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Space Shuttle Orbiter and Earth of Johnson Space Center (JSC) and California
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Sally Ride, First U.S. Woman
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| 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 |
|
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 |
|
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 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 |
|
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. |
|
Shuttle Carrier Aircraft (SC
…
| Title |
Shuttle Carrier Aircraft (SCA) Fleet 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. 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 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. |
| Date |
09.28.1995 |
|
Shuttle Enterprise Mated to
…
| Title |
Shuttle Enterprise Mated to 747 SCA in Flight |
| Description |
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 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., 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. 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 |
| Date |
01.01.1983 |
|
Shuttle Enterprise Mated to
…
| Title |
Shuttle Enterprise Mated to 747 SCA on Ramp |
| 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. 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 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. |
| Date |
01.01.1982 |
|
The five crew members of the
…
| Title |
The five crew members of the Space Shuttle Atlantis on the STS-98 mission depart NASA Dryden to retu |
| Description |
The five crew members of the Space Shuttle Atlantis on the STS-98 mission depart NASA Dryden to return to the Johnson Space Center at Houston. They briefly extended greetings to Dryden staff members on the ramp area behind Dryden's Main Building at a crew ceremony on February 21, 2001. Space Shuttle Atlantis landed at 12:33 p.m. February 20, 2001, on the runway at Edwards Air Force Base, California, where NASA's Dryden Flight Research Center is located. The mission, which began February 7, logged 5.3 million miles as the shuttle orbited earth while delivering the Destiny science laboratory to the International Space Station. Inclement weather conditions in Florida prompted the decision to land Atlantis at Edwards. The last time a space shuttle landed at Edwards was Oct. 24, 2000. |
| Date |
02.21.2001 |
|
X-38 Drop Model: Glides to E
…
| Title |
X-38 Drop Model: Glides to Earth After Being Dropped from a Cessna |
| 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. 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. It's 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, Dryden's 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. |
| Date |
01.01.1995 |
|
X-38 Drop Model: Testing Par
…
| Title |
X-38 Drop Model: Testing Parafoil Landing System during Drop Tests |
| 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. 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. It's 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, Dryden's 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. |
| Date |
01.01.1995 |
|
X-38 Drop Model: Used to Tes
…
| Title |
X-38 Drop Model: Used to Test Parafoil Landing System during Drop Tests |
| 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. 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. It's 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, Dryden's 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. |
| Date |
01.01.1995 |
|
X-38: Artist Concept of Re-E
…
| Title |
X-38: Artist Concept of Re-Entering Earth's Atmosphere |
| 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 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. It's 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, Dryden's 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. |
| Date |
01.01.1997 |
|
Southern tip of Sumatra, Ind
…
PIA00953
Sol (our sun)
Electronic Still Camera
| Title |
Southern tip of Sumatra, Indonesia |
| Original Caption Released with Image |
Middle school students across the country photographed the fires and smoke over southern Sumatra from a camera aboard the Space Shuttle Atlantis Saturday, September 27. A joint effort between 23 of the 52 schools participating in this mission, the KidSat camera was used to image a 140 km wide, 1950 km long strip that starts in the northwest (5.24 degrees N, 97.11 degrees E), and follows the Pegunungan Barisan range across the equator to the southern tip of Sumatra (7.44S, 106.1E). [MET 00215343 - 00215750]. Smoldering underground fires have raged uncontrolled for the past few weeks in Southeast Asia. Originally set to clear land for agriculture, the fires are usually extinguished by the annual monsoon rains. However, this year, the rains had not come due to El Niño which produces dry conditions in the Indonesia region. Due to the lack of trade winds, the seasonal warm waters in the eastern Pacific have spread over to South America. Consequently, the water temperature in Indonesia has dropped significantly. This decrease in temperature has not produced enough warm water vapor to produce the normal seasonal showers that usually encompass the area. The fire has now been blamed for two fatal accidents and countless health hazards. At one point, the pollution index of the region reached 839. To put a relative point to this number, a pollution index of 300 is a equivalent of smoking 20 cigarettes a day. The smoke, during one time, blanketed an area that was larger than the continental United States. Currently, the fire's rage has been quelled by winds and rain which have lifted the smog and dampened the fires. However it is estimated that 100,000 fire fighters are needed to stop the fire. This KidSat image (MET 00215624) of the southern tip of Sumatra was captured on September 27, 1997 during Space Shuttle flight STS-86. It is centered at 3.0 degrees S, 102.9 degrees E and is 140 km wide and 205 km long. A clear view is visible of the southern tip of Sumatra with the volcanoes that make up the backbone of the island appearing darker than the surrounding land. Travelling northwest, the first smoke plumes are visible in the rain forests east of the mountains where land is being cleared for palm plantations. The prevailing winds are from the southeast and are blowing most of the smoke to the northwest of this image (see images 00215637/PIA00954 and 00215701/PIA00955). The KidSat camera that photographed these fires is mounted in the overhead starboard window of the Shuttle Atlantis and operates before and after docking with Mir when the Shuttle's windows face the Earth. Students on the ground are linked to the camera through the Internet and a series of satellites. High school and undergraduate students work in collaboration with scientists and engineers to develop and operate the KidSat systems. Curriculum developed by The Johns Hopkins University Institute for the Academic Advancement of Youth is used in the middle school classrooms to encourage, scientific inquiry based on the images. The photographs from the three missions of the KidSat pilot program can be accessed at the following URL: http://www.jpl.nasa.gov/kidsat The KidSat program was developed by the Jet Propulsion Laboratory, The Johns Hopkins University Institute for the Academic Advancement of Youth, and The University of California, San Diego, with support from NASA's Johnson Space Center. The project is supported by NASA's Office of Human Resources and Education with support from NASA's Offices of Mission to Planet Earth, Space Flight, and Space Science. JPL is a division of the California Institute of Technology (Caltech). |
|
Southern Sumatra, Indonesia
PIA00954
Sol (our sun)
Electronic Still Camera
| Title |
Southern Sumatra, Indonesia |
| Original Caption Released with Image |
Middle school students across the country photographed the fires and smoke over southern Sumatra from a camera aboard the Space Shuttle Atlantis September 27. A joint effort between 23 of the 52 schools participating in this mission, the KidSat camera was used to image a 140 km wide, 1950 km long strip that starts in the northwest (5.24 degrees N, 97.11 degrees E), and follows the Pegunungan Barisan range across the equator to the southern tip of Sumatra (7.44S, 106.1E). [MET 00215343 - 00215750]. Smoldering underground fires have raged uncontrolled for the past few weeks in Southeast Asia. Originally set to clear land for agriculture, the fires are usually extinguished by the annual monsoon rains. However, this year, the rains had not come due to El Niño which produces dry conditions in the Indonesia region. Due to the lack of trade winds, the seasonal warm waters in the eastern Pacific have spread over to South America. Consequently, the water temperature in Indonesia has dropped significantly. This decrease in temperature has not produced enough warm water vapor to produce the normal seasonal showers that usually encompass the area. The fire has now been blamed for two fatal accidents and countless health hazards. At one point, the pollution index of the region reached 839. To put a relative point to this number, a pollution index of 300 is a equivalent of smoking 20 cigarettes a day. The smoke, during one time, blanketed an area that was larger than the continental United States. Currently, the fire's rage has been quelled by winds and rain which have lifted the smog and dampened the fires. However it is estimated that 100,000 fire fighters are needed to stop the fire. This KidSat image (MET 00215637) of the southern region of Sumatra was captured on September 27, 1997 during the Shuttle flight STS-86. It is centered at 3.7 degrees S 103.4 degrees E and is 140 km wide and 205 km long. The smoke plumes appear in the rain forests east of the mountains where land is being cleared for palm plantations, the plumes indicate a prevailing wind to the northwest and rise above the continuous layer of smoke. Within a short distance, the region becomes completely blanketed in smoke with only the peaks of the volcanoes rising above the gray haze layer. The KidSat camera that photographed these fires is mounted in the overhead starboard window of the Shuttle Atlantis and operates before and after docking with Mir when the Shuttle's windows face the Earth. Students on the ground are linked to the camera through the Internet and a series of satellites. High school and undergraduate students work in collaboration with scientists and engineers to develop and operate the KidSat systems. Curriculum developed by The Johns Hopkins University Institute for the Academic Advancement of Youth is used in the middle school classrooms to encourage scientific inquiry based on the images. The photographs from the three missions of the KidSat pilot program can be, accessed at the following URL: http://www.jpl.nasa.gov/kidsat The KidSat program was developed by the Jet Propulsion Laboratory, The Johns Hopkins University Institute for the Academic Advancement of Youth, and The University of California, San Diego, with support from NASA's Johnson Space Center. The project is supported by NASA's Office of Human Resources and Education with support from NASA's Offices of Mission to Planet Earth, Space Flight, and Space Science. JPL is a division of the California Institute of Technology (Caltech). |
|
Sumatra, Indonesia
PIA00955
Sol (our sun)
Electronic Still Camera
| Title |
Sumatra, Indonesia |
| Original Caption Released with Image |
Middle school students across the country photographed the fires and smoke over southern Sumatra from a camera aboard the Space Shuttle Atlantis on September 27. A joint effort between 23 of the 52 schools participating in this mission, the KidSat camera was used to image a 140 km wide, 1950 km long strip that starts in the northwest (5.24 degrees N, 97.11 degrees E), and follows the Pegunungan Barisan range across the equator to the southern tip of Sumatra (7.44S, 106.1E) [MET 00215343 - 00215750]. Smoldering underground fires have raged uncontrolled for the past few weeks in Southeast Asia. Originally set to clear land for agriculture, the fires are usually extinguished by the annual monsoon rains. However, this year, the rains had not come due to El Niño which produces dry conditions in the Indonesia region. Due to the lack of trade winds, the seasonal warm waters in the eastern Pacific have spread over to South America. Consequently, the water temperature in Indonesia has dropped significantly. This decrease in temperature has not produced enough warm water vapor to produce the normal seasonal showers that usually encompass the area. The fire has now been blamed for two fatal accidents and countless health hazards. At one point, the pollution index of the region reached 839. To put a relative point to this number, a pollution index of 300 is a equivalent of smoking 20 cigarettes a day. The smoke, during one time, blanketed an area that was larger than the continental United States. Currently, the fire's rage has been quelled by winds and rain which have lifted the smog and dampened the fires. However it is estimated that 100,000 fire fighters are needed to stop the fire. This KidSat image (MET 00215701) of Sumatra was captured on September 27, 1997 during the Shuttle flight STS-86. It is centered at 4.9 degrees S 104.3 degrees E and is 140 km wide and 205 km long. The smoke plumes appear in the rain forests east of the mountains where land is being cleared for palm plantations, the plumes indicate a prevailing wind to the northwest and rise above the continuous layer of smoke. For a geographic reference, see image #00215701_img_map. The KidSat camera that photographed these fires is mounted in the overhead starboard window of the Shuttle Atlantis and operates before and after docking with Mir when the Shuttle's windows face the Earth. Students on the ground are linked to the camera through the Internet and a series of satellites. High school and undergraduate students work in collaboration with scientists and engineers to develop and operate the KidSat systems. Curriculum developed by The Johns Hopkins University Institute for the Academic Advancement of Youth is used in the middle school classrooms to encourage scientific inquiry based on the images. The photographs from the three missions of the KidSat pilot program can be accessed at the following URL: http://www.jpl.nasa.gov/kidsat The KidSat program was developed by the Jet, Propulsion Laboratory, The Johns Hopkins University Institute for the Academic Advancement of Youth, and The University of California, San Diego, with support from NASA's Johnson Space Center. The project is supported by NASA's Office of Human Resources and Education with support from NASA's Offices of Mission to Planet Earth, Space Flight, and Space Science. JPL is a division of the California Institute of Technology (Caltech). |
|
Kidsat image of Sumatra, Ind
…
PIA00956
Sol (our sun)
Electronic Still Camera
| Title |
Kidsat image of Sumatra, Indonesia & map |
| Original Caption Released with Image |
Middle school students across the country photographed the fires and smoke over southern Sumatra from a camera aboard the Space Shuttle Atlantis last Friday, September 26. A joint effort between 23 of the 52 schools participating in this mission, the KidSat camera was used to image a 140 km wide, 1950 km long strip that starts in the northwest (5.24 degrees N, 97.11 degrees E), and follows the Pegunungan Barisan range across the equator to the southern tip of Sumatra (7.44S, 106.1E) [MET 00215343 - 00215750]. Smoldering underground fires have raged uncontrolled for the past few weeks in Southeast Asia. Originally set to clear land for agriculture, the fires are usually extinguished by the annual monsoon rains. However, this year, the rains had not come due to El Niño which produces dry conditions in the Indonesia region. Due to the lack of trade winds, the seasonal warm waters in the eastern Pacific have spread over to South America. Consequently, the water temperature in Indonesia has dropped significantly. This decrease in temperature has not produced enough warm water vapor to produce the normal seasonal showers that usually encompass the area. The fire has now been blamed for two fatal accidents and countless health hazards. At one point, the pollution index of the region reached 839. To put a relative point to this number, a pollution index of 300 is a equivalent of smoking 20 cigarettes a day. The smoke, during one time, blanketed an area that was larger than the continental United States. Currently, the fire's rage has been quelled by winds and rain which have lifted the smog and dampened the fires. However it is estimated that 100,000 fire fighters are needed to stop the fire. This KidSat image (MET 00215701) of Sumatra was captured on September 27, 1997 during the Shuttle flight STS-86. It is centered at 4.9 degrees S 104.3 degrees E and is 140 km wide and 205 km long. The smoke plumes appear in the rain forests east of the mountains where land is being cleared for palm plantations, the plumes indicate a prevailing wind to the northwest and rise above the continuous layer of smoke. The image is shown on a map of the region for geographic reference. Smoke from the fires completely covers the land. The KidSat camera that photographed these fires is mounted in the overhead starboard window of the Shuttle Atlantis and operates before and after docking with Mir when the Shuttle's windows face the Earth. Students on the ground are linked to the camera through the Internet and a series of satellites. High school and undergraduate students work in collaboration with scientists and engineers to develop and operate the KidSat systems. Curriculum developed by The Johns Hopkins University Institute for the Academic Advancement of Youth is used in the middle school classrooms to encourage scientific inquiry based on the images. The photographs from the three missions of the KidSat pilot program can be accessed at the following URL:, http://www.jpl.nasa.gov/kidsat The KidSat program was developed by the Jet Propulsion Laboratory, The Johns Hopkins University Institute for the Academic Advancement of Youth, and The University of California, San Diego, with support from NASA's Johnson Space Center. The project is supported by NASA's Office of Human Resources and Education with support from NASA's Offices of Mission to Planet Earth, Space Flight, and Space Science. JPL is a division of the California Institute of Technology (Caltech). |
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Smoke over Lake Toba, Indone
…
PIA00951
Sol (our sun)
Electronic Still Camera
| Title |
Smoke over Lake Toba, Indonesia |
| Original Caption Released with Image |
As the Space Shuttle Atlantis flew over the Indonesian archipelago on Saturday, September 27, middle school students across the country used the Kidsat camera to photograph the fires and smoke that blanket the island of Sumatra . A joint effort between 23 of the 52 schools participating in this mission, the KidSat camera was used to image a 140 km wide, 1950 km long strip that starts in the northwest (5.24 degrees N, 97.11 degrees E), and follows the Pegunungan Barisan range across the equator to the southern tip of Sumatra (7.44S, 106.1E). [Mission Elapsed Time (MET) 00215343 - 00215750] Smoldering underground fires have raged uncontrolled for the past few weeks in Southeast Asia. Originally set to clear land for agriculture, the fires are usually extinguished by the annual monsoon rains. However, this year, the rains had not come due to El Niño which produces dry conditions in the Indonesia region. Due to the lack of trade winds, the seasonal warm waters in the eastern Pacific have spread over to South America. Consequently, the water temperature in Indonesia has dropped significantly. This decrease in temperature has not produced enough warm water vapor to produce the normal seasonal showers that usually encompass the area. The effects of the fires have been astronomical. So far the fire has been blamed for two fatal accidents and countless health hazards. At one point, the pollution index of the region reached 839. To put a relative point to this number, a pollution index of 300 is a equivalent of smoking 20 cigarettes a day. The smoke, during one time, blanketed an area that was larger than the continental United States. Currently, the fire's rage has been quelled by winds and rain which have lifted the smog and dampened the fires. However it is estimated that 100,000 fire fighters are needed to stop the fire. This KidSat image (MET 00215424) of the northern regions of Sumatra was captured on September 27, 1997 during the Shuttle flight STS-86. It is centered at 3.1 degrees S 98.6 degrees E and is 140 km wide and 205 km long. Smoke from the fires completely covers the land. The only indication of surface features is from the clouds that rise above the smoke over Danau Toba, the largest lake in Sumatra. The KidSat camera that photographed these fires is mounted in the overhead starboard window of the Shuttle Atlantis and operates before and after docking with Mir when the Shuttle's windows face the Earth. Students on the ground are linked to the camera through the Internet and a series of satellites. Commands are sent from middle schools through a Mission Operations Gateway at the University of California, San Diego, to a Thinkpad on the Shuttle flight deck. Images are transmitted back to the Jet Propulsion Laboratory where they are immediately placed on the Internet for the KidSat students and the rest of the world to view and use. High school and undergraduate students work in collaboration with scientists and engineers to develop and, operate the KidSat systems. Curriculum developed by The Johns Hopkins University Institute for the Academic Advancement of Youth is used in the middle school classrooms to encourage scientific inquiry based on the images. The photographs from the three missions of the KidSat pilot program can be accessed at the following URL: http://www.jpl.nasa.gov/kidsat The KidSat program was developed by the Jet Propulsion Laboratory, The Johns Hopkins University Institute for the Academic Advancement of Youth, and The University of California, San Diego, with support from NASA's Johnson Space Center. The project is supported by NASA's Office of Human Resources and Education with support from NASA's Offices of Mission to Planet Earth, Space Flight, and Space Science. JPL is a division of the California Institute of Technology (Caltech). |
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Map of northern Sumatra, Ind
…
PIA00952
Sol (our sun)
Electronic Still Camera
| Title |
Map of northern Sumatra, Indonesia |
| Original Caption Released with Image |
This map corresponds to KidSat image MET 00215424 of the northern regions of Sumatra that was captured on September 27, 1997 during the Shuttle flight STS-86. It is centered at 3.1 degrees S 98.6 degrees E. As the Space Shuttle Atlantis flew over the Indonesian archipelago last Friday, middle school students across the country photographed the fires and smoke that blanket Sumatra. A joint effort between 23 of the 52 schools participating in this mission, the KidSat camera was used to image a 140 km wide, 1950 km long strip that starts in the northwest (5.24 degrees N, 97.11 degrees E), and follows the Pegunungan Barisan range across the equator to the southern tip of Sumatra (7.44S, 106.1E). Smoldering underground fires have raged uncontrolled for the past few weeks in Southeast Asia. Originally set to clear land for agriculture, the fires are usually extinguished by the annual monsoon rains. However, this year, the rains had not come due to El Niño which produces dry conditions in the Indonesia region. The KidSat camera that photographed these fires is mounted in the overhead starboard window of the Shuttle Atlantis and operates before and after docking with Mir when the Shuttle's windows face the Earth. Students on the ground are linked to the camera through the Internet and a series of satellites. Commands are sent from middle schools through a Mission Operations Gateway at the University of California, San Diego, to a Thinkpad on the Shuttle flight deck. Images are transmitted back to the Jet Propulsion Laboratory where they are immediately placed on the Internet for the KidSat students and the rest of the world to view and use. High school and undergraduate students work in collaboration with scientists and engineers to develop and operate the KidSat systems. Curriculum developed by The Johns Hopkins University Institute for the Academic Advancement of Youth is used in the middle school classrooms to encourage scientific inquiry based on the images. The photographs from the three missions of the KidSat pilot program can be accessed at the following URL: http://www.jpl.nasa.gov/kidsat The KidSat program was developed by the Jet Propulsion Laboratory, The Johns Hopkins University Institute for the Academic Advancement of Youth, and The University of California, San Diego, with support from NASA's Johnson Space Center. The project is supported by NASA's Office of Human Resources and Education with support from NASA's Offices of Mission to Planet Earth, Space Flight, and Space Science. JPL is a division of the California Institute of Technology (Caltech). |
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Mosaic image of fires in Ind
…
PIA00950
Sol (our sun)
Electronic Still Camera
| Title |
Mosaic image of fires in Indonesia |
| Original Caption Released with Image |
Middle school students across the country photographed the fires and smoke over southern Sumatra from a camera aboard the Space Shuttle Atlantis September 27. A joint effort between 23 of the 52 schools participating in this mission, the KidSat camera was used to image a 140 km wide, 1950 km long strip that starts in the northwest (5.24 degrees N, 97.11 degrees E), and follows the Pegunungan Barisan range across the equator to the southern tip of Sumatra 7.44S, 106.1E [MET 00215343 - 00215750]. Smoldering underground fires have raged uncontrolled for the past few weeks in Southeast Asia. Originally set to clear land for agriculture, the fires are usually extinguished by the annual monsoon rains. However, this year, the rains had not come due to El Niño which produces dry conditions in the Indonesia region. Due to the lack of trade winds, the seasonal warm waters in the eastern Pacific have spread over to South America. Consequently, the water temperature in Indonesia has dropped significantly. This decrease in temperature has not produced enough warm water vapor to produce the normal seasonal showers that usually encompass the area. The fire has now been blamed for two fatal accidents and countless health hazards. At one point, the pollution index of the region reached 839. To put a relative point to this number, a pollution index of 300 is a equivalent of smoking 20 cigarettes a day. The smoke, during one time, blanketed an area that was larger than the continental United States. Currently, the fire's rage has been quelled by winds and rain which have lifted the smog and dampened the fires. However it is estimated that 100,000 fire fighters are needed to stop the fire. The KidSat image shown here is a mosaic of three images of the 16 image series (Mission Elapsed Time) 00215624, 00215637, 00215701, the center latitude and longitude of each image, respectively, is 3.0 degrees S 102.9 degrees E, 3.7 degrees S 103.4 degrees E, 4.9 degrees S 104.3 degrees E and is 140 km wide and 400 km long. The images were captured on September 27, 1997 during Shuttle flight STS-86. Starting in the south (right) and traveling northwest (left), a clear view is visible of the southern tip of Sumatra with the volcanoes that make up the backbone of the island appearing darker than the surrounding land. Further northwest, the first smoke plumes appear in the rain forests east of the mountains where land is being cleared for palm plantations, the plumes indicate a prevailing wind to the northwest. Within a short distance, the region becomes completely blanketed in smoke with only the peaks of the volcanoes rising above the gray haze layer. The KidSat camera that photographed these fires is mounted in the overhead starboard window of the Shuttle Atlantis and operates before and after docking with Mir when the Shuttle's windows face the Earth. Students on the ground are linked to the camera through the Internet and a series of satellites. High school and undergraduate, students work in collaboration with scientists and engineers to develop and operate the KidSat systems. Curriculum developed by The Johns Hopkins University Institute for the Academic Advancement of Youth is used in the middle school classrooms to encourage scientific inquiry based on the images. The photographs from the three missions of the KidSat pilot program can be accessed at the following URL: http://www.jpl.nasa.gov/kidsat The KidSat program was developed by the Jet Propulsion Laboratory, The Johns Hopkins University Institute for the Academic Advancement of Youth, and The University of California, San Diego, with support from NASA's Johnson Space Center. The project is supported by NASA's Office of Human Resources and Education with support from NASA's Offices of Mission to Planet Earth, Space Flight, and Space Science. JPL is a division of the California Institute of Technology (Caltech). |
|
| General Description |
STS-111 Shuttle Mission Imagery |
|
Mojave Desert, California
| Title |
Mojave Desert, California |
| Description |
An orbital view of the space shuttle landing strip at the Mojave Desert dry lakebeds (35.0N, 118.0W) of Edwards Air Force Base, California. Just beneath the clouds on the coast at the top of the picture is the San Bernardino Valley and the city of Los Angeles. |
| Date Taken |
1981-04-14 |
|
Los Angeles, CA.
| Title |
Los Angeles, CA. |
| Description |
A general view of the greater Los Angeles region of California (34,0N, 118.5W) showing the coastline, Vandenberg AFB, the south end of the Central Valley and the dry lake beds at Edwards AFB, landing site of the space shuttle. |
| Date Taken |
1982-03-30 |
|
Landing, Edwards AFB, CA
| Title |
Landing, Edwards AFB, CA |
| Description |
This space shuttle landing scene shows the final approach to the concrete runway at Edwards AFB, CA (35.0N, 118.0W) and was taken from the flight deck looking through the front windows just before the vehicle made landfall. |
| Date Taken |
1983-04-09 |
|
STS-65 Pilot Halsell points
…
| Title |
STS-65 Pilot Halsell points camera out window on OV-102's aft flight deck |
| Description |
STS-65 Pilot James D. Halsell, Jr uses a handheld HASSELBLAD camera at aft flight deck overhead window W8 to take Earth photographs while aboard the orbiting Space Shuttle Columbia, Orbiter Vehicle (OV) 102. Part of Baja, California can be seen in the upper left quadrant of the photo. This photo was one of the first released by NASA following the International Microgravity Laboratory 2 (IML-2) mission. |
| Date Taken |
1994-07-23 |
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