifting body designed at 80 percent of the size of a projected emergency crew return vehicle for the International Space Station, although two later versions were planned at 100 percent of the CRV size. The X-38 and the actual CRV are patterned after a lifting-body shape first employed in the Air Force-NASA X-24 lifting-body project in the early to mid-1970s. The current vehicle design is base lined with life support supplies for about nine hours of orbital free flight from the space station. ItÕs landing will be fully automated with backup systems which allow the crew to control orientation in orbit, select a deorbit site, and steer the parafoil, if necessary. The X-38 vehicles (designated V131, V132, and V-131R) are 28.5 feet long, 14.5 feet wide, and weigh approximately 16,000 pounds on average. The vehicles have a nitrogen-gas-operated attitude control system and a bank of batteries for internal power. The actual CRV to be flown in space was expected to be 30 feet long. The X-38 project is a joint effort between the Johnson Space Center, Houston, Texas (JSC), Langley Research Center, Hampton, Virginia (LaRC) and Dryden Flight Research Center, Edwards, California (DFRC) with the program office located at JSC. A, contract was awarded to Scaled Composites, Inc., Mojave, California, for construction of the X-38 test airframes. The first vehicle was delivered to the JSC in September 1996. The vehicle was fitted with avionics, computer systems and other hardware at Johnson. A second vehicle was delivered to JSC in December 1996. Flight research with the X-38 at Dryden began with an unpiloted captive-carry flight in which the vehicle remained attached to its future launch vehicle, DrydenÕs B-52 008. There were four captive flights in 1997 and three in 1998, plus the first drop test on March 12, 1998, using the parachutes and parafoil. Further captive and drop tests occurred in 1999. In March 2000 Vehicle 132 completed its third and final free flight in the highest, fastest, and longest X-38 flight to date. It was released at an altitude of 39,000 feet and flew freely for 45 seconds, reaching a speed of over 500 miles per hour before deploying its parachutes for a landing on Rogers Dry Lakebed. In the drop tests, the X-38 vehicles have been autonomous after airlaunch from the B-52. After they deploy the parafoil, they have remained autonomous, but there is also a manual mode with controls from the ground. |
| Photo Date |
1995 |
|
X-38 Drop Model: Used to Tes
| Photo Description |
A 4-foot-long model of NASA's X-38, an experimental crew return vehicle, glides to earth after being dropped from a Cessna aircraft in late 1995. The model was used to test the ram-air parafoil landing system, which could allow for accurate and controlled landings of an emergency Crew Return Vehicle spacecraft returning to Earth. |
| Project Description |
The X-38 Crew Return Vehicle (CRV) research project is designed to develop the technology for a prototype emergency crew return vehicle, or lifeboat, for the International Space Station. The project is also intended to develop a crew return vehicle design that could be modified for other uses, such as a joint U.S. and international human spacecraft that could be launched on the French Ariane-5 Booster. The X-38 project is using available technology and off-the-shelf equipment to significantly decrease development costs. Original estimates to develop a capsule-type crew return vehicle were estimated at more than $2 billion. X-38 project officials have estimated that development costs for the X-38 concept will be approximately one quarter of the original estimate. Off-the-shelf technology is not necessarily "old" technology. Many of the technologies being used in the X-38 project have never before been applied to a human-flight spacecraft. For example, the X-38 flight computer is commercial equipment currently used in aircraft and the flight software operating system is a commercial system already in use in many aerospace applications. The video equipment for the X-38 is existing equipment, some of which has already flown on the space shuttle for previous NASA experiments. The X-38's primary navigational equipment, the Inertial Navigation System/Global Positioning System, is a unit already in use on Navy fighters. The X-38 electromechanical actuators come from previous joint NASA, U.S. Air Force, and U.S. Navy research and development projects. Finally, an existing special coating developed by NASA will be used on the X-38 thermal tiles to make them more durable than those used on the space shuttles. The X-38 itself was an unpiloted lifting body designed at 80 percent of the size of a projected emergency crew return vehicle for the International Space Station, although two later versions were planned at 100 percent of the CRV size. The X-38 and the actual CRV are patterned after a lifting-body shape first employed in the Air Force-NASA X-24 lifting-body project in the early to mid-1970s. The current vehicle design is base lined with life support supplies for about nine hours of orbital free flight from the space station. ItÕs landing will be fully automated with backup systems which allow the crew to control orientation in orbit, select a deorbit site, and steer the parafoil, if necessary. The X-38 vehicles (designated V131, V132, and V-131R) are 28.5 feet long, 14.5 feet wide, and weigh approximately 16,000 pounds on average. The vehicles have a nitrogen-gas-operated attitude control system and a bank of batteries for internal power. The actual CRV to be flown in space was expected to be 30 feet long. The X-38 project is a joint effort between the Johnson Space Center, Houston, Texas (JSC), Langley Research Center, Hampton, Virginia (LaRC) and Dryden Flight Research Center, Edwards, California (DFRC) with the program office located at JSC. A, contract was awarded to Scaled Composites, Inc., Mojave, California, for construction of the X-38 test airframes. The first vehicle was delivered to the JSC in September 1996. The vehicle was fitted with avionics, computer systems and other hardware at Johnson. A second vehicle was delivered to JSC in December 1996. Flight research with the X-38 at Dryden began with an unpiloted captive-carry flight in which the vehicle remained attached to its future launch vehicle, DrydenÕs B-52 008. There were four captive flights in 1997 and three in 1998, plus the first drop test on March 12, 1998, using the parachutes and parafoil. Further captive and drop tests occurred in 1999. In March 2000 Vehicle 132 completed its third and final free flight in the highest, fastest, and longest X-38 flight to date. It was released at an altitude of 39,000 feet and flew freely for 45 seconds, reaching a speed of over 500 miles per hour before deploying its parachutes for a landing on Rogers Dry Lakebed. In the drop tests, the X-38 vehicles have been autonomous after airlaunch from the B-52. After they deploy the parafoil, they have remained autonomous, but there is also a manual mode with controls from the ground. |
| Photo Date |
1995 |
|
Shuttle Carrier Aircraft (SC
| Photo Description |
NASA's two Boeing 747 Shuttle Carrier Aircraft (SCA) are seen here nose to nose at Dryden Flight Research Center, Edwards, California. The front mounting attachment for the Shuttle can just be seen on top of each. The SCAs are used to ferry Space Shuttle orbiters from landing sites back to the launch complex at the Kennedy Space Center, and also to and from other locations too distant for the orbiters to be delivered by ground transportation. The orbiters are placed atop the SCAs by Mate-Demate Devices, large gantry-like structures which hoist the orbiters off the ground for post-flight servicing, and then mate them with the SCAs for ferry flights. Features which distinguish the two SCAs from standard 747 jetliners are, three struts, with associated interior structural strengthening, protruding from the top of the fuselage (two aft, one forward) on which the orbiter is attached, and two additional vertical stabilizers, one on each end of the standard horizontal stabilizer, to enhance directional stability. The two SCAs are under the operational control of NASA's Johnson Space Center, Houston, Texas. |
| Project Description |
470,000 pounds. The engines burn a mixture of liquid oxygen and liquid hydrogen. In orbit, the Space Shuttles circle the earth at a speed of 17,500 miles per hour with each orbit taking about 90 minutes. A Space Shuttle crew sees a sunrise or sunset every 45 minutes. When Space Shuttle flights began in April 1981, Dryden Flight Research Center, Edwards, California, was the primary landing site for the Shuttles. Now Kennedy Space Center, Florida, is the primary landing site with Dryden remaining as the principal alternate landing site., Space Shuttles are the main element of America?s Space Transportation System and are used for space research and other space applications. The shuttles are the first vehicles capable of being launched into space and returning to Earth on a routine basis. Space Shuttles are used as orbiting laboratories in which scientists and mission specialists conduct a wide variety of scientific experiments. Crews aboard shuttles place satellites in orbit, rendezvous with satellites to carry out repair missions and return them to space, and retrieve satellites and return them to Earth for refurbishment and reuse. Space Shuttles are true aerospace vehicles. They leave Earth and its atmosphere under rocket power provided by three liquid-propellant main engines with two solid-propellant boosters attached plus an external liquid-fuel tank. After their orbital missions, they streak back through the atmosphere and land like airplanes. The returning shuttles, however, land like gliders, without power and on runways. Other rockets can place heavy payloads into orbit, but, they can only be used once. Space Shuttles are designed to be continually reused. When Space Shuttles are used to transport complete scientific laboratories into space, the laboratories remain inside the payload bay throughout the mission. They are then removed after the Space Shuttle returns to Earth and can be reused on future flights. Some of these orbital laboratories, like the Spacelab, provide facilities for several specialists to conduct experiments in such fields as medicine, astronomy, and materials manufacturing. Some types of satellites deployed by Space Shuttles include those involved in environmental and resources protection, astronomy, weather forecasting, navigation, oceanographic studies, and other scientific fields. The Space Shuttles can also launch spacecraft into orbits higher than the Shuttle?s altitude limit through the use of Inertial Upper Stage (IUS) propulsion units. After release from the Space Shuttle payload bay, the IUS is ignited to carry the spacecraft into deep space. The Space Shuttles are also being used to carry elements of the International Space Station into space where they are assembled in orbit. The Space Shuttles were built by Rockwell International?s Space Transportation Systems Division, Downey, California. Rockwell?s Rocketdyne Division (now part of Boeing) builds the three main engines, and Thiokol, Brigham City, Utah, makes the solid rocket booster motors. Martin Marietta Corporation (now Lockheed Martin), New Orleans, Louisiana, makes the external tanks. Each orbiter (Space Shuttle) is 121 feet long, has a wingspan of 78 feet, and a height of 57 feet. The Space Shuttle is approximately the size of a DC-9 commercial airliner and can carry a payload of 65,000 pounds into orbit. The payload bay is 60 feet long and 15 feet in diameter. Each main engine is capable of producing a sea level thrust of 375,000 pounds and a vacuum (orbital) thrust of |
| Photo Date |
28 September 1995 |
|
Shuttle Enterprise Mated to
| Photo Description |
The Space Shuttle Enterprise, the nation's prototype space shuttle orbiter, before departing NASA's Dryden Flight Research Center, Edwards, California, at 11:00 a.m., 16 May 1983, on the first leg of its trek to the Paris Air Show at Le Bourget Airport, Paris, France. Seen here atop the huge 747 Shuttle Carrier Aircraft (SCA), the first stop for the Enterprise was Peterson AFB, Colorado Springs, Colorado. Piloting the 747 on the Europe trip were Joe Algranti, Johnson Space Center Chief Pilot, Astronaut Dick Scobee, and NASA Dryden Chief Pilot Tom McMurtry. Flight engineers for that portion of the flight were Dryden's Ray Young and Johnson Space Center's Skip Guidry. The Enterprise, named after the spacecraft of Star Trek fame, was originally carried and launched by the 747 during the Approach and Landing Tests (ALT) at Dryden Flight Research Center. |
| Project Description |
470,000 pounds. The engines burn a mixture of liquid oxygen and liquid hydrogen. In orbit, the Space Shuttles circle the earth at a speed of 17,500 miles per hour with each orbit taking about 90 minutes. A Space Shuttle crew sees a sunrise or sunset every 45 minutes. When Space Shuttle flights began in April 1981, Dryden Flight Research Center, Edwards, California, was the primary landing site for the Shuttles. Now Kennedy Space Center, Florida, is the primary landing site with Dryden remaining as the principal alternate landing site., Space Shuttles are the main element of America?s Space Transportation System and are used for space research and other space applications. The shuttles are the first vehicles capable of being launched into space and returning to Earth on a routine basis. Space Shuttles are used as orbiting laboratories in which scientists and mission specialists conduct a wide variety of scientific experiments. Crews aboard shuttles place satellites in orbit, rendezvous with satellites to carry out repair missions and return them to space, and retrieve satellites and return them to Earth for refurbishment and reuse. Space Shuttles are true aerospace vehicles. They leave Earth and its atmosphere under rocket power provided by three liquid-propellant main engines with two solid-propellant boosters attached plus an external liquid-fuel tank. After their orbital missions, they streak back through the atmosphere and land like airplanes. The returning shuttles, however, land like gliders, without power and on runways. Other rockets can place heavy payloads into orbit, but, they can only be used once. Space Shuttles are designed to be continually reused. When Space Shuttles are used to transport complete scientific laboratories into space, the laboratories remain inside the payload bay throughout the mission. They are then removed after the Space Shuttle returns to Earth and can be reused on future flights. Some of these orbital laboratories, like the Spacelab, provide facilities for several specialists to conduct experiments in such fields as medicine, astronomy, and materials manufacturing. Some types of satellites deployed by Space Shuttles include those involved in environmental and resources protection, astronomy, weather forecasting, navigation, oceanographic studies, and other scientific fields. The Space Shuttles can also launch spacecraft into orbits higher than the Shuttle?s altitude limit through the use of Inertial Upper Stage (IUS) propulsion units. After release from the Space Shuttle payload bay, the IUS is ignited to carry the spacecraft into deep space. The Space Shuttles are also being used to carry elements of the International Space Station into space where they are assembled in orbit. The Space Shuttles were built by Rockwell International?s Space Transportation Systems Division, Downey, California. Rockwell?s Rocketdyne Division (now part of Boeing) builds the three main engines, and Thiokol, Brigham City, Utah, makes the solid rocket booster motors. Martin Marietta Corporation (now Lockheed Martin), New Orleans, Louisiana, makes the external tanks. Each orbiter (Space Shuttle) is 121 feet long, has a wingspan of 78 feet, and a height of 57 feet. The Space Shuttle is approximately the size of a DC-9 commercial airliner and can carry a payload of 65,000 pounds into orbit. The payload bay is 60 feet long and 15 feet in diameter. Each main engine is capable of producing a sea level thrust of 375,000 pounds and a vacuum (orbital) thrust of |
| Photo Date |
1982 |
|
Shuttle Enterprise Mated to
| Photo Description |
The Space Shuttle Enterprise, the nation's prototype space shuttle orbiter, departed NASA's Dryden Flight Research Center, Edwards, California, at 11:00 a.m., 16 May 1983, on the first leg of its trek to the Paris Air Show at Le Bourget Airport, Paris, France. Carried by the huge 747 Shuttle Carrier Aircraft (SCA), the first stop for the Enterprise was Peterson AFB, Colorado Springs, Colorado. Piloting the 747 on the Europe trip were Joe Algranti, Johnson Space Center Chief Pilot, Astronaut Dick Scobee, and NASA Dryden Chief Pilot Tom McMurtry. Flight engineers for that portion of the flight were Dryden's Ray Young and Johnson Space Center's Skip Guidry. The Enterprise, named after the spacecraft of Star Trek fame, was originally carried and launched by the 747 during the Approach and Landing Tests (ALT) at Dryden Flight Research Center. |
| Project Description |
470,000 pounds. The engines burn a mixture of liquid oxygen and liquid hydrogen. In orbit, the Space Shuttles circle the earth at a speed of 17,500 miles per hour with each orbit taking about 90 minutes. A Space Shuttle crew sees a sunrise or sunset every 45 minutes. When Space Shuttle flights began in April 1981, Dryden Flight Research Center, Edwards, California, was the primary landing site for the Shuttles. Now Kennedy Space Center, Florida, is the primary landing site with Dryden remaining as the principal alternate landing site., Space Shuttles are the main element of America?s Space Transportation System and are used for space research and other space applications. The shuttles are the first vehicles capable of being launched into space and returning to Earth on a routine basis. Space Shuttles are used as orbiting laboratories in which scientists and mission specialists conduct a wide variety of scientific experiments. Crews aboard shuttles place satellites in orbit, rendezvous with satellites to carry out repair missions and return them to space, and retrieve satellites and return them to Earth for refurbishment and reuse. Space Shuttles are true aerospace vehicles. They leave Earth and its atmosphere under rocket power provided by three liquid-propellant main engines with two solid-propellant boosters attached plus an external liquid-fuel tank. After their orbital missions, they streak back through the atmosphere and land like airplanes. The returning shuttles, however, land like gliders, without power and on runways. Other rockets can place heavy payloads into orbit, but, they can only be used once. Space Shuttles are designed to be continually reused. When Space Shuttles are used to transport complete scientific laboratories into space, the laboratories remain inside the payload bay throughout the mission. They are then removed after the Space Shuttle returns to Earth and can be reused on future flights. Some of these orbital laboratories, like the Spacelab, provide facilities for several specialists to conduct experiments in such fields as medicine, astronomy, and materials manufacturing. Some types of satellites deployed by Space Shuttles include those involved in environmental and resources protection, astronomy, weather forecasting, navigation, oceanographic studies, and other scientific fields. The Space Shuttles can also launch spacecraft into orbits higher than the Shuttle?s altitude limit through the use of Inertial Upper Stage (IUS) propulsion units. After release from the Space Shuttle payload bay, the IUS is ignited to carry the spacecraft into deep space. The Space Shuttles are also being used to carry elements of the International Space Station into space where they are assembled in orbit. The Space Shuttles were built by Rockwell International?s Space Transportation Systems Division, Downey, California. Rockwell?s Rocketdyne Division (now part of Boeing) builds the three main engines, and Thiokol, Brigham City, Utah, makes the solid rocket booster motors. Martin Marietta Corporation (now Lockheed Martin), New Orleans, Louisiana, makes the external tanks. Each orbiter (Space Shuttle) is 121 feet long, has a wingspan of 78 feet, and a height of 57 feet. The Space Shuttle is approximately the size of a DC-9 commercial airliner and can carry a payload of 65,000 pounds into orbit. The payload bay is 60 feet long and 15 feet in diameter. Each main engine is capable of producing a sea level thrust of 375,000 pounds and a vacuum (orbital) thrust of |
| Photo Date |
1983 |
|
Fluid-Gas Mixture in Space
| Name of Image |
Fluid-Gas Mixture in Space |
| Date of Image |
1985-08-08 |
| Full Description |
The lack of normal convection in microgravity is demonstrated by a carbonated soft drink floating in the middeck of the Space Shuttle. While the droplet is oscillating slightly and starting to assume a spherical shape, it is filled with carbon dioxide bubbles in a range of sizes. On Earth, the bubbles would quickly foat up to form a head. In space, they are suspended. They may drift with time and eventually the surface tension between individual bubbles breaks, allowing larger bubbles to form. This image was taken during STS-51F mission (Spacelab 2) which carried test models of dispensers from two pupular soft drink manufacturers. Photo credit: NASA/Johnson Space Center (JSC) |
|
STS-99 Crew Portrait
| Name of Image |
STS-99 Crew Portrait |
| Date of Image |
1999-06-01 |
| Full Description |
An international crew assigned to STS-99 takes a break from training to pose for the traditional crew portrait at NASA's Johnson Space Center (JSC). In front are international astronauts and mission specialists Mamoru Mohri, representing Japan's Space Agency (NASDA), and Gerhard P. J. Thiele of Germany, representing the European Space Agency (ESA). In back are astronauts Janice Voss, mission specialist, Kevin R. Kregel, mission commander, Dominic L. Gorie, pilot, and Janet L. Kavandi, mission specialist. STS-99 was a Shuttle Radar Topography Mission (SRTM), the most ambitious Earth mapping mission to date. Two radar anternas, one located in the Shuttle bay and the other located on the end of a 60-meter deployable mast, was used during the mission to map Earth's features. The goal was to provide a 3-dimensional topographic map of the world's surface up to the Arctic and Antarctic Circles. Launched aboard the Space Shuttle Endeavor on February 11, 2000, the 11-day mission provided enough information to fill more than 20,000 CDs. |
|
Protein Crystal Growth Sampl
| Name of Image |
Protein Crystal Growth Samples Placed Aboard Mir Space Station |
| Date of Image |
1996-03-24 |
| Full Description |
Astronaut Michael Clifford places a liquid nitrogen Dewar containing frozen protein solutions aboard Russia's space station Mir during a visit by the Space Shuttle (STS-76). The protein samples were flash-frozen on Earth and will be allowed to thaw and crystallize in the microgravity environment on Mir Space Station. A later crew will return the Dewar to Earth for sample analysis. Dr. Alexander McPherson of the University of California at Riverside is the principal investigator. Photo credit: NASA/Johnson Space Center. |
|
Protein Crystal Growth Sampl
| Name of Image |
Protein Crystal Growth Samples Placed Aboard Mir Space Station |
| Date of Image |
1996-09-20 |
| Full Description |
Astronaut Tom Akers places a liquid nitrogen Dewar containing frozen protein solutions aboard Russia's space Station Mir during a visit by the Space Shuttle (STS-79). The protein samples were flash-frozen on Earth and will be allowed to thaw and crystallize in the microgravity environment on Mir Space Station. A later crew will return the Dewar to Earth for sample analysis. Dr. Alexander McPherson of the University of California at Riverside is the principal investigator. Photo credit: NASA/Johnson Space Center. |
|
Colon tumor cells grown in N
| Name of Image |
Colon tumor cells grown in NASA Bioreactor |
| Date of Image |
2001-05-15 |
| Full Description |
These photos compare the results of colon carcinoma cells grown in a NASA Bioreactor flown on the STS-70 Space Shuttle in 1995 flight and ground control experiments. The cells grown in microgravity (left) have aggregated to form masses that are larger and more similar to tissue found in the body than the cells cultured on the ground (right). The principal investigator is Milburn Jessup of the University of Texas M. D. Anderson Cancer Center. The NASA Bioreactor provides a low turbulence culture environment which promotes the formation of large, three-dimensional cell clusters. Due to their high level of cellular organization and specialization, samples constructed in the bioreactor more closely resemble the original tumor or tissue found in the body. NASA-sponsored bioreactor research has been instrumental in helping scientists to better understand normal and cancerous tissue development. In cooperation with the medical community, the bioreactor design is being used to prepare better models of human colon, prostate, breast and ovarian tumors. Cartilage, bone marrow, heart muscle, skeletal muscle, pancreatic islet cells, liver and kidney are just a few of the normal tissues being cultured in rotating bioreactors by investigators. Cell constructs grown in a rotating bioreactor on Earth (left) eventually become too large to stay suspended in the nutrient media. In the microgravity of orbit, the cells stay suspended. Rotation then is needed for gentle stirring to replenish the media around the cells. The work is sponsored by NASA's Office of Biological and Physical Research. The bioreactor is managed by the Biotechnology Cell Science Program at NASA's Johnson Space Center (JSC). Credit: NASA and University of Texas M. D. Anderson Cancer Center. |
|
Space Station Systems Analys
| Name of Image |
Space Station Systems Analysis Study (SSSAS) |
| Date of Image |
1977-01-01 |
| Full Description |
The Marshall Space Flight Center (MSFC) and the Johnson Space Center (JSC) were each awarded 16-month contracts in April 1976 for the Space Station Systems Analysis Study (SSSAS). Grumman Aerospace Corporation was MSFC's contractor and McDornell Douglas Aerospace Company was JSC's contractor. The goal of this study was to formulate plans for a permanent operational base and laboratory facility in Earth orbit in addition to developing a space construction base design for implementing the program. An expended Space Shuttle external tank was to be the central core platform of the base, and additional pressurized modules could be added to provide laboratory facilities. This artist's concept depicts a space construction base design for implementing the SSSAS. |
|
Mission STS-113 Crew
| Name of Image |
Mission STS-113 Crew |
| Date of Image |
2002-03-25 |
| Full Description |
Pictured is the crew for the Shuttle Endeavor STS-113 mission snapped during a training session in the Space Vehicle Mockup Facility at the Johnson Space Center. From the left are Astronauts James D. Wetherbee, STS-113 mission commander, Christopher J. (Gus) Loria, pilot, Michael E. Lopez-Alegria and John B. Herrington, mission specialists, Kerneth D. Bowersox, Expedition Six mission commander, Cosmonaut Nikloai M. Budarin and astronaut Donald A. Thomas, Expedition Six Flight Engineers. The 16th American assembly flight and 112th overall American flight to the International Space Station (ISS), STS-113 mission objectives included the delivery of the Expedition Six Crew to the ISS, the return of Expedition Five back to Earth, and the installation and activation of the Port 1 Integrated Truss Assembly (P1). The first major component installed on the left side of the Station, the P1 truss provides an additional three External Thermal Control System radiators. Weighing in at 27,506 pounds, the P1 truss is 45 feet (13.7 meters) long, 15 feet (4.6 meters) wide, and 13 feet (4 meters) high. Three space walks, aided by the use of the Robotic Manipulator Systems of both the Shuttle and the Station, were performed in the installation of P1. Also, more than 2,500 pounds (1,134 kilograms) of cargo were transferred between the Shuttle and Station. The Space Shuttle Orbiter Endeavor launched on November 23, 2002 from Kennedy's launch pad 39A and returned 11 days later on December 4, 2002. |
|
Onboard Photo: Astronauts Us
| Name of Image |
Onboard Photo: Astronauts Use Shuttle Amateur Radio Experiment II (SAREX-II) |
| Date of Image |
1993-04-08 |
| Full Description |
Space Shuttle Discovery (STS-56) onboard photo of Pilot Stephen S. Oswald (wearing a headset) uses the Shuttle Amateur Radio Experiment II (SAREX-II) while sitting at the pilot's station on the forward flight deck. Oswald smiled from behind the microphone as he talks to amateur radio operators on Earth via the SAREX equipment. SAREX cables and the interface module freefloat in front of Oswald. The anterna located in the forward flight deck window is visible in the background. SAREX was established by NASA, the American Radio League/Amateur Radio Satellite Corporation and the Johnson Space Center (JSC) Amateur Radio Club to encourage public participation in the space program through a program to demonstrate the effectiveness of conducting short-wave radio transmissions between the Shuttle and ground-based radio operators at low-cost ground stations with amateur and digital techniques. |
|
In-flight Video Captured by
| Name of Image |
In-flight Video Captured by External Tank Camera System |
| Date of Image |
2005-07-26 |
| Full Description |
In this July 26, 2005 video, Earth slowly fades into the background as the STS-114 Space Shuttle Discovery climbs into space until the External Tank (ET) separates from the orbiter. An External Tank ET Camera System featuring a Sony XC-999 model camera provided never before seen footage of the launch and tank separation. The camera was installed in the ET LO2 Feedline Fairing. From this position, the camera had a 40% field of view with a 3.5 mm lens. The field of view showed some of the Bipod area, a portion of the LH2 tank and Intertank flange area, and some of the bottom of the shuttle orbiter. Contained in an electronic box, the battery pack and transmitter were mounted on top of the Solid Rocker Booster (SRB) crossbeam inside the ET. The battery pack included 20 Nickel-Metal Hydride batteries (similar to cordless phone battery packs) totaling 28 volts DC and could supply about 70 minutes of video. Located 95 degrees apart on the exterior of the Intertank opposite orbiter side, there were 2 blade S-Band antennas about 2 1/2 inches long that transmitted a 10 watt signal to the ground stations. The camera turned on approximately 10 minutes prior to launch and operated for 15 minutes following liftoff. The complete camera system weighs about 32 pounds. Marshall Space Flight Center (MSFC), Johnson Space Center (JSC), Goddard Space Flight Center (GSFC), and Kennedy Space Center (KSC) participated in the design, development, and testing of the ET camera system. |
|
STS-95 Crew Portrait
| Name of Image |
STS-95 Crew Portrait |
| Date of Image |
1997-12-14 |
| Full Description |
Five astronauts based at the Johnson Space Center (JSC) and two payload specialists comprising the STS-95 mission take a break from their training schedule to pose for the STS-95 preflight portrait. Seated (left to right) are Steven W. Lindsey, pilot, and Curtis L. Brown, commander. Standing (left to right) are Scott E. Parazynski, mission specialist, Stephen K. Robinson, mission specialist, Chiaki Mukai (NASDA), payload specialist, Pedro Duque (ESA), mission specialist, and John H. Glenn, payload specialist. Glenn was a U.S. Senator and the first American to orbit the Earth in Friendship 7 in February of 1962. The seven launched into Earth orbit aboard the Space Shuttle Discovery on October 29, 1998 at 2:19:34 pm (EST). The primary payload was SPACEHAB, in which many experiments were carried out. |
|
Aurora from the Space Shuttl
| Title |
Aurora from the Space Shuttle |
| Description |
Astronauts aboard the STS-97 Space Shuttle mission in December observed and photographed the northern lights after undocking from the International Space Station. This image was taken on December 11, 2000. At the time, the Shuttle was just east of Newfoundland at 49.7N 51.6 W, at an altitude of 362 km. The image view is to the north (Polaris, the North Star, is visible), and shows two separate atmospheric optical phenomena. The faint, thin greenish band stretching across and above the horizon is airglow, radiation emitted by the atmosphere from a layer about 30 km thick and about 100 km altitude. The predominant emission in airglow is the green 5577 Angstrom wavelength emission from oxygen atoms. Airglow is always and everywhere present in the atmosphere, it results from the recombination of molecules that have been broken apart by solar radiation during the day. But the phenomenon is so faint that it can only be seen at night by looking "edge on" at the emission layer, such as the view astronauts have in orbit. Astronaut Tom Jones gives a nice astronaut perspective of airglow on the web at http://neurolab.jsc.nasa.gov/jones.htm [ http://earthobservatory.nasa.gov/cgi-bin/redirect?http://neurolab.jsc.nasa.gov/jones.htm ] The other phenomenon in the photo (the green blob to the left of center) is the aurora. Green aurora occur from about 100 km to 250 km altitude only in the auroral zones at polar latitudes. They are also caused by the emission of 5577 Angstrom wavelength light from oxygen atoms that have been raised to a higher energy level (excited) by collisions with energetic electrons pouring down from the Earth's magnetosphere. The light is emitted when the atoms return to their original unexcited state. Image STS097-354-36 [ http://eol.jsc.nasa.gov/scripts/sseop/photo.pl?mission=STS097&roll=354&frame=36 ] was provided by the Earth Science and Image Analysis Laboratory, Johnson Space Center. Additional images taken by astronauts can be viewed at NASA-JSC's Gateway to Astronaut Photography of Earth at http://eol.jsc.nasa.gov [ http://earthobservatory.nasa.gov/cgi-bin/redirect?http://eol.jsc.nasa.gov/ ]. |
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Thunderstorms over Brazil
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Thunderstorms over Brazil |
| Description |
This photograph, acquired in February 1984 by an astronaut aboard the space shuttle, shows a series of mature thunderstorms located near the Parana River in southern Brazil. With abundant warm temperatures and moisture-laden air in this part of Brazil, large thunderstorms are commonplace. A number of overshooting tops and anvil clouds are visible at the tops of the clouds. Storms of this magnitude can drop large amounts of rainfall in a short period of time, causing flash floods. However, a NASA-funded researcher has discovered that tiny airborne particles of pollution may modify developing thunderclouds by increasing the quantity and reducing the size of the ice crystals within them. These modifications may affect the clouds? impact on the Earth?s ?radiation budget,? or the amount of radiation that enters and leaves our planet. Steven Sherwood, a professor at Yale University, found that airborne aerosols reduce the size of ice crystals in thunderclouds and may reduce precipitation as well. Using several satellites and instruments including NASA?s Total Ozone Mapping Spectrometer (TOMS) and NASA?s Tropical Rainfall Measuring Mission (TRMM) satellite, Sherwood observed how airborne pollution particles (aerosols) affect large thunderstorms, or cumulonimbus clouds in the tropics. Common aerosols include mineral dust, smoke, and sulfates. An increased number of these particles create a larger number of smaller ice crystals in cumulonimbus clouds. As a result of their smaller size, the ice crystals evaporate from a solid state directly into a gas, instead of falling as rain. Sherwood noted that this effect is more prevalent over land than open ocean areas. Previous research by Daniel Rosenfeld of Hebrew University revealed that aerosols and pollution reduced rainfall in shallow cumulus clouds of liquid water, which do not have the capability to produce as much rainfall. Sherwood expanded on that research by looking at cumulonimbus clouds with more ice particles. Studies have also proven that ice particles are smaller in the upper reaches of thunderclouds when there is more pollution and when the rising air in the clouds (convection) is stronger. Aerosols seem to have the most influence on seasonal and longer timescales such as during the warmer months when plants and undergrowth are burned to clear fields. Over areas where biomass burning occurs, such as South America, aerosols have been found to reduce the diameter of ice crystals in the clouds by as much as 20 percent. Areas over deserts, such as Africa's Sahel Region where dust is a primary aerosol, there was a 10 percent decrease in the diameter of ice crystals in cumulonimbus clouds. Aerosol particles are necessary for clouds to form, and it has been suspected that clouds might be altered by large concentrations of them. By looking at ten years of aerosol data and statistically analyzing many thunderclouds, Sherwood was able to confirm that they were affected. Sherwood found that ice, crystals are smaller in clouds over continents than oceans, which could be attributed to the amount of pollution generated over land. The highest values occur widely over Northern Africa, where desert dust and smoke from agricultural burning occur. Intermediate values prevail over much of Asia, through the Indonesia region and into the south Pacific. The largest ice crystal sizes were found over the eastern Pacific and southern Indian Oceans. Sherwood?s article, ?Aerosols and Ice Particle Size in Tropical Cumulonimbus,? appears in the May 1, 2002, issue of the American Meteorological Society "Journal of Climate". This work was performed under the NASA Earth Observing System/Interdisciplinary Science (IDS) program under the Earth Science Enterprise (ESE). Image STS41B-41-2347 [ http://earth.jsc.nasa.gov/photoinfo.cgi?PHOTO=STS41B-41-2347 ] was provided by the Earth Sciences and Image Analysis Laboratory [ http://earthobservatory.nasa.gov/cgi-bin/redirect?http://eol.jsc.nasa.gov/ ] at Johnson Space Center. Additional images taken by astronauts and cosmonauts can be viewed at the NASA-JSC Gateway to Astronaut Photography of Earth [ http://earthobservatory.nasa.gov/cgi-bin/redirect?http://eol.jsc.nasa.gov/sseop/ ] |
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