• Smithsonian NASM | Gemini Rogallo Paraglider Wing
    Wikipedia | Rogallo wing
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    Details, quoting from Smithsonian National Air and Space Museum | Mobile Quarantine Facility

    Contractor:
    Melpar, Inc.

    Manufacturer:
    Airstream, Inc.

    Country of Origin:
    United States of America

    Dimensions:
    Overall: 8 ft. 7 in. tall x 9 ft. wide x 35 ft. deep, 12499.9 lb. (261.62 x 274.32 x 1066.8cm, 5669.9kg)

    Materials:
    Aluminum, Glass

    This Mobile Quarantine Facility (MQF) was one of four built by NASA for astronauts returning from the Moon. Its purpose was to prevent the unlikely spread of lunar contagions by isolating the astronauts from contact with other people. A converted Airstream trailer, the MQF contained living and sleeping quarters, a kitchen, and a bathroom. Quarantine was assured by keeping the air pressure inside lower than the pressure outside and by filtering the air vented from the facility.

    This MQF was used by Apollo 11 astronauts Armstrong, Aldrin, and Collins immediately after their return to Earth. They remained in it for 65 hours, while the MQF was flown from the aircraft carrier Hornet to the Johnson Space Center in Houston. They were allowed to emerge once scientists were sure they were not infected with "moon germs."

    NASA transferred the MQF to the Smithsonian Institution in 1974.

    Transferred from the National Aeronautics and Space Administration
  • Gemini TTV-1 Paraglider Capsule
    www.nasm.si.edu/collections/artifact.cfm?id=A19750833000
  • Gemini VII Capsule
    www.nasm.si.edu/collections/artifact.cfm?id=A19680273000
  • Satellites:
    Explorer 1 satellite mock-up (Wikipedia)
    Explorer 6 satellite (Wikipedia)
    Explorer 7 satellite (Wikipedia)
    Explorer 8 satellite (Wikipedia)
    Explorer 10 satellite (Wikipedia)
    Explorer 17 satellite (Wikipedia)
    IMP-A satellite (Wikipedia)
    LOFTI-I satellite (Wikipedia)
    Vanguard 3 satellite (Wikipedia)
    Vanguard Lyman Alpha satellite (Wikipedia)
    Vanguard Magnetometer satellite (Wikipedia)
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    Details, quoting from Smithsonian National Air and Space Museum | Smithsonian NASM | Tracking and Data Relay Satellite (TDRSS Satellite)

    Manufacturer:
    TRW Design Models Inc.

    Country of Origin:
    United States of America

    Dimensions:
    Overall (antennas and solar arrays deployed): 14 ft. tall x 43 ft. wide x 57 ft. deep, 1800 lb. (426.7 x 1310.6 x 1737.4cm, 816.5kg)

    Materials:
    Wood, glass, capton, plastic

    During the first decades of the Space Age, NASA required a worldwide network of ground stations to communicate with satellites and human-operated spacecraft. The Tracking and Data Relay Satellite (TDRS) system, a constellation of three spacecraft placed into geosynchronous orbit beginning in 1983, was designed to replace this expensive, far-flung system. Positioned equidistant in orbit, they provide nearly continuous contact with spacecraft in low Earth orbit-an especially crucial capability for ensuring the safety of Space Shuttle crews. A TDRS transmits both voice and data communications. Under optimum conditions, it can transfer in a second the equivalent of a 20-volume encyclopedia.

    This artifact is a high-fidelity model built by Design Models, Inc., under the direction of TRW, which manufactured the first several TDRS spacecraft. TRW donated the model in 1986.

    Gift of TRW, Inc.
  • Mercury Capsule "Big Joe"
    www.nasm.si.edu/collections/artifact.cfm?id=A19680244000
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    Details, quoting from Smithsonian National Air and Space Museum | Apollo Boilerplate Command Module

    Manufacturer:
    North American Aviation Inc.

    Country of Origin:
    United States of America

    Dimensions:
    Overall: 10 ft. 7 in. tall x 12 ft. 10 in. diameter, 4000 lb. (322.58 x 391.16cm, 1814.4kg)

    Materials:
    Aluminum structure; painted fibreglass exterior

    As part of the Apollo program, a number of so-called "boilerplate" (bp) command modules were constructed to undergo various tests and to serve as training vehicles for astronauts and other mission crew members. BP 1102A is actually constructed of aluminum, with a fiberglass outer shell and an actual Command Module hatch. The initial use of BP1102A was as the water egress trainer for all Apollo flights, including by the crew of Apollo 11, the first lunar landing mission. As such, it was fitted with actual or mock-up interior components and used by astronauts to practice routine and emergency exits from the spacecraft.

    Subsequently, the interior was set up to be configured either as Apollo/Soyuz or a five-man rescue vehicle as once proposed for Skylab so that astronauts could train for those missions. It was finally transferred from NASA to the Smithsonian in 1977, and is displayed now at the Hazy Center with the flotation collar and bags that were attached to Columbia at the end of its historic mission.

    Transferred from the National Aeronautics and Space Administration, Johnson Space Center.
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    Details, quoting from Smithsonian National Air and Space Museum | Space Shuttle Enterprise:

    Manufacturer:
    Rockwell International Corporation

    Country of Origin:
    United States of America

    Dimensions:
    Overall: 57 ft. tall x 122 ft. long x 78 ft. wing span, 150,000 lb.
    (1737.36 x 3718.57 x 2377.44cm, 68039.6kg)

    Materials:
    Aluminum airframe and body with some fiberglass features; payload bay doors are graphite epoxy composite; thermal tiles are simulated (polyurethane foam) except for test samples of actual tiles and thermal blankets.

    The first Space Shuttle orbiter, "Enterprise," is a full-scale test vehicle used for flights in the atmosphere and tests on the ground; it is not equipped for spaceflight. Although the airframe and flight control elements are like those of the Shuttles flown in space, this vehicle has no propulsion system and only simulated thermal tiles because these features were not needed for atmospheric and ground tests. "Enterprise" was rolled out at Rockwell International's assembly facility in Palmdale, California, in 1976. In 1977, it entered service for a nine-month-long approach-and-landing test flight program. Thereafter it was used for vibration tests and fit checks at NASA centers, and it also appeared in the 1983 Paris Air Show and the 1984 World's Fair in New Orleans. In 1985, NASA transferred "Enterprise" to the Smithsonian Institution's National Air and Space Museum.

    Transferred from National Aeronautics and Space Administration

    • • •

    Quoting from Wikipedia | Space Shuttle Enterprise:

    The Space Shuttle Enterprise (NASA Orbiter Vehicle Designation: OV-101) was the first Space Shuttle orbiter. It was built for NASA as part of the Space Shuttle program to perform test flights in the atmosphere. It was constructed without engines or a functional heat shield, and was therefore not capable of spaceflight.

    Originally, Enterprise had been intended to be refitted for orbital flight, which would have made it the second space shuttle to fly after Columbia. However, during the construction of Columbia, details of the final design changed, particularly with regard to the weight of the fuselage and wings. Refitting Enterprise for spaceflight would have involved dismantling the orbiter and returning the sections to subcontractors across the country. As this was an expensive proposition, it was determined to be less costly to build Challenger around a body frame (STA-099) that had been created as a test article. Similarly, Enterprise was considered for refit to replace Challenger after the latter was destroyed, but Endeavour was built from structural spares instead.


    Service

    Construction began on the first orbiter on June 4, 1974. Designated OV-101, it was originally planned to be named Constitution and unveiled on Constitution Day, September 17, 1976. A write-in campaign by Trekkies to President Gerald Ford asked that the orbiter be named after the Starship Enterprise, featured on the television show Star Trek. Although Ford did not mention the campaign, the president—who during World War II had served on the aircraft carrier USS Monterey (CVL-26) that served with USS Enterprise (CV-6)—said that he was "partial to the name" and overrode NASA officials.

    The design of OV-101 was not the same as that planned for OV-102, the first flight model; the tail was constructed differently, and it did not have the interfaces to mount OMS pods. A large number of subsystems—ranging from main engines to radar equipment—were not installed on this vehicle, but the capacity to add them in the future was retained. Instead of a thermal protection system, its surface was primarily fiberglass.

    In mid-1976, the orbiter was used for ground vibration tests, allowing engineers to compare data from an actual flight vehicle with theoretical models.

    On September 17, 1976, Enterprise was rolled out of Rockwell's plant at Palmdale, California. In recognition of its fictional namesake, Star Trek creator Gene Roddenberry and most of the principal cast of the original series of Star Trek were on hand at the dedication ceremony.

    Approach and landing tests (ALT)

    Main article: Approach and Landing Tests

    On January 31, 1977, it was taken by road to Dryden Flight Research Center at Edwards Air Force Base, to begin operational testing.

    While at NASA Dryden, Enterprise was used by NASA for a variety of ground and flight tests intended to validate aspects of the shuttle program. The initial nine-month testing period was referred to by the acronym ALT, for "Approach and Landing Test". These tests included a maiden "flight" on February 18, 1977 atop a Boeing 747 Shuttle Carrier Aircraft (SCA) to measure structural loads and ground handling and braking characteristics of the mated system. Ground tests of all orbiter subsystems were carried out to verify functionality prior to atmospheric flight.

    The mated Enterprise/SCA combination was then subjected to five test flights with Enterprise unmanned and unactivated. The purpose of these test flights was to measure the flight characteristics of the mated combination. These tests were followed with three test flights with Enterprise manned to test the shuttle flight control systems.

    Enterprise underwent five free flights where the craft separated from the SCA and was landed under astronaut control. These tests verified the flight characteristics of the orbiter design and were carried out under several aerodynamic and weight configurations. On the fifth and final glider flight, pilot-induced oscillation problems were revealed, which had to be addressed before the first orbital launch occurred.

    On August 12, 1977, the space shuttle Enterprise flew on its own for the first time.

    Preparation for STS-1

    Following the ALT program, Enterprise was ferried among several NASA facilities to configure the craft for vibration testing. In June 1979, it was mated with an external tank and solid rocket boosters (known as a boilerplate configuration) and tested in a launch configuration at Kennedy Space Center Launch Pad 39A.

    Retirement

    With the completion of critical testing, Enterprise was partially disassembled to allow certain components to be reused in other shuttles, then underwent an international tour visiting France, Germany, Italy, the United Kingdom, Canada, and the U.S. states of California, Alabama, and Louisiana (during the 1984 Louisiana World Exposition). It was also used to fit-check the never-used shuttle launch pad at Vandenberg AFB, California. Finally, on November 18, 1985, Enterprise was ferried to Washington, D.C., where it became property of the Smithsonian Institution.

    Post-Challenger

    After the Challenger disaster, NASA considered using Enterprise as a replacement. However refitting the shuttle with all of the necessary equipment needed for it to be used in space was considered, but instead it was decided to use spares constructed at the same time as Discovery and Atlantis to build Endeavour.

    Post-Columbia

    In 2003, after the breakup of Columbia during re-entry, the Columbia Accident Investigation Board conducted tests at Southwest Research Institute, which used an air gun to shoot foam blocks of similar size, mass and speed to that which struck Columbia at a test structure which mechanically replicated the orbiter wing leading edge. They removed a fiberglass panel from Enterprise's wing to perform analysis of the material and attached it to the test structure, then shot a foam block at it. While the panel was not broken as a result of the test, the impact was enough to permanently deform a seal. As the reinforced carbon-carbon (RCC) panel on Columbia was 2.5 times weaker, this suggested that the RCC leading edge would have been shattered. Additional tests on the fiberglass were canceled in order not to risk damaging the test apparatus, and a panel from Discovery was tested to determine the effects of the foam on a similarly-aged RCC leading edge. On July 7, 2003, a foam impact test created a hole 41 cm by 42.5 cm (16.1 inches by 16.7 inches) in the protective RCC panel. The tests clearly demonstrated that a foam impact of the type Columbia sustained could seriously breach the protective RCC panels on the wing leading edge.

    The board determined that the probable cause of the accident was that the foam impact caused a breach of a reinforced carbon-carbon panel along the leading edge of Columbia's left wing, allowing hot gases generated during re-entry to enter the wing and cause structural collapse. This caused Columbia to spin out of control, breaking up with the loss of the entire crew.

    Museum exhibit

    Enterprise was stored at the Smithsonian's hangar at Washington Dulles International Airport before it was restored and moved to the newly built Smithsonian's National Air and Space Museum's Steven F. Udvar-Hazy Center at Dulles International Airport, where it has been the centerpiece of the space collection. On April 12, 2011, NASA announced that Space Shuttle Discovery, the most traveled orbiter in the fleet, will be added to the collection once the Shuttle fleet is retired. When that happens, Enterprise will be moved to the Intrepid Sea-Air-Space Museum in New York City, to a newly constructed hangar adjacent to the museum. In preparation for the anticipated relocation, engineers evaluated the vehicle in early 2010 and determined that it was safe to fly on the Shuttle Carrier Aircraft once again.
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    Details, quoting from Smithsonian National Air and Space Museum | Space Shuttle Radar Topography Mission Canister, Antenna

    Manufacturer:
    AEC-Able Engineering Co.

    Country of Origin:
    United States of America

    Dimensions:
    Overall: 292.1 length x 136cm diameter, 984.3kg weight (9ft 7in. x 4ft 5 9/16in., 2170lb.)

    Materials:
    Aluminum, steel, titanium, plastic, copper

    In 2000, the Shuttle Endeavor carried the Shuttle Radar Topography Mission (SRTM) payload into orbit. Shuttle astronauts used the payload, manufactured by the AEC-Able Engineering Co., to map in high detail and three dimensions more than 70 percent of the Earth's surface--the most complete and accurate rendering of the planet's land masses ever attempted. The Museum possesses two components--the mast canister (this artifact) and the outboard support structure with its antennas--crucial to that mission.

    To acquire this data, the SRTM used a novel hardware system that featured a main antenna located in the Shuttle payload bay, a folding mast (in the mast canister) that extended 60 meters from the Shuttle, and then another antenna system that was positioned at the end of the mast (the outboard structure). It was this dual antenna system--the largest rigid structure then flown in space--that produced, through interferometry (a technique for combining the information obtained from the two, separate antennas), a three-dimensional mapping of the Earth.

    The mission was a joint undertaking of NASA's Jet Propulsion Laboratory and the Department of Defense's National Imagery and Mapping Agency. The military will use the highest resolution data from SRTM for terrain navigation for planes and cruise missiles. A lower resolution data set will be made available to civilian scientists and other users.

    NASA transferred these artifacts to the Museum in 2003.

    Transferred from NASA

    • • • • •

    Quoting from Wikipedia | Shuttle Radar Topography Mission

    The Shuttle Radar Topography Mission (SRTM) is an international research effort that obtained digital elevation models on a near-global scale from 56° S to 60° N,[2] to generate the most complete high-resolution digital topographic database of Earth prior to the release of the ASTER GDEM in 2009. SRTM consisted of a specially modified radar system that flew on board the Space Shuttle Endeavour during the 11-day STS-99 mission in February 2000, based on the older Spaceborne Imaging Radar-C/X-band Synthetic Aperture Radar (SIR-C/X-SAR), previously used on the Shuttle in 1994. To acquire topographic (elevation) data, the SRTM payload was outfitted with two radar antennas.[2] One antenna was located in the Shuttle's payload bay, the other – a critical change from the SIR-C/X-SAR, allowing single-pass interferometry – on the end of a 60-meter (200-foot) mast[2] that extended from the payload bay once the Shuttle was in space. The technique employed is known as Interferometric Synthetic Aperture Radar.

    The elevation models are arranged into tiles, each covering one degree of latitude and one degree of longitude, named according to their south western corners. It follows that "n45e006" stretches from 45°N 6°E to 46°N 7°E and "s45w006" from 45°S 6°W to 44°S 5°W. The resolution of the cells of the source data is one arc second, but 1" (approx. 30 meter) data have only been released over United States territory; for the rest of the world, only three-arc-second (approx. 90-meter) data are available.[3] Each one arc second tile has 3,601 rows, each consisting of 3,601 16 bit bigendian cells. The dimensions of the three-arc-second tiles are 1201 x 1201.

    The elevation models derived from the SRTM data are used in Geographic Information Systems. They can be downloaded freely over the Internet, and their file format (.hgt) is supported by several software developments.

    The Shuttle Radar Topography Mission is an international project spearheaded by the U.S. National Geospatial-Intelligence Agency (NGA) and the U.S. National Aeronautics and Space Administration (NASA).
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    Details, quoting from Smithsonian National Air and Space Museum | Homing Overlay Experiment Test Vehicle

    Manufacturer:
    Lockheed Missiles and Space Division

    Country of Origin:
    United States of America

    Dimensions:
    Overall: 168 in. diameter (at the vanes) x 204 in. long x 36 in. diameter (booster) , 2400 lb. HOE and dolly (426.72 cm. x 518.16 cm. x 91.44 cm., 1088.6kg), HOE weight 1064 lbs

    Materials:
    Aluminum structure; internal electronics and metal components

    Lockheed built this unflown antiballistic missile (ABM) test vehicle for the U.S. Army's Homing Overlay Experiment (HOE). The HOE vehicle was designed to destroy a missile by physically impacting it - a concept known as "hit-to-kill." After separating from the booster, the vehicle would use its onboard sensors to identify and lock-on to the incoming missile and would use other components to direct it to impact. On the last of four HOE tests, a vehicle intercepted an incoming dummy warhead in the first successful demonstration of hit-to-kill technology in June 1984. The United States is now using much smaller hit-to-kill vehicles in deployed ABMs. Lockheed built this HOE test vehicle, and the U.S. Army transferred it to NASM in 1986.

    Transferred from the United States Army.

    • • • • •

    Quoting from Wikipedia | National Missile Defense: Homing Overlay Experiment:

    Given concerns about the previous programs using nuclear tipped interceptors, in the 1980s the U.S. Army began studies about the feasibility of hit-to-kill vehicles, where an interceptor missile would destroy an incoming ballistic missile just by colliding with it.

    The first program, which actually tested a hit-to-kill missile interceptor, was the Army's HOE (Homing Overlay Experiment) which used a Kinetic Kill Vehicle (KKV) . The KKV was equipped with an infrared seeker, guidance electronics and a propulsion system. Once in space, the KKV could extend a folded structure similar to an umbrella skeleton of 4 m (13 ft) diameter to enhance its effective cross section. This device would destroy the ICBM reentry vehicle on collision. After test failures with the first three flight tests, the fourth and final test on 10 June 1984 was successful, intercepting the Minuteman RV with a closing speed of about 6.1 km/s at an altitude of more than 160 km.
  • (I think this is one of the following (can't tell):

    Spartan 201 Satellite
    www.nasm.si.edu/collections/artifact.cfm?id=A20040121000

    New Horizons model
    www.nasm.si.edu/collections/artifact.cfm?id=A20080394000
  • Gemini Paraglider Research Vehicle 1-A with wing
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    Details, quoting from Smithsonian National Air and Space Museum | Manned Maneuvering Unit

    Manufacturer:
    Martin Marietta Aerospace

    Country of Origin:
    United States of America

    Dimensions:
    Overall: 4 ft. 2 in. tall x 2 ft. 9 5/16 in. wide x 2 ft. 4 in. deep (127 x 84.61 x 71.12cm)

    Materials:
    Aluminum structure; internal electronics and metal components

    The Manned Maneuvering Unit (MMU) is a backpack propulsion device that gave astronauts mobility for extravehicular activities outside the Space Shuttle. It enabled them to maneuver within the payload bay or fly some distance away without needing safety tethers anchored to the vehicle. The MMU had 24 small gaseous nitrogen thrusters and was operated with hand controllers on the arms of the unit.

    On February 7, 1984, on Space Shuttle mission STS 41-B, astronaut Bruce McCandless tested this MMU, serial number 3. He made the first untethered spacewalk as he flew some 300 feet from the Shuttle. This MMU also flew on missions STS 41-C as the backup unit for the Solar Max satellite retrieval and STS 51-A as the prime unit for retrieving the Palapa communications satellite. Astronauts Bruce McCandless, Robert Stewart, James van Hoften, and Joseph Allen flew MMU #3 a total of 6 hours 29 minutes during these three 1984 missions. The MMUs were not used again. NASA transferred this one to the Museum in 2001.

    Transferred from NASA Johnson Space Center, Houston, TX

    • • • • •

    Quoting from Wikipedia | Manned Maneuvering Unit:

    The Manned Maneuvering Unit (MMU) is an astronaut propulsion unit which was used by NASA on three space shuttle missions in 1984. The MMU allowed the astronauts to perform untethered EVA spacewalks at a distance from the shuttle. The MMU was used in practice to retrieve a pair of faulty communications satellites, Westar VI and Palapa B2. Following the third mission the unit was retired from use. A smaller successor, the Simplified Aid for EVA Rescue (SAFER), was first flown in 1994, and is intended for emergency use only.

    Overview

    The unit featured redundancy to protect against failure of individual systems. It was designed to fit over the life-support system backpack of the Space Shuttle Extravehicular Mobility Unit (EMU). When carried into space, the MMU was stowed in a support station attached to the wall of the payload bay near the airlock hatch. Two MMUs were carried on a mission, with the second unit mounted across from the first on the opposite payload bay wall. The MMU controller arms were folded for storage. When an astronaut backed into the unit and snapped the life-support system into place, the arms were unfolded.

    To adapt to astronauts with different arm lengths, controller arms could be adjusted over a range of approximately 13 centimetres. The MMU was small enough to be maneuvered with ease around and within complex structures. With a full propellant load, its mass was 148 kilograms (326 pounds).

    Gaseous nitrogen was used as the propellant for the MMU. Two aluminium tanks with Kevlar wrappings contained 5.9 kilograms of nitrogen each, enough propellant for a six-hour EVA depending on the amount of maneuvering done. Typical MMU delta-v (velocity change) capability was about 80 feet per second (24.4 meters/sec).

    There were 24 nozzle thrusters placed at different locations on the MMU. To operate the propulsion system, the astronaut used his fingertips to manipulate hand controllers at the ends of the MMU's two arms. The right controller produced rotational acceleration for roll, pitch, and yaw. The left controller produced translational acceleration for moving forward-back, up-down, and left-right. Coordination of the two controllers produced intricate movements in the unit. Once a desired orientation was achieved, the astronaut could engage an automatic attitude-hold function that maintained the inertial attitude of the unit in flight. This freed both hands for work.

    History

    In 1966, the US Air Force developed an Astronaut Maneuvering Unit (AMU), a self-contained rocket pack very similar to the MMU. This was planned to be tested during Project Gemini on an EVA by Eugene Cernan from Gemini 9A on June 5, 1966. But the test had to be cancelled because Cernan tired and overheated, sweatting so profusely that his helmet visor fogged, before he could get to the AMU mounted on the back of the spacecraft. Astronauts had not yet learned how to work during EVA without tiring, until the final Gemini 12 mission, but no AMU was carried on that flight. Since there was no real need for self-contained astronaut EVA flight in the Apollo and Skylab programs, the idea had to wait for the advent of the Space Shuttle program, though a maneuvering device was tested inside the Skylab.

    The MMU was used on three Shuttle missions in 1984. It was first tested on February 7 during mission STS-41-B by astronauts Bruce McCandless II and Robert L. Stewart. Two months later during mission STS-41-C, astronauts James van Hoften and George Nelson attempted to use the MMU to capture the Solar Maximum Mission satellite and to bring it into the orbiter's payload bay for repairs and servicing. The plan was to use an astronaut-piloted MMU to grapple the SMM with the Trunion Pin Attachment Device (TPAD) mounted between the hand controllers of the MMU, null its rotation rates, and allow the Shuttle to bring it into the Shuttle's payload bay for stowage. Three attempts to grapple the satellite using the TPAD failed. The TPAD jaws could not lock onto Solar Max because of an obstructing grommet on the satellite not included in the blueprints for the satellite. This led to an improvised plan which nearly ended the satellite's mission. The improvisation had the MMU astronaut use his hands to grab hold of an SMM solar array and null the rates by a push from MMU's thrusters. Instead, this attempt induced higher rates and in multiple axes; the satellite was tumbling out of control and quickly losing battery life. SMM Operations Control Center engineers shut down all non-essential SMM subsystems and with a bit of luck were able to recover the SMM minutes before total failure. The ground support engineers then stabilized the satellite and nulled its rotation rates for capture with the orbiter's robotic arm, the Shuttle Remote Manipulator System (SRMS). This proved to be a much better plan. Their successful work increased the lifespan of the satellite.

    The final MMU mission was STS-51-A, which flew in November 1984. The propulsion unit was used to retrieve two communication satellites, Westar VI and Palapa B2, that did not reach their proper orbits because of faulty propulsion modules. Astronauts Joseph P. Allen and Dale Gardner captured the two satellites and brought them into the Orbiter payload bay for stowage and return to Earth.

    After the Space Shuttle Challenger disaster, the MMU was judged too risky for further use. NASA also discontinued using the Shuttle for commercial satellite contracts, and the military discontinued the use of the Shuttle, eliminating the main potential uses. Although the MMU was envisioned as a natural aid for constructing the International Space Station, with its retirement, NASA developed different tethered spacewalk approaches. Additionally, the MMU gas ejecta was considered too damaging for the only other ongoing task, upkeep of the Hubble Space Telescope.[citation needed]

    NASA transferred the flight article #3 to the National Air and Space Museum in 1998.[1][2] The remaining MMU are stored at NASA (location not known).[citation needed]

    References

    ^ Collect Space - Full Coverage: Udvar-Hazy Space Hangar - October 26, 2004
    ^ Smithsonian National Air and Space Museum

    External links
    "More Favored than the Birds": The Manned Maneuvering Unit in Space
    NASA Manned maneuvering unit: User's guide - 1978 (PDF document)
    Assessment of the NASA Manned Maneuvering Unit - 1988 (PDF document)
    Interactive MMU
    Shuttle MMU
    Lockheed Martin - Manned Maneuvering Unit
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    Details, quoting from Smithsonian National Air and Space Museum | Apollo 11 Flotation Bags (3)

    Manufacturer:
    North American Rockwell

    Country of Origin:
    United States of America

    Dimensions:
    Overall: 3 ft. 8 in. diameter (111.76cm)

    Materials:
    Rubberized fabric

    When an Apollo command module landed in the ocean, it could settle into one of two stable positions: nose up or nose down. Landing nose down left its recovery antennas underwater and increased the possibility that the spacecraft might fill with sea water. To turn the command module upright, three inflatable bags were installed in the Command Module's forward (nose) compartment. Astronauts could right the spacecraft by activating air compressors in the aft (blunt) end of the spacecraft. The compressors were connected to the bags with tubing.

    This is one of three flotation bags used on Apollo 11 at the end of its historic lunar landing mission on July 24, 1969. The astronauts deployed it after the command module settled nose down, enabling the spacecraft to right itself about six and half minutes after splashdown.

    This object was transferred from NASA to the Smithsonian in 1973.

    Transferred from the National Aeronautics and Space Administration, through Rockwell International.
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    Details, quoting from Smithsonian National Air and Space Museum | Apollo 11 Flotation Collar

    Manufacturer:
    Naval Air Rework Facility

    Country of Origin:
    United States of America

    Dimensions:
    Deflated: 2ft 4in. width x 36ft length (71.12 x 1097.28cm)

    Materials:
    Overall: Rubber, stainless steel snaps, nylon webbing, rubber covered textile, steel cables, nylon rope

    Following the July 24, 1969 splashdown of the Apollo 11 Command Module in the mid-Pacific ocean, about 13 nautical miles from the prime recovery ship, USS HORNET, a recovery helicopter dropped Navy swimmers into the water. The swimmer's first task was to stabilize the command module by attaching and inflating a custom-made flotation collar around the blunt end of the spacecraft. The next task was to attach a large, seven-man raft to the flotation collar into which the astronauts, after donning special "Biological Isolation Garments," exited from the Command Module. After further decontamination, the astronauts were flown by Navy Helicopter to the HORNET.

    This collar attached to the "egress trainer" command module is the actual unit deployed during the recovery of Apollo 11. It was transferred from NASA to the Smithsonian in 1977.

    Transferred from the National Aeronautics and Space Administration, Johnson Space Center.
  • Saturn V Instrument Ring
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Steven F. Udvar-Hazy Center: Space exhibit panorama (hang glider, Space Shuttle Enterprise)

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Details, quoting from Smithsonian National Air and Space Museum | Space Shuttle Enterprise:

Manufacturer:
Rockwell International Corporation

Country of Origin:
United States of America

Dimensions:
Overall: 57 ft. tall x 122 ft. long x 78 ft. wing span, 150,000 lb.
(1737.36 x 3718.57 x 2377.44cm, 68039.6kg)

Materials:
Aluminum airframe and body with some fiberglass features; payload bay doors are graphite epoxy composite; thermal tiles are simulated (polyurethane foam) except for test samples of actual tiles and thermal blankets.

The first Space Shuttle orbiter, "Enterprise," is a full-scale test vehicle used for flights in the atmosphere and tests on the ground; it is not equipped for spaceflight. Although the airframe and flight control elements are like those of the Shuttles flown in space, this vehicle has no propulsion system and only simulated thermal tiles because these features were not needed for atmospheric and ground tests. "Enterprise" was rolled out at Rockwell International's assembly facility in Palmdale, California, in 1976. In 1977, it entered service for a nine-month-long approach-and-landing test flight program. Thereafter it was used for vibration tests and fit checks at NASA centers, and it also appeared in the 1983 Paris Air Show and the 1984 World's Fair in New Orleans. In 1985, NASA transferred "Enterprise" to the Smithsonian Institution's National Air and Space Museum.

Transferred from National Aeronautics and Space Administration

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Quoting from Wikipedia | Space Shuttle Enterprise:

The Space Shuttle Enterprise (NASA Orbiter Vehicle Designation: OV-101) was the first Space Shuttle orbiter. It was built for NASA as part of the Space Shuttle program to perform test flights in the atmosphere. It was constructed withoutengines or a functional heat shield, and was therefore not capable of spaceflight.

Originally, Enterprise had been intended to be refitted for orbital flight, which would have made it the second space shuttle to fly after Columbia. However, during the construction of Columbia, details of the final design changed, particularly with regard to the weight of the fuselage and wings. Refitting Enterprise for spaceflight would have involved dismantling the orbiter and returning the sections to subcontractors across the country. As this was an expensive proposition, it was determined to be less costly to build Challenger around a body frame (STA-099) that had been created as a test article. Similarly, Enterprise was considered for refit to replace Challenger after the latter was destroyed, but Endeavour was built from structural spares instead.

Service

Construction began on the first orbiter on June 4, 1974. Designated OV-101, it was originally planned to be named Constitution and unveiled on Constitution Day, September 17, 1976. A write-in campaign by Trekkies to President Gerald Ford asked that the orbiter be named after the Starship Enterprise, featured on the television show Star Trek. Although Ford did not mention the campaign, the president—who during World War II had served on the aircraft carrier USS Monterey (CVL-26) that served with USS Enterprise (CV-6)—said that he was "partial to the name" and overrode NASA officials.

The design of OV-101 was not the same as that planned for OV-102, the first flight model; the tail was constructed differently, and it did not have the interfaces to mount OMS pods. A large number of subsystems—ranging from main engines to radar equipment—were not installed on this vehicle, but the capacity to add them in the future was retained. Instead of a thermal protection system, its surface was primarily fiberglass.

In mid-1976, the orbiter was used for ground vibration tests, allowing engineers to compare data from an actual flight vehicle with theoretical models.

On September 17, 1976, Enterprise was rolled out of Rockwell's plant at Palmdale, California. In recognition of its fictional namesake, Star Trek creator Gene Roddenberry and most of the principal cast of the original series of Star Trek were on hand at the dedication ceremony.

Approach and landing tests (ALT)

Main article: Approach and Landing Tests

On January 31, 1977, it was taken by road to Dryden Flight Research Center at Edwards Air Force Base, to begin operational testing.

While at NASA Dryden, Enterprise was used by NASA for a variety of ground and flight tests intended to validate aspects of the shuttle program. The initial nine-month testing period was referred to by the acronym ALT, for "Approach and Landing Test". These tests included a maiden "flight" on February 18, 1977 atop a Boeing 747 Shuttle Carrier Aircraft (SCA) to measure structural loads and ground handling and braking characteristics of the mated system. Ground tests of all orbiter subsystems were carried out to verify functionality prior to atmospheric flight.

The mated Enterprise/SCA combination was then subjected to five test flights with Enterprise unmanned and unactivated. The purpose of these test flights was to measure the flight characteristics of the mated combination. These tests were followed with three test flights with Enterprise manned to test the shuttle flight control systems.

Enterprise underwent five free flights where the craft separated from the SCA and was landed under astronaut control. These tests verified the flight characteristics of the orbiter design and were carried out under several aerodynamic and weight configurations. On the fifth and final glider flight, pilot-induced oscillation problems were revealed, which had to be addressed before the first orbital launch occurred.

On August 12, 1977, the space shuttle Enterprise flew on its own for the first time.

Preparation for STS-1

Following the ALT program, Enterprise was ferried among several NASA facilities to configure the craft for vibration testing. In June 1979, it was mated with an external tank and solid rocket boosters (known as a boilerplate configuration) and tested in a launch configuration at Kennedy Space Center Launch Pad 39A.

Retirement

With the completion of critical testing, Enterprise was partially disassembled to allow certain components to be reused in other shuttles, then underwent an international tour visiting France, Germany, Italy, the United Kingdom, Canada, and the U.S. states of California, Alabama, and Louisiana (during the 1984 Louisiana World Exposition). It was also used to fit-check the never-used shuttle launch pad at Vandenberg AFB, California. Finally, on November 18, 1985, Enterprise was ferried to Washington, D.C., where it became property of the Smithsonian Institution.

Post-Challenger

After the Challenger disaster, NASA considered using Enterprise as a replacement. However refitting the shuttle with all of the necessary equipment needed for it to be used in space was considered, but instead it was decided to use spares constructed at the same time as Discovery and Atlantis to build Endeavour.

Post-Columbia

In 2003, after the breakup of Columbia during re-entry, the Columbia Accident Investigation Board conducted tests at Southwest Research Institute, which used an air gun to shoot foam blocks of similar size, mass and speed to that which struck Columbia at a test structure which mechanically replicated the orbiter wing leading edge. They removed a fiberglass panel from Enterprise's wing to perform analysis of the material and attached it to the test structure, then shot a foam block at it. While the panel was not broken as a result of the test, the impact was enough to permanently deform a seal. As the reinforced carbon-carbon (RCC) panel on Columbia was 2.5 times weaker, this suggested that the RCC leading edge would have been shattered. Additional tests on the fiberglass were canceled in order not to risk damaging the test apparatus, and a panel from Discovery was tested to determine the effects of the foam on a similarly-aged RCC leading edge. On July 7, 2003, a foam impact test created a hole 41 cm by 42.5 cm (16.1 inches by 16.7 inches) in the protective RCC panel. The tests clearly demonstrated that a foam impact of the type Columbia sustained could seriously breach the protective RCC panels on the wing leading edge.

The board determined that the probable cause of the accident was that the foam impact caused a breach of a reinforced carbon-carbon panel along the leading edge of Columbia's left wing, allowing hot gases generated during re-entry to enter the wing and cause structural collapse. This caused Columbia to spin out of control, breaking up with the loss of the entire crew.

Museum exhibit

Enterprise was stored at the Smithsonian's hangar at Washington Dulles International Airport before it was restored and moved to the newly built Smithsonian's National Air and Space Museum's Steven F. Udvar-Hazy Center at Dulles International Airport, where it has been the centerpiece of the space collection. On April 12, 2011, NASA announced that Space Shuttle Discovery, the most traveled orbiter in the fleet, will be added to the collection once the Shuttle fleet is retired. When that happens, Enterprise will be moved to the Intrepid Sea-Air-Space Museum in New York City, to a newly constructed hangar adjacent to the museum. In preparation for the anticipated relocation, engineers evaluated the vehicle in early 2010 and determined that it was safe to fly on the Shuttle Carrier Aircraft once again.

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