The BYEMAN Control System , or simply BYEMAN (designated BYE , or B ), was a security control system put in place to protect information about the National Reconnaissance Office and its operations.
77-466: The KH-8 ( BYEMAN codename Gambit-3 ) was a long-lived series of reconnaissance satellites of the " Key Hole " (KH) series used by the United States from July 1966 to April 1984, and also known as Low Altitude Surveillance Platform. The satellite ejected "film-bucket" canisters of photographic film that were retrieved as they descended through the atmosphere by parachute . Ground resolution of
154-420: A Gemini capsule on a Titan II-C , the latter being much less expensive in the case where cargo was not needed. Proposals ranged from an Apollo-based station with two to three men, or a small "canister" for four men with Gemini capsules resupplying it, to a large, rotating station with 24 men and an operating lifetime of about five years. A proposal to study the use of a Saturn S-IVB as a crewed space laboratory
231-441: A dart set , playing cards , and other recreational equipment in addition to books and music players, the window with its view of Earth became the most popular way to relax in orbit. Prior to departure about 80 experiments were named, although they are also described as "almost 300 separate investigations". Experiments were divided into six broad categories: Because the solar scientific airlock – one of two research airlocks –
308-552: A solar observatory , Earth observation and hundreds of experiments . Skylab's orbit eventually decayed and it disintegrated in the atmosphere on July 11, 1979, scattering debris across the Indian Ocean and Western Australia . As of 2024, Skylab was the only space station operated exclusively by the United States. A permanent station was planned starting in 1988, but its funding was canceled and U.S. participation shifted to
385-447: A " wet workshop " concept, because of the conversion of an active fuel tank. The station filled the entire interior of the S-II stage's hydrogen tank, with the equipment section forming a "spine" and living quarters located between it and the walls of the booster. This would have resulted in a very large 33 by 45 feet (10 by 14 m) living area. Power was to be provided by solar cells lining
462-466: A Saturn IB rocket from Launch Pad 39B. Skylab 1 was the last uncrewed launch from LC-39A until February 19, 2017, when SpaceX CRS-10 was launched from there. Three crewed missions, designated Skylab 2 , Skylab 3 , and Skylab 4 , were made to Skylab in the Apollo command and service modules . The first crewed mission, Skylab 2, launched on May 25, 1973, atop a Saturn IB and involved extensive repairs to
539-452: A film with a resolving power equivalent to the Kodak's Type 3409 film of 320 to 630 line pairs per mm, GAMBIT would have been able to record ground features as small as 5 cm to 10 cm (2" to 4"). The initial September 2011 release of "The Gambit Story" quotes "The mature system produced examples of imagery better than four inches ground-resolution distance". This number was again redacted in
616-476: A handful of websites were set up to direct users through the retirement process. An individual inside the CIA's Special Security Center chose the name from a random list of four words drawn from the CIA's codeword file. A byeman is a man who works underground; it is unknown if the individual knew the word's meaning before its selection. This is a small list of the publicly acknowledged programs that were held within
693-420: A large, circular station 250 feet (75 m) in diameter that would rotate to generate artificial gravity and require a fleet of 7,000 short tons (6,400 metric tons) space shuttles for construction in orbit. The 80 men aboard the station would include astronomers operating a telescope, meteorologists to forecast the weather, and soldiers to conduct surveillance. Von Braun expected that future expeditions to
770-473: A later release. Five to ten centimeters corresponds to the resolution limit imposed by atmospheric turbulence as derived by Fried and, independently, Evvard in the mid-1960s; remarkably, GAMBIT had reached a physical limit on resolution only a few years after the US launched its first reconnaissance satellite. GAMBIT was also able to record objects in orbit. The capability was developed to photograph Soviet spacecraft, but
847-619: A mission mode that would not need in-orbit assembly. A smaller station that a single rocket could launch retained value, however, for scientific purposes. In 1959, von Braun, head of the Development Operations Division at the Army Ballistic Missile Agency , submitted his final Project Horizon plans to the U.S. Army . The overall goal of Horizon was to place men on the Moon, a mission that would soon be taken over by
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#1733086312242924-487: A misspelling of the word, (i.e. "BYMAN") is used on a cover sheet protecting photos of the incoming asteroid. (the correct spelling, BYEMAN, was still classified " Confidential " at that time.) Skylab Skylab was the United States' first space station , launched by NASA , occupied for about 24 weeks between May 1973 and February 1974. It was operated by three trios of astronaut crews: Skylab 2 , Skylab 3 , and Skylab 4 . Operations included an orbital workshop,
1001-465: A multiple docking adapter with two docking ports, an airlock module with extravehicular activity (EVA) hatches, and the orbital workshop, the main habitable space inside Skylab. Electrical power came from solar arrays and fuel cells in the docked Apollo CSM. The rear of the station included a large waste tank, propellant tanks for maneuvering jets, and a heat radiator. Astronauts conducted numerous experiments aboard Skylab during its operational life. For
1078-585: A private area the size of a small walk-in closet , with a curtain, sleeping bag, and locker. Designers also added a shower and a toilet for comfort and to obtain precise urine and feces samples for examination on Earth. The waste samples were so important that they would have been priorities in any rescue mission . Skylab did not have recycling systems such as the conversion of urine to drinking water; it also did not dispose of waste by dumping it into space. The S-IVB's 73,280 liters (16,120 imp gal; 19,360 U.S. gal) liquid oxygen tank below
1155-535: A replacement heat shade and freed the jammed solar panels to save Skylab. This was the first time that a repair of this magnitude was performed in space. The Apollo Telescope significantly advanced solar science, and observation of the Sun was unprecedented. Astronauts took thousands of photographs of Earth, and the Earth Resources Experiment Package (EREP) viewed Earth with sensors that recorded data in
1232-732: A result of a NASA contest. The actual stage that flew was the upper stage of the AS-212 rocket (the S-IVB stage, S-IVB 212). The mission computer used aboard Skylab was the IBM System/4Pi TC-1, a relative of the AP-101 Space Shuttle computers. The Saturn V with serial number SA-513, originally produced for the Apollo program – before the cancellation of Apollo 18, 19, and 20 – was repurposed and redesigned to launch Skylab. The Saturn V's third stage
1309-580: A series of films with silver-halide crystals of very uniform size and shape. The size of silver-halide crystals decreased from 1,550 angstrom in film Type SO-315, to 1,200 angstrom in SO-312, and ultimately to 900 angstrom in SO-409. Under optimal conditions GAMBIT would thus have been able to record ground features as small as 0.28 to 0.56 m (0.92 to 1.84 ft) using the Eastman Kodak Type 3404 film. Using
1386-557: A shower once a week, but found drying themselves in weightlessness and vacuuming excess water difficult; later crews usually cleaned themselves daily with wet washcloths instead of using the shower. Astronauts also found that bending over in weightlessness to put on socks or tie shoelaces strained their abdominal muscles. Breakfast began at 7 a.m. Astronauts usually stood to eat, as sitting in microgravity also strained their abdominal muscles. They reported that their food – although greatly improved from Apollo –
1463-425: A single Gambit Block 3 mission was operated in 'dual-mode', orbiting first at a higher altitude to capture wide-area search imagery before lowering its perigee to capture normal surveillance imagery. The first film return capsule failed to separate correctly due to a new pyro mechanism failing to perform correctly. The contingency release mechanism separated the film bucket and parachute from its return capsule, and left
1540-492: A system that help detect and control the orientation of the station in space. Other sensors that helped with this were a Sun tracker and a star tracker . The sensors fed data to the main computer, which could then use the control gyroscopes and or the thruster system to keep Skylab pointed as desired. Skylab had a zero-gravity shower system in the work and experiment section of the Orbital Workshop designed and built at
1617-536: A two-person crew. The station was the same diameter as a Titan II upper stage , and would be launched with the crew riding atop in a modified Gemini capsule with a hatch cut into the heat shield on the bottom of the capsule. MOL competed for funding with a NASA station for the next five years and politicians and other officials often suggested that NASA participate in MOL or use the DoD design. The military project led to changes to
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#17330863122421694-672: A variety of LM or CSM-based hardware. Although it did not look at the space station specifically, over the next two years the office would become increasingly dedicated to this role. In August 1965, the office was renamed, becoming the Apollo Applications Program (AAP). As part of their general work, in August 1964 the Manned Spacecraft Center (MSC) presented studies on an expendable lab known as Apollo X , short for Apollo Extension System . Apollo X would have replaced
1771-407: Is a single strip camera, designed to gather high-resolution images of ground targets. In the strip camera the ground image is reflected by a steerable flat mirror to a 1.21 m (48 in) diameter stationary concave primary mirror. The primary mirror reflects the light through an opening in the flat mirror and through a Ross corrector . At periapsis altitude of 75 nautical miles (139 km),
1848-581: The Apollo Logistic Support System Office , originally intended to study various ways to modify the Apollo hardware for scientific missions. The office initially proposed a number of projects for direct scientific study, including an extended-stay lunar mission which required two Saturn V launchers, a "lunar truck" based on the Lunar Module (LM), a large, crewed solar telescope using an LM as its crew quarters, and small space stations using
1925-546: The International Space Station in 1993. Skylab had a mass of 199,750 pounds (90,610 kg) with a 31,000-pound (14,000 kg) Apollo command and service module (CSM) attached and included a workshop, a solar observatory, and several hundred life science and physical science experiments. It was launched uncrewed into low Earth orbit by a Saturn V rocket modified to be similar to the Saturn INT-21 , with
2002-481: The Manned Spaceflight Center . It had a cylindrical curtain that went from floor to ceiling and a vacuum system to suck away water. The floor of the shower had foot restraints. To bathe, the user coupled a pressurized bottle of warmed water to the shower's plumbing, then stepped inside and secured the curtain. A push-button shower nozzle was connected by a stiff hose to the top of the shower. The system
2079-516: The Moon and Mars would leave from the station. The development of the transistor , the solar cell , and telemetry , led in the 1950s and early 1960s to uncrewed satellites that could take photographs of weather patterns or enemy nuclear weapons and send them to Earth. A large station was no longer necessary for such purposes, and the United States Apollo program to send men to the Moon chose
2156-665: The Multiple Docking Adapter , mainly because the structure could not carry enough weight for a single larger film vault. The orbital workshop could handle a single larger safe, which is also more efficient for shielding. A later example of a radiation vault is the Juno Radiation Vault for the Juno Jupiter orbiter, launched in 2011, which was designed to protect much of the uncrewed spacecraft's electronics, using 1 cm thick walls of titanium . The large vault in
2233-510: The S-II second stage of a Saturn V. His design replaced the S-IVB third stage with an aeroshell, primarily as an adapter for the CSM on top. Inside the shell was a 10 feet (3.0 m) cylindrical equipment section. On reaching orbit, the S-II second stage would be vented to remove any remaining hydrogen fuel, then the equipment section would be slid into it via a large inspection hatch. This became known as
2310-587: The S-IVB third stage not available for propulsion because the orbital workshop was built out of it. This was the final flight for the rocket more commonly known for carrying the crewed Apollo Moon landing missions. Three subsequent missions delivered three-astronaut crews in the Apollo CSM launched by the smaller Saturn IB rocket. Skylab included the Apollo Telescope Mount (a multi-spectral solar observatory),
2387-680: The visible , infrared , and microwave spectral regions. The record for human time spent in orbit was extended beyond the 23 days set by the Soyuz 11 crew aboard Salyut 1 to 84 days by the Skylab 4 crew. Later plans to reuse Skylab were stymied by delays in the development of the Space Shuttle, and Skylab's decaying orbit could not be stopped. Skylab's atmospheric reentry began on July 11, 1979, amid worldwide media attention. Before re-entry, NASA ground controllers tried to adjust Skylab's orbit to minimize
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2464-584: The AAP program. Although this would have allowed them to develop von Braun's original S-II-based mission, by this time so much work had been done on the S-IV-based design that work continued on this baseline. With the extra power available, the wet workshop was no longer needed; the S-IC and S-II lower stages could launch a "dry workshop", with its interior already prepared, directly into orbit. A dry workshop simplified plans for
2541-467: The Apollo Telescope Mount, and to resist various forces that can change the station's orientation. Some of the forces acting on Skylab that the pointing system needed to resist: The Skylab-A attitude and pointing control system has been developed to meet the high accuracy requirements established by the desired experiment conditions. Conditions must be maintained by the control system under
2618-625: The BCS: While many other NRO programs resided within the BCS, their codenames have not been made public through proper disclosure or official declassification. By order of the Director of Central Intelligence (DCI), BYEMAN was retired on 20 May 2005. Most information held within the BCS was transitioned into the Talent Keyhole Control System. In the 1998 blockbuster movie Armageddon ,
2695-459: The LM carried on the top of the S-IVB stage with a small space station slightly larger than the CSM's service area, containing supplies and experiments for missions between 15 and 45 days' duration. Using this study as a baseline, a number of different mission profiles were looked at over the next six months. In November 1964, von Braun proposed a more ambitious plan to build a much larger station built from
2772-585: The NASA plans so that they would resemble MOL less. NASA management was concerned about losing the 400,000 workers involved in Apollo after landing on the Moon in 1969. A reason von Braun, head of NASA's Marshall Space Flight Center during the 1960s, advocated a smaller station after his large one was not built was that he wished to provide his employees with work beyond developing the Saturn rockets, which would be completed relatively early during Project Apollo. NASA set up
2849-707: The Orbital Work Shop was used to store trash and wastewater, passed through an airlock . On August 8, 1969, the McDonnell Douglas Corporation received a contract for the conversion of two existing S-IVB stages to the Orbital Workshop configuration. One of the S-IV test stages was shipped to McDonnell Douglas for the construction of a mock-up in January 1970. The Orbital Workshop was renamed "Skylab" in February 1970 as
2926-467: The Orbital Workshop would be launched as a part of Apollo mission AS-209, originally one of the Earth-orbit CSM test launches, followed by two Saturn I/CSM crew launches, AAP-1 and AAP-2. The Manned Orbiting Laboratory (MOL) remained AAP's chief competitor for funds, although the two programs cooperated on technology. NASA considered flying experiments on MOL or using its Titan IIIC booster instead of
3003-408: The S-IV stage, before it was replaced by the S-IVB. On April 1, 1966, MSC sent out contracts to Douglas, Grumman , and McDonnell for the conversion of an S-IVB spent stage, under the name Saturn S-IVB spent-stage experiment support module (SSESM). In May 1966, astronauts voiced concerns over the purging of the stage's hydrogen tank in space. Nevertheless, in late July 1966, it was announced that
3080-626: The Skylab digital computer. Two of three were active and their input was averaged, while the third was a backup. From NASA SP-400 Skylab, Our First Space Station , "each Skylab control-moment gyroscope consisted of a motor-driven rotor, electronics assembly, and power inverter assembly. The 21-inch-diameter (530 mm) rotor weighed 155 pounds (70 kg) and rotated at approximately 8950 revolutions per minute". There were three control moment gyroscopes on Skylab, but only two were required to maintain pointing. The control and sensor gyroscopes were part of
3157-499: The Skylab missions would last for months. NASA sent a scientist on Jacques Piccard 's Ben Franklin submarine in the Gulf Stream in July and August 1969 to learn how six people would live in an enclosed space for four weeks. Astronauts were uninterested in watching movies on a proposed entertainment center or in playing games, but they did want books and individual music choices. Food
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3234-659: The Soviet Soyuz 11 crew aboard the space station Salyut 1 on June 30, 1971. Skylab 2 lasted 28 days, Skylab 3 – 56 days, and Skylab 4 – 84 days. Astronauts performed ten spacewalks, totaling 42 hours and 16 minutes. Skylab logged about 2,000 hours of scientific and medical experiments, 127,000 frames of film of the Sun and 46,000 of Earth. Solar experiments included photographs of eight solar flares and produced valuable results that scientists stated would have been impossible to obtain with uncrewed spacecraft. The existence of
3311-513: The Sun's coronal holes was confirmed because of these efforts. Many of the experiments conducted investigated the astronauts' adaptation to extended periods of microgravity . A typical day began at 6 a.m. Central Time Zone . Although the toilet was small and noisy, both veteran astronauts – who had endured earlier missions' rudimentary waste-collection systems – and rookies complimented it. The first crew enjoyed taking
3388-736: The agency announced that the lunar mapping and base construction missions examined by the AAP were being canceled. Only the Earth-orbiting missions remained, namely the Orbital Workshop and Apollo Telescope Mount solar observatory . The success of Apollo 8 in December 1968, launched on the third flight of a Saturn V, made it likely that one would be available to launch a dry workshop. Later, several Moon missions were canceled as well, originally to be Apollo missions 18 through 20 . The cancellation of these missions freed up three Saturn V boosters for
3465-586: The atmosphere. A few months later, pieces of the satellite turned up in England and the US managed to arrange for their hasty return. The third failure was satellite #39 on June 26, 1973, which suffered a stuck Agena fuel valve. The Bell 8096 engine failed to start and the satellite burned up in the atmosphere. The KH-8 was manufactured by Lockheed . The camera system/satellite was manufactured by Eastman Kodak 's A&O Division in Rochester, New York . The Gambit codename
3542-470: The birth of X-ray astronomy . Skylab had certain features to protect vulnerable technology from radiation . The window was vulnerable to darkening, and this darkening could affect experiment S190. As a result, a light shield that could be open or shut was designed and installed on Skylab. To protect a wide variety of films, used for a variety of experiments and for astronaut photography , there were five film vaults. There were four smaller film vaults in
3619-465: The environment and established comfortable working relationships with ground control. The figure (below) lists an overview of most major experiments. Skylab 4 carried out several more experiments, such as to observe Comet Kohoutek . Riccardo Giacconi shared the 2002 Nobel Prize in Physics for his study of X-ray astronomy , including the study of emissions from the Sun onboard Skylab, contributing to
3696-470: The film bucket stranded in orbit. In September 2002, the film bucket re-entered over the South Atlantic into deep water. As the film bucket lacked its protective heatshield or the parachute needed to slow its descent, no attempt was made to recover it. The Camera Optics Module of KH-8 consists of four cameras. The main camera of KH-8B (introduced in 1971) with a focal length of 175.6 in (4.46 m)
3773-516: The final two crewed missions to Skylab, NASA assembled a backup Apollo CSM/Saturn IB in case an in-orbit rescue mission was needed, but this vehicle was never flown. The station was damaged during launch when the micrometeoroid shield tore away from the workshop, taking one of the main solar panel arrays with it and jamming the other main array. This deprived Skylab of most of its electrical power and also removed protection from intense solar heating, threatening to make it unusable. The first crew deployed
3850-404: The heaviest items that had to be returned at the end of each mission. The heaviest canisters weighed 40 kg and could hold up to 16,000 frames of film. There were two types of gyroscopes on Skylab. Control-moment gyroscopes (CMG) could physically move the station, and rate gyroscopes measured the rate of rotation to find its orientation. The CMG helped provide the fine pointing needed by
3927-518: The idea of building a smaller "wet workshop" based on the S-IVB, launched as the second stage of a Saturn IB. A number of S-IVB-based stations were studied at MSC from mid-1965, which had much in common with the Skylab design that eventually flew. An airlock would be attached to the hydrogen tank, in the area designed to hold the LM , and a minimum amount of equipment would be installed in the tank itself in order to avoid taking up too much fuel volume. Floors of
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#17330863122424004-546: The influence of external and internal disturbance torques, such as gravity gradient and aerodynamic disturbances and onboard astronaut motion. Skylab was the first large spacecraft to use big gyroscopes, capable of controlling its attitude. The control could also be used to help point the instruments. The gyroscopes took about ten hours to get spun up if they were turned off. There was also a thruster system to control Skylab's attitude. There were 9 rate-gyroscope sensors, 3 for each axis. These were sensors that fed their output to
4081-472: The interior of the station. Industrial design firm Raymond Loewy /William Snaith recommended emphasizing habitability and comfort for the astronauts by providing a wardroom for meals and relaxation and a window to view Earth and space, although astronauts were dubious about the designers' focus on details such as color schemes. Habitability had not previously been an area of concern when building spacecraft due to their small size and brief mission durations, but
4158-524: The launch dates of July 28, 1973, (Skylab 3) and November 16, 1973, (Skylab 4), and mission durations of 59 and 84 days, respectively. The last Skylab crew returned to Earth on February 8, 1974. In addition to the three crewed missions, there was a rescue mission on standby that had a crew of two, but could take five back down. Also of note was the three-man crew of Skylab Medical Experiment Altitude Test (SMEAT), who spent 56 days in 1972 at low-pressure on Earth to evaluate medical experiment equipment. This
4235-511: The lost micrometeoroid shield further complicated matters by becoming tangled in the remaining solar panel, preventing its full deployment and thus leaving the station with a huge power deficit. Immediately following Skylab's launch, Pad 39A at Kennedy Space Center was deactivated, and construction proceeded to modify it for the Space Shuttle program, originally targeting a maiden launch in March 1979 . The crewed missions to Skylab would occur using
4312-467: The main camera imaged a 6.3 km wide ground swath on a 8.811 in (223.8 mm) wide moving portion of film through a small slit aperture, resulting in an image scale of 28 meter / millimeter. The Astro-Position Terrain Camera (APTC) contains three cameras: a 75mm focal length terrain frame camera, and two 90mm focal length stellar cameras. The terrain frame camera takes exposures of Earth in direction of
4389-651: The mature satellite system was better than 4 inches (0.10 m). There were 54 launch attempts of the 3,000 kilogram satellites, all from Vandenberg Air Force Base , on variants of the Titan III rocket. Three launches failed to achieve orbit. The first one was satellite #5 on April 26, 1967, which fell into the Pacific Ocean after the Titan second stage developed low thrust. The second was satellite #35 on May 20, 1972, which suffered an Agena pneumatic regulator failure and reentered
4466-549: The much more expensive Saturn IB. The agency decided that the Air Force station was not large enough and that converting Apollo hardware for use with Titan would be too slow and too expensive. The DoD later canceled MOL in June 1969. Design work continued over the next two years, in an era of shrinking budgets. (NASA sought US$ 450 million for Apollo Applications in fiscal year 1967, for example, but received US$ 42 million.) In August 1967,
4543-487: The orbital workshop had an empty mass of 2,398 pounds (1,088 kg). The four smaller vaults had combined mass of 1,545 lb (701 kg). The primary construction material of all five safes was aluminum. When Skylab re-entered there was one 180 pounds (82 kg) chunk of aluminum found that was thought to be a door to one of the film vaults. The large film vault was one of the heaviest single pieces of Skylab to re-enter Earth's atmosphere . The Skylab film vault
4620-445: The outside of the S-II stage. One problem with this proposal was that it required a dedicated Saturn V launch to fly the station. At the time the design was being proposed, it was not known how many of the then-contracted Saturn Vs would be required to achieve a successful Moon landing. However, several planned Earth-orbit test missions for the LM and CSM had been canceled, leaving a number of Saturn IBs free for use. Further work led to
4697-420: The rapidly forming NASA. Although concentrating on the Moon missions, von Braun also detailed an orbiting laboratory built out of a Horizon upper stage, an idea used for Skylab. A number of NASA centers studied various space station designs in the early 1960s. Studies generally looked at platforms launched by the Saturn V, followed up by crews launched on Saturn IB using an Apollo command and service module , or
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#17330863122424774-461: The risk of debris landing in populated areas, targeting the south Indian Ocean, which was partially successful. Debris showered Western Australia , and recovered pieces indicated that the station had disintegrated lower than expected. As the Skylab program drew to a close, NASA's focus had shifted to the development of the Space Shuttle. NASA space station and laboratory projects included Spacelab , Shuttle- Mir , and Space Station Freedom , which
4851-453: The station would be made from an open metal framework that allowed the fuel to flow through it. After launch, a follow-up mission launched by a Saturn IB would launch additional equipment, including solar panels, an equipment section and docking adapter, and various experiments. Douglas Aircraft Company , builder of the S-IVB stage, was asked to prepare proposals along these lines. The company had for several years been proposing stations based on
4928-661: The station. The crew deployed a parasol-like sunshade through a small instrument port from the inside of the station, bringing station temperatures down to acceptable levels and preventing overheating that would have melted the plastic insulation inside the station and released poisonous gases. This solution was designed by Jack Kinzler , who won the NASA Distinguished Service Medal for his efforts. The crew conducted further repairs via two spacewalks ( extravehicular activity or EVA). The crew stayed in orbit with Skylab for 28 days. Two additional missions followed, with
5005-463: The vehicle roll position for attitude determination. The stellar cameras observed in 180 degree opposite directions and took images of star fields. The films used by GAMBIT were provided by Eastman Kodak , and evolved through a series of successively higher definition films, starting with Type 3404 with a resolving power of 50 to 100 line pairs per mm . Subsequent films used were Type 1414 high-definition film, SO-217 high-definition fine-grain film, and
5082-469: The water tank. After dinner, which was scheduled for 6 p.m., crews performed household chores and prepared for the next day's experiments. Following lengthy daily instructions (some of which were up to 15 meters long) sent via teleprinter , the crews were often busy enough to postpone sleep. The station offered what a later study called "a highly satisfactory living and working environment for crews", with enough room for personal privacy. Although it had
5159-477: Was a spaceflight analog test in full gravity, but Skylab hardware was tested and medical knowledge was gained. Originally intended to be visited by one 28–day and two 56–day missions for a total of 140 days, Skylab was ultimately occupied for 171 days and 13 hours during its three crewed expeditions, orbiting the Earth 2,476 times. Each of these extended the human record of 23 days for amount of time spent in space set by
5236-400: Was also important; early Apollo crews complained about its quality, and a NASA volunteer found it intolerable to live on the Apollo food for four days on Earth. Its taste and composition were unpleasant, in the form of cubes and squeeze tubes. Skylab food significantly improved on its predecessors by prioritizing palatability over scientific needs. For sleeping in space , each astronaut had
5313-570: Was also used by the satellite's predecessor, the KH-7 Gambit . Gambit 3 satellites were the same width as the Gambit 1 models, but also slightly longer – reaching about 29 feet (8.8 m) in length. They carried 12,241 feet (3,731 meters) of film and were designed for longer missions of up to 31 days. While Gambit was primarily designed and operated as a surveillance satellite, capturing high definition images of specific targets at low orbital altitudes,
5390-408: Was bland and repetitive, and weightlessness caused utensils, food containers, and bits of food to float away; also, gas in their drinking water contributed to flatulence . After breakfast and preparation for lunch, experiments, tests and repairs of spacecraft systems and, if possible, 90 minutes of physical exercise followed; the station had a bicycle and other equipment, and astronauts could jog around
5467-519: Was documented in 1962 by the Douglas Aircraft Company . The Department of Defense (DoD) and NASA cooperated closely in many areas of space. In September 1963, NASA and the DoD agreed to cooperate in building a space station. The DoD wanted its own crewed facility, however, and in December 1963 it announced Manned Orbital Laboratory (MOL), a small space station primarily intended for photo reconnaissance using large telescopes directed by
5544-511: Was first used to aid NASA engineers designing repairs for the damaged Skylab space station in 1973. (NSSDC ID Numbers: See COSPAR ) In May 1973 Gambit KH8-38 was used to observe the crippled Skylab space station, as part of the preparation for repairing it by the Skylab 2 mission. The total cost of the 54 flight KH-8 program from FY1964 to FY1985, without non-recurring costs, was US$ 2.3 billion in respective year dollars. Byeman Control System The BYEMAN Control System (BCS)
5621-576: Was merged into the International Space Station. Rocket engineer Wernher von Braun , science fiction writer Arthur C. Clarke , and other early advocates of crewed space travel, expected until the 1960s that a space station would be an important early step in space exploration. Von Braun participated in the publishing of a series of influential articles in Collier's magazine from 1952 to 1954, titled " Man Will Conquer Space Soon! ". He envisioned
5698-540: Was put in place in 1961 by the Central Intelligence Agency . Discussions regarding BCS retirement were held as early as 2003. NRO Director Peter B. Teets spoke at a 2003 NRO Town Hall meeting, mentioning that retiring the BCS would remove barriers that prevented the NRO and U.S. Intelligence Community from working together as a team. The use of BCS was so prevalent throughout the U.S. Intelligence Community, that
5775-406: Was removed and replaced with Skylab, but with the controlling Instrument Unit remaining in its standard position. Skylab was launched on May 14, 1973, by the modified Saturn V. The launch is sometimes referred to as Skylab 1. Severe damage was sustained during launch and deployment, including the loss of the station's micrometeoroid shield/sun shade and one of its main solar panels . Debris from
5852-474: Was unexpectedly occupied by the "parasol" that replaced the missing meteorite shield, a few experiments were instead installed outside with the telescopes during spacewalks or shifted to the Earth-facing scientific airlock. Skylab 2 spent less time than planned on most experiments due to station repairs. On the other hand, Skylab 3 and Skylab 4 far exceeded the initial experiment plans, once the crews adjusted to
5929-455: Was used for storing film from various sources including the Apollo Telescope Mount solar instruments. Six ATM experiments used film to record data, and over the course of the missions over 150,000 successful exposures were recorded. The film canister had to be manually retrieved on crewed spacewalks to the instruments during the missions. The film canisters were returned to Earth aboard the Apollo capsules when each mission ended, and were among
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