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Orion Crew Module for the Or …
Photo Description The boiler …
11/5/08
Description Photo Description The boilerplate Orion crew module for the Orion Launch Abort System Pad Abort-1 flight test is tilted on jacks during weight and balance testing at NASA Dryden. Project Description NASA Dryden Flight Research Center has a critical role in the early development of the Constellation systems. Applying Dryden's expertise with testing unique flight configurations, Dryden is helping to manage and implement the abort flight tests for the Orion Crew Exploration Vehicle. Dryden will lead the development and integration of the full-size Orion test articles along with development of the ground support equipment, flight instrumentation and launch facility construction for the early pad abort and all ascent abort flight tests. The Orion Abort Flight Test effort includes two pad abort tests, simulating aborts during a launch pad emergency, and four ascent aborts, simulating aborts during first stage flight of Orion spacecraft. Dryden manages procurement and oversees development of the solid fuel abort test booster rockets used for ascent abort testing, and is responsible for the integration of the Orion test articles with their booster rockets. NASA Dryden is also supporting Constellation program technical integration activities. Future Dryden support roles include assisting with the development of lunar lander test and verification support and flight simulation support of the Constellation training facility. Other potential support include west coast recovery operations, and operation of a lunar / Mars surface analog test site. The Orion Abort Flight Test project is managed by NASA Dryden under the leadership of the Project Orion Flight Test Office at NASA's Johnson Space Center, Houston, Texas. Part of NASA's fleet of next generation spacecraft, Orion is being designed to take astronauts to the International Space Station and then back to the moon by 2020. November 5, 2008 NASA / Photo Tony Landis ED08-0230-236
Date 11/5/08
The Boilerplate Orion Crew M …
Photo Description The boiler …
11/5/08
Description Photo Description The boilerplate Orion crew module for the Orion Launch Abort System Pad Abort-1 flight test undergoes moment-of-inertia testing. Project Description NASA Dryden Flight Research Center has a critical role in the early development of the Constellation systems. Applying Dryden's expertise with testing unique flight configurations, Dryden is helping to manage and implement the abort flight tests for the Orion Crew Exploration Vehicle. Dryden will lead the development and integration of the full-size Orion test articles along with development of the ground support equipment, flight instrumentation and launch facility construction for the early pad abort and all ascent abort flight tests. The Orion Abort Flight Test effort includes two pad abort tests, simulating aborts during a launch pad emergency, and four ascent aborts, simulating aborts during first stage flight of Orion spacecraft. Dryden manages procurement and oversees development of the solid fuel abort test booster rockets used for ascent abort testing, and is responsible for the integration of the Orion test articles with their booster rockets. NASA Dryden is also supporting Constellation program technical integration activities. Future Dryden support roles include assisting with the development of lunar lander test and verification support and flight simulation support of the Constellation training facility. Other potential support include west coast recovery operations, and operation of a lunar / Mars surface analog test site. The Orion Abort Flight Test project is managed by NASA Dryden under the leadership of the Project Orion Flight Test Office at NASA's Johnson Space Center, Houston, Texas. Part of NASA's fleet of next generation spacecraft, Orion is being designed to take astronauts to the International Space Station and then back to the moon by 2020. November 5, 2008 NASA / Photo Tony Landis ED08-0230-362
Date 11/5/08
Oblique Wing Research
ECN-17954 Standing in front …
4/23/09
Description ECN-17954 Standing in front of the AD-1 Oblique Wing research aircraft is research pilot Richard E. Gray. Richard E. Gray joined National Aeronautics and Space Administration's Johnson Space Center, Houston, Texas, in November 1978, as an aerospace research pilot. In November 1981, Dick joined the NASA's Ames-Dryden Flight Research Facility, Edwards, California, as a research pilot. Dick was a former Co-op at the NASA Flight Research Center (a previous name of the Ames-Dryden Flight Research Facility), serving as an Operations Engineer. At Ames-Dryden, Dick was a pilot for the F-14 Aileron Rudder Interconnect Program, AD-1 Oblique Wing Research Aircraft, F-8 Digital Fly-By-Wire and Pilot Induced Oscillations investigations. He also flew the F-104, T-37, and the F-15. On November 8, 1982, Gray was fatally injured in a T-37 jet aircraft while making a pilot proficiency flight. Dick graduated with a Bachelors degree in Aeronautical Engineering from San Jose State University in 1969. He joined the U.S. Navy in July 1969, becoming a Naval Aviator in January 1971, when he was assigned to F-4 Phantoms at Naval Air Station (NAS) Miramar, California. In 1972, he flew 48 combat missions in Vietnam in F-4s with VF-111 aboard the USS Coral Sea. After making a second cruise in 1973, Dick was assigned to Air Test and Evaluation Squadron Four (VX-4) at NAS Point Mugu, California, as a project pilot on various operational test and evaluation programs. In November 1978, Dick retired from the Navy and joined NASA's Johnson Space Center. At JSC Gray served as chief project pilot on the WB-57F high-altitude research projects and as the prime television chase pilot in a T-38 for the landing portion of the Space Shuttle orbital flight tests. Dick had over 3,000 hours in more than 30 types of aircraft, an airline transport rating, and 252 carrier arrested landings. He was a member of the Society of Experimental Test Pilots serving on the Board of Directors as Southwest Section Technical Adviser in 1981/1982. &#8250, Read Project Description January 1, 1982 NASA Photo /
Date 4/23/09
Meteorite Hunters
title Meteorite Hunters
description When a meteorite is found, the ANSMET (Antarctic Search for Meteorites) team records its location, size, color, amount of fusion crust, probable type, and anything else that might be important. Some of their tools are similar to those used by the Apollo astronauts to collect samples, and some are the latest high-tech (like Global Positioning Satellite navigation). The team takes great care not to contaminate the meteorites. Meteorites are handled only with stainless steel instruments, and are immediately sealed in sterile plastic or aluminum foil packages. Meteorites collected by the ANSMET team in Antarctica are packed in dry ice to mimic conditions in the field and shipped to the Antarctic Meteorite Laboratory at NASA's Johnson Space Center in Houston, Texas. *Image Credit*: NASA Johnson Space Center
Meteorite Processing
title Meteorite Processing
description After meteorites are found in Antarctica, they are carried to the Antarctic Meteorite Laboratory at NASA's Johnson Space Center in Houston, Texas. There, the meteorites are cataloged, examined, classified, and stored. This slide shows technicians working with meteorites in a sterile cabinet filled with dry nitrogen gas. The dry gas keeps the meteorites relatively free of contamination and keeps them from rusting. The technician on the left is examining a meteorite through a microscope, and the technician on the right is breaking a meteorite to expose its interior. The technicians put their hands into the black rubber gloves on the cabinets, which allows them to work without getting the meteorites dirty or exposing them to air. *Image Credit*: NASA Johnson Space Center
Aaron Cohen
Title Aaron Cohen
Full Description Aaron Cohen served as NASA Acting Deputy Administrator from February 19, 1992 to November 1, 1992. Mr. Cohen started at NASA's Johnson Space Center in 1962 working on the Apollo program. After Apollo he served as Manager of the Space Shuttle orbiter, directing the development and testing of the orbiter. In 1986 he assumed the position of Johnson Space Center Director. After retiring from NASA in 1993, Mr. Cohen became the Zachry Professor of Engineering at his alma mater, Texas A&M University.
Date 12/20/1982
NASA Center Johnson Space Center
Aerial View of the Johnson S …
Title Aerial View of the Johnson Space Center
Full Description An aerial view of the complete Johnson Space Center facility in Houston, Texas. A portion of Clear Lake can be seen at the top of the view.
Date 08/10/1989
NASA Center Johnson Space Center
Apollo 15 Crew and Family Me …
Title Apollo 15 Crew and Family Members
Full Description The three Apollo 15 crew receive a welcome on their arrival at Ellington Air Force Base, Houston, Texas, after en eight-hour flight aboard a U.S. Air Force C-141 jet aircraft from Hawaii. Left to right are: Astronauts David R. Scott, Alfred M. Worden and James B. Irwin. Members of the astronaut's families identified in picture are left to right: Scott's daughter, Tracy, Worden's father, Merrill Worden, Worden's daughter, Merrill, and Irwin's two daughters, Joy and Jill.
Date 08/08/1971
NASA Center Johnson Space Center
Northrop T-38A Talon
Title Northrop T-38A Talon
Full Description This Northrop T-38A flew at Langley from 1972 until 1980, when it was returned to the Johnson Space Center's flight operations at Ellington AFB, Texas. While at Langley, the Talon flew as a mission support aircraft and participated in aircraft noise studies. It was also used as an adversary against the XV-6A Kestrel "jump jet" in one-on-one combat to test Vectoring in Forward Flight (VIFF).
Date 9/19/1974
NASA Center Langley Research Center
Astronaut John Glenn being H …
Title Astronaut John Glenn being Honored
Full Description Astronaut John Glenn, Jr. is honored by President John F. Kennedy after his historical first manned orbital flight. The ceremony is being held at the Manned Spacecraft Center in Langley, Virginia. The Center moved to Houston, Texas later that year, where it continues to reside.
Date 2/23/1962
NASA Center Johnson Space Center
Bell Lunar Landing Training …
Title Bell Lunar Landing Training Vehicle (LLTV)
Full Description Following the crash of a sister Lunar Landing Training Vehicle at Ellington Field in Houston, Texas, the Bell LLTV (NASA 952) was sent from Houston to Langley for tests in the 30 x 60 Full Scale Tunnel. The LLTV was returned to Houston for further training use a short time later. NASA 952 is now on exhibit at the Johnson Space Center in Houston, Texas.
Date 1/16/1969
NASA Center Langley Research Center
Challenger Ferry Flight Flyo …
Title Challenger Ferry Flight Flyover
Full Description View of the Shuttle Challenger atop the Shuttle Carrier Aircraft (SCA), NASA-905, during its return to Kennedy Space Center (KSC) and flyover of the Johnson Space Center (JSC) and the Houston skyline on Saturday, April 9, 1983.
Date 04/18/1983
NASA Center Johnson Space Center
President Reagan at Mission …
Title President Reagan at Mission Control, Houston
Full Description President Ronald Reagan gets a laugh from NASA officials in Mission Control when he jokingly asks crew members, astronauts Joe Engle and Richard Truly if they could stop by Washington en route to their California landing site in order that he might come along. The STS-2 crew was in their next to last day on orbit when the conversation took place. From left to right standing: Terry J. Hart, NASA Deputy Administrator Dr. Hans Mark, NASA Administrator James M. Beggs, JSC Director Dr. Christopher C. Kraft Jr. From left to right seated: CAPCOM, Astronaut Daniel C. Brandenstein President, Ronald Reagan Directly above the President in the background: JSC Flight Operations Director, Eugene F. Kranz
Date 11/13/1981
NASA Center Headquarters
Dr. Mae C. Jemison, First Af …
Title Dr. Mae C. Jemison, First African-American Woman in Space
Full Description The first African-American woman in space, Dr. Mae C. Jemison was born on October 17, 1956 in Decatur, Alabama but considers Chicago, Illinois her hometown. She received a Bachelor in Chemical Engineering (and completed the requirements for a Bachelor in African and Afro-American studies) at Stanford University in 1977. Dr. Jemison also received a Doctorate degree in medicine from Cornell University in 1981. After medical school she did post graduate medical training at the Los Angeles County University of Southern California Medical Center. As an area Peace Corps medical officer for Sierra Leone and Liberia in West Africa, she managed the health care delivery system for U.S. Peace Corps and U.S. Embassy personnel. Jemison's background includes work in the areas of nuclear magnetic resonance spectroscopy, and reproductive biology. She also developed and participated in research projects on the Hepatitis B vaccine and rabies. Jemison was a General Practitioner and attending graduate Engineering classes in Los Angeles when she was named an astronaut candidate in 1987. She flew her first flight as a science mission specialist on STS-47, Spacelab-J, in September 1992. She was co-investigator for the Bone Cell Research Experiment on that mission. In completing her first space flight, Jemison logged 190 hours, 30 minutes and 23 seconds in space. Jemison resigned from NASA in March 1993. In 1994, she founded and began a term as chair of The Earth We Share (TEWS), an annual international science camp where students, aged 12 to 16, work together to solve current global dilemmas. From 1995- 2002 she was a professor of Environmental Studies at Dartmouth College. She is currently director of the Jemison Institute for Advancing Technology in developing countries. She is the recipient of numerous awards and honors, including induction into the National Women's Hall of Fame and several corporate boards of directors on the Texas Governor's State Council for Science and Biotechnology Development. Dr. Jemison published her memoirs, Find Where DE:the Wind Goes:Moments from My Life in 2001. She currently resides in Houston, Texas.
Date 07/1992
NASA Center Johnson Space Center
Skylab Solar Shield
Title Skylab Solar Shield
Full Description A sail like sunshade for possible use as a sunscreen for the Skylab Orbital Workshop (OWS) is shown being fabricated in the GE Building across the street from Johnson Space Center, Houston Texas. Three people help the steamstress feed the material through the sewing machine. The three-layered sunshade will be composed of a top layer of aluminized mylar, a middle layer of laminated nylon ripstop, and a bottom layer of thin nylon. Working on the sunshade are from left to right: Dale Gentry, Elizabeth Gauldin, Alyene Baker, and James H. Barnett Jr. Mrs. Baker, a GE employee, operates the double needle Singer sewing machine. Barnett is head of the Crew Equipment Development Section of JSC Crew Systems Division. Mrs. Gauldin is also with the Crew Systems Division. Gentry works for GE. The work shown here is part of the crash program underway to prepare a sunshield for Skylab to replace the orginal shield which was lost when Skylab 1 was launched on May 14, 1973. The improvised solar shield selected to be used will be carried to Earth orbit by the Skylab 2 crewman who will then deploy the reflective parasol to shade part of the OWS from the hot rays of the sun. Loss of the orginal sun shield has caused an overheating problem. in the Orbital Work Shop.
Date 01/01/1973
NASA Center Headquarters
Female Astronauts
Title Female Astronauts
Full Description Astronauts Dr. N. Jan Davis (left) and Dr. Mae C. Jemison (right) were mission specialists on board the STS-47 mission. Born on November 1, 1953 in Cocoa Beach, Florida, Dr. N. Jan Davis received a Master degree in Mechanical Engineering in 1983 followed by a Doctorate in Engineering from the University of Alabama in Huntsville in 1985. In 1979 she joined NASA Marshall Space Flight Center as an aerospace engineer. A veteran of three space flights, Dr. Davis has logged over 678 hours in space since becoming an astronaut in 1987. She flew as a mission specialist on STS-47 in 1992 and STS-60 in 1994, and was the payload commander on STS-85 in 1997. In July 1999, she transferred to the Marshall Space Flight Center, where she became Director of Flight Projects. Dr. Mae C. Jemison, the first African-American woman in space, was born on October 17, 1956 in Decatur, Alabama but considers Chicago, Illinois her hometown. She received a Bachelor degree in Chemical Engineering (and completed the requirements for a Bachelor degree in African and Afro-American studies) at Stanford University in 1977, and a Doctorate degree in medicine from Cornell University in 1981. After receiving her doctorate, she worked as a General Practitioner while attending graduate engineering classes in Los Angeles. She was named an astronaut candidate in 1987, and flew her first flight as a science mission specialists on STS-47, Spacelab-J, in September 1992, logging 190 hours, 30 minutes, 23 seconds in space. In March 1993, Dr. Jemison resigned from NASA, thought she still resides in Houston, Texas. She went on to publish her memoirs, Find Where the Wind Goes: Moments from My Life, in 2001. The astronauts are shown preparing to deploy the lower body negative pressure (LBNP) apparatus in this 35mm frame taken in the science module aboard the Earth-orbiting Space Shuttle Endeavor. Fellow astronauts Robert L. Gibson (Commander), Curtis L. Brown (Junior Pilot), Mark C. Lee (Payload Commander), Jay Apt (Mission Specialist), and Mamoru Mohri (Payload Specialist) joined the two on their maiden space flight. The Spacelab-J mission was a joint effort between Japan and the United States.
Date 09/15/1992
NASA Center Johnson Space Center
Gemini Mission Control
Title Gemini Mission Control
Full Description Overall view of the Mission Control Center (MCC), Houston, Texas, during the Gemini 5 flight. Note the screen at the front of the MCC which is used to track the progress of the Gemini spacecraft.
Date 08/21/1965
NASA Center Johnson Space Center
Gemini water egress training
Title Gemini water egress training
Full Description Astronauts John Young and Virgil I. (Gus) Grissom are pictured during water egress training in a large indoor pool at Ellington Air Force Base, Texas. Young is seated on top of the Gemini capsule while Grissom is in the water with a life raft.
Date 02/05/1965
NASA Center Johnson Space Center
JSC Aerial View
Title JSC Aerial View
Full Description This North-looking view shows some of the Johnson Space Center's central buildings and facilities neighboring its Project Management Facility (Building 1) from which this scene was photographed. The Houston-based Mission Control Center is in the center of the frame. Visible buildings surrounding the mall area include the Flight Operations Facility, Crew Systems Laboratory, Photographic Technology Laboratory, Technical Services shop, branch cafeteria, Mission Control Center office wing and the Central Data Office.
Date 12/08/1982
NASA Center Johnson Space Center
Kranz on Console
Title Kranz on Console
Full Description View of the Flight Directors console in the Mission Control Center (MCC), Houston, Texas, during the Gemini 5 flight. Seated at the console are Eugene F. Kranz (foreground) and Dr. Christopher C. Kraft Jr. (background). Standing in front of the console are Dr. Charles Berry (left), an unidentified man in the center and astronaut Elliot M. See.
Date 08/21/1965
NASA Center Johnson Space Center
X-38: Close-up of Pyrotechni …
Photo Description In these close-ups, the canister containing the seven-foot-diameter X-38 Flight Termination System (FTS) parachute can be seen launching safely away from an aft-end mockup of the X-38 by a pyrotechnic firing system in December 19, 1996, at NASA Dryden Flight Research Center, Edwards, California. The test was economically accomplished by mounting the mockup of the X-38's aft-end, minus vertical stabilizers, on a truck prior to installation in the X-38.
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 December 1996
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 …
X-38 research aircraft - sec …
X-38 research aircraft - Fir …
X-38 vehicle descending towa …
X-38 research aircraft deorb …
X-38 research aircraft landi …
X-38 research aircraft launc …
Research pilot Mark Stucky
Photo Date February 15, 1996
Research pilot Fred Haise
Photo Date April 7, 1966
Test pilot Michael R. Swann
Photo Date August 21, 1978
NASA Dryden Flight Research …
Photo Description NASA Dryden Flight Research Center's chief pilot Gordon Fullerton in the cockpit of the center's T-38 Talon mission support aircraft.
Project Description A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s.
Photo Date February 24, 2005
Photo Description Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center.
Project Description A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s.
Photo Date February 24, 2005
Photo Description A close-up of the panels on the F-15B's flight test fixture shows five divots of TPS foam were successfully ejected during the LIFT experiment flight #2, the first flight with TPS foam.
Project Description NASA's Dryden Flight Research Center at Edwards Air Force Base, California, conducted a series of flights with the center's F-15B Research Testbed aircraft in support of Space Shuttle Return-to-Flight engineering efforts. The Shuttle Return to Flight team requested data on the structural survivability of external tank insulating foam debris or "divots" that are shed from the tank during a Shuttle launch. The Lifting Insulating Foam Trajectory (LIFT) flight test series used NASA's F-15B to test these ?divots? in a real flight environment at speeds up to about Mach 2. Small-scale divoting, commonly called popcorning, results from adhesive strength failure of external tank thermal protection system (TPS) foam brought about by decreasing atmospheric pressure combined with increased heating during Shuttle ascent. According to LIFT project manager Stephen Corda, objectives of the flight tests on the F-15B included determining divot structural survivability in a flight environment, assessing divot stability, quantifying divot trajectories using videography, and providing flight verification of debris tracking systems to be used for Shuttle launches. "We're using the unique capabilities of the supersonic F-15B aircraft and the aerodynamic flight test fixture to provide a means to eject these debris or divots from the fixture, and then photograph them with a high speed digital video system, where we're able to video these divots in flight at up to 10,000 frames per second," Corda noted. The debris tracking systems were verified using the F-15B as a surrogate Space Shuttle while the aircraft ejects TPS foam divots. These tracking systems included a Weibel Doppler radar and a high-definition video system aboard a NASA WB-57 aircraft. NASA' s Space Shuttle Systems Engineering and Integration office at the Johnson Space Center (JSC) in Houston, Texas, funded the LIFT flight tests at NASA Dryden as part of the STS-114 Return-to-Flight effort. JSC aeroscience engineer Ricardo Machin said the current LIFT flight tests will help them validate the models that they use for debris transport analysis."In particular, it's going to help us understand whether the divots break up once they come off the external tank, and secondly whether they will trim and begin to fly, or if they'll tumble. The difference between trimming and flying makes a huge difference ? the amount of kinetic energy that this piece of debris can impart to the shuttle," Machin said. The LIFT flight test requires two new capabilities: an in-flight foam divot ejection system, and a high-speed video system to track and record the trajectories of the divots in flight. Both capabilities were developed by Dryden engineers. Dryden's LIFT team designed, fabricated, and ground-tested four different divot ejection systems, completing 70 ground tests to determine and refine the best approach. NASA Dryden engineers designed and procured the very high-speed digital video equipment, including, development of a system to synchronize the cameras with the divot ejection system. In addition, they developed videography analysis techniques in order to quantify divot trajectories. The Dryden team completed the design and ground tests of these systems over a compact 2 1/2-month period.
Photo Date February 16, 2005
Photo Description All six divots of thermal insulation foam have been ejected from the flight test fixture on NASA's F-15B testbed as it returns from a LIFT experiment flight.
Project Description NASA's Dryden Flight Research Center at Edwards Air Force Base, California, conducted a series of flights with the center's F-15B Research Testbed aircraft in support of Space Shuttle Return-to-Flight engineering efforts. The Shuttle Return to Flight team requested data on the structural survivability of external tank insulating foam debris or "divots" that are shed from the tank during a Shuttle launch. The Lifting Insulating Foam Trajectory (LIFT) flight test series used NASA's F-15B to test these ?divots? in a real flight environment at speeds up to about Mach 2. Small-scale divoting, commonly called popcorning, results from adhesive strength failure of external tank thermal protection system (TPS) foam brought about by decreasing atmospheric pressure combined with increased heating during Shuttle ascent. According to LIFT project manager Stephen Corda, objectives of the flight tests on the F-15B included determining divot structural survivability in a flight environment, assessing divot stability, quantifying divot trajectories using videography, and providing flight verification of debris tracking systems to be used for Shuttle launches. "We're using the unique capabilities of the supersonic F-15B aircraft and the aerodynamic flight test fixture to provide a means to eject these debris or divots from the fixture, and then photograph them with a high speed digital video system, where we're able to video these divots in flight at up to 10,000 frames per second," Corda noted. The debris tracking systems were verified using the F-15B as a surrogate Space Shuttle while the aircraft ejects TPS foam divots. These tracking systems included a Weibel Doppler radar and a high-definition video system aboard a NASA WB-57 aircraft. NASA' s Space Shuttle Systems Engineering and Integration office at the Johnson Space Center (JSC) in Houston, Texas, funded the LIFT flight tests at NASA Dryden as part of the STS-114 Return-to-Flight effort. JSC aeroscience engineer Ricardo Machin said the current LIFT flight tests will help them validate the models that they use for debris transport analysis."In particular, it's going to help us understand whether the divots break up once they come off the external tank, and secondly whether they will trim and begin to fly, or if they'll tumble. The difference between trimming and flying makes a huge difference ? the amount of kinetic energy that this piece of debris can impart to the shuttle," Machin said. The LIFT flight test requires two new capabilities: an in-flight foam divot ejection system, and a high-speed video system to track and record the trajectories of the divots in flight. Both capabilities were developed by Dryden engineers. Dryden's LIFT team designed, fabricated, and ground-tested four different divot ejection systems, completing 70 ground tests to determine and refine the best approach. NASA Dryden engineers designed and procured the very high-speed digital video equipment, including, development of a system to synchronize the cameras with the divot ejection system. In addition, they developed videography analysis techniques in order to quantify divot trajectories. The Dryden team completed the design and ground tests of these systems over a compact 2 1/2-month period.
Photo Date February 14, 2005
Photo Description NASA's F-15B carrying thermal insulation foam on its flight test fixture is shadowed by a NASA F-18B chase aircraft during a LIFT experiment research flight.
Project Description Before the Space Shuttle can safely return to flight, engineers need data on how insulating foam debris or "divots" behave when these small pieces are shed from the Shuttle's external fuel tank during launch. NASA's Dryden Flight Research Center conducted a series of flight tests of the divots as part of the Return to Flight team effort. The Lifting Insulating Foam Trajectory (LIFT) flight test series at Dryden used the center's F-15B Research Testbed aircraft to test these "divots" in a real flight environment at speeds up to about Mach 2, or twice the speed of sound. Small-scale divoting occurs when the adhesive on the external tank thermal protection system (TPS) foam fails. This occurs as a result of decreasing atmospheric pressure combined with increased heating during Shuttle ascent causing air trapped beneath the TPS to expand. Objectives of the LIFT flight tests on the F-15B include determining divot structural survivability and stability in flight and quantifying divot trajectories using videography. The flight data of divot trajectories may also be used for Computational Fluid Dynamic code validation. NASA's Space Shuttle Systems Engineering and Integration office at the Johnson Space Center (JSC) in Houston, Texas, funded the LIFT flight tests at NASA Dryden as part of the Space Shuttle Return-to-Flight effort. The LIFT flight test required two new capabilities: an in-flight foam divot ejection system, and a high-speed video system to track and record the trajectories of the divots in flight. Both capabilities were developed by Dryden engineers in just over two months. Dryden's LIFT team designed, fabricated, and ground-tested four different divot ejection systems, completing 70 ground tests to determine and refine the best approach. NASA Dryden engineers also designed and procured the very high-speed digital video equipment, including development of a system to synchronize the cameras with the divot ejection system. In addition, they developed videography analysis techniques in order to quantify divot trajectories.
Photo Date February 16, 2005
Photo Description A post-flight inspection of the panels on the F-15B's flight test fixture shows five divots of TPS foam were successfully ejected during the LIFT experiment flight #2, the first flight with TPS foam.
Project Description Before the Space Shuttle can safely return to flight, engineers need data on how insulating foam debris or "divots" behave when these small pieces are shed from the Shuttle's external fuel tank during launch. NASA's Dryden Flight Research Center conducted a series of flight tests of the divots as part of the Return to Flight team effort. The Lifting Insulating Foam Trajectory (LIFT) flight test series at Dryden used the center's F-15B Research Testbed aircraft to test these "divots" in a real flight environment at speeds up to about Mach 2, or twice the speed of sound. Small-scale divoting occurs when the adhesive on the external tank thermal protection system (TPS) foam fails. This occurs as a result of decreasing atmospheric pressure combined with increased heating during Shuttle ascent causing air trapped beneath the TPS to expand. Objectives of the LIFT flight tests on the F-15B include determining divot structural survivability and stability in flight and quantifying divot trajectories using videography. The flight data of divot trajectories may also be used for Computational Fluid Dynamic code validation. NASA's Space Shuttle Systems Engineering and Integration office at the Johnson Space Center (JSC) in Houston, Texas, funded the LIFT flight tests at NASA Dryden as part of the Space Shuttle Return-to-Flight effort. The LIFT flight test required two new capabilities: an in-flight foam divot ejection system, and a high-speed video system to track and record the trajectories of the divots in flight. Both capabilities were developed by Dryden engineers in just over two months. Dryden's LIFT team designed, fabricated, and ground-tested four different divot ejection systems, completing 70 ground tests to determine and refine the best approach. NASA Dryden engineers also designed and procured the very high-speed digital video equipment, including development of a system to synchronize the cameras with the divot ejection system. In addition, they developed videography analysis techniques in order to quantify divot trajectories.
Photo Date February 16, 2005
Photo Description Puffy white clouds and a flooded lakebed form a backdrop as a T-38 support aircraft taxies across the ramp in front of NASA's Boeing 747 Shuttle Carrier Aircraft.
Project Description A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s.
Photo Date February 24, 2005
Photo Description Pilot Gordon Fullerton taxies NASA Dryden's "newest" mission support aircraft, a T-38 Talon, into position on the ramp upon its arrival on February 24, 2005.
Project Description A sleek, supersonic T-38 trainer jet is taxied into the parking ramp at NASA's Dryden Flight Research Center by Dryden's chief pilot Gordon Fullerton, marking the return of the type to Dryden for the first time in more than 10 years. Formerly assigned to NASA's Langley Research Center in Hampton, Va., the aircraft had supported various aeronautics research projects there for a number of years. The aircraft will be used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s.
Photo Date February 24, 2005
Photo Description Two panels of Space Shuttle TPS insulation were mounted on the flight test fixture underneath NASA's F-15B during the Lifting Foam Trajectory flight test series.
Project Description Before the Space Shuttle can safely return to flight, engineers need data on how insulating foam debris or "divots" behave when these small pieces are shed from the Shuttle's external fuel tank during launch. NASA's Dryden Flight Research Center conducted a series of flight tests of the divots as part of the Return to Flight team effort. The Lifting Insulating Foam Trajectory (LIFT) flight test series at Dryden used the center's F-15B Research Testbed aircraft to test these "divots" in a real flight environment at speeds up to about Mach 2, or twice the speed of sound. Small-scale divoting occurs when the adhesive on the external tank thermal protection system (TPS) foam fails. This occurs as a result of decreasing atmospheric pressure combined with increased heating during Shuttle ascent causing air trapped beneath the TPS to expand. Objectives of the LIFT flight tests on the F-15B include determining divot structural survivability and stability in flight and quantifying divot trajectories using videography. The flight data of divot trajectories may also be used for Computational Fluid Dynamic code validation. NASA's Space Shuttle Systems Engineering and Integration office at the Johnson Space Center (JSC) in Houston, Texas, funded the LIFT flight tests at NASA Dryden as part of the Space Shuttle Return-to-Flight effort. The LIFT flight test required two new capabilities: an in-flight foam divot ejection system, and a high-speed video system to track and record the trajectories of the divots in flight. Both capabilities were developed by Dryden engineers in just over two months. Dryden's LIFT team designed, fabricated, and ground-tested four different divot ejection systems, completing 70 ground tests to determine and refine the best approach. NASA Dryden engineers also designed and procured the very high-speed digital video equipment, including development of a system to synchronize the cameras with the divot ejection system. In addition, they developed videography analysis techniques in order to quantify divot trajectories.
Photo Date February 16, 2005
Photo Description NASA Dryden's T-38 Talon trainer jet in flight over the main base complex at Edwards Air Force Base. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center.
Project Description Formerly assigned to NASA's Langley Research Center in Hampton, Va., the T-38 aircraft had supported various aeronautics research projects there for a number of years. The aircraft is used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s.
Photo Date May 5, 2006
Photo Description NASA Dryden's T-38 Talon trainer aircraft in flight near Edwards Air Force Base. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center.
Project Description Formerly assigned to NASA's Langley Research Center in Hampton, Va., the T-38 aircraft had supported various aeronautics research projects there for a number of years. The aircraft is used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s.
Photo Date May 5, 2006
Photo Description NASA Dryden's T-38 trainer aircraft in flight over Cuddeback Dry Lake in Southern California. Formerly at NASA's Langley Research Center, this Northrop T-38 Talon is now used for mission support and pilot proficiency at the Dryden Flight Research Center.
Project Description Formerly assigned to NASA's Langley Research Center in Hampton, Va., the T-38 aircraft had supported various aeronautics research projects there for a number of years. The aircraft is used by NASA Dryden's research pilots for proficiency and mission support flights. Dryden operated two T-38s for a number of years, replacing them with newer F-18s. However, the cost of maintaining and operating the F-18s make the fuel-friendly, lower maintenance T-38 an attractive addition to Dryden's fleet. NASA has also operated a small fleet of T-38s for pilot proficiency and training for astronauts at the Johnson Space Center in Texas since the mid-1960s.
Photo Date May 5, 2006
X-38 Being Prepared for Ship …
Photo Description Technicians prepare the X-38 research vehicle for shipment in a Dryden Flight Research Center hangar in May 2000.
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 May 2000
The X-38 Second Prototype Gl …
Photo Description The X-38 technology demonstrator descends under its steerable parafoil toward a lakebed landing in a March 2000 test flight.
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 March 2000
The X-38 lifting body resear …
Photo Description The X-38 lifting body research vehicle, seen here wrapped in a protective material, is lowered onto a truck for shipping from the Dryden Flight Research Center in May 2000.
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 May 2000
X-38 Being Prepared for Ship …
Photo Description Technicians prepare the X-38 lifting body research vehicle, seen here wrapped in a protective material, for shipping in May 2000.
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 May 2000
The X-38 Second Prototype Fl …
Photo Description The X-38, a research vehicle built to help develop technology for an emergency Crew Return Vehicle from the International Space Station, is seen just before touchdown on a lakebed near the Dryden Flight Research Center, Edwards California, at the end of a March 2000 test flight.
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 March 2000
X-38 Being Prepared for Ship …
Photo Description Technicians prepare the X-38 lifting body research vehicle, seen here wrapped in a protective material, for shipping in May 2000.
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 May 2000
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