{"id":67446,"date":"2016-03-09T18:43:53","date_gmt":"2016-03-09T23:43:53","guid":{"rendered":"http:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/skylab-wikipedia-the-free-encyclopedia\/"},"modified":"2016-03-09T18:43:53","modified_gmt":"2016-03-09T23:43:53","slug":"skylab-wikipedia-the-free-encyclopedia","status":"publish","type":"post","link":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/transhuman-news-blog\/space-station\/skylab-wikipedia-the-free-encyclopedia\/","title":{"rendered":"Skylab &#8211; Wikipedia, the free encyclopedia"},"content":{"rendered":"<p><p>Skylab                                                          Skylab as photographed by its departing final crew        (Skylab 4)                                                        Station statistics                            COSPAR ID                    1973-027A                            Call sign                    Skylab                            Crew                    3 per mission (9 total)                            Launch                    May 14, 1973        17:30:00 UTC                            Launch        pad                    Kennedy Space Center LC-39A                            Reentry                    July 11, 1979        16:37:00 UTC        near Perth,        Australia                            Mission status                    Complete; uncontrolled re-entry                            Mass                    150,300lb (68,175kg)[1]        w\/o Apollo CSM                            Length                    82.4 feet (25.1m)        w\/o Apollo CSM                            Width                    55.8 feet (17.0m)        w\/ one solar panel                            Height                    36.3 feet (11.1m)        w\/ telescope mount                            Diameter                    21.67 feet (6.6m)                            Pressurised volume                    12,417cuft (351.6m3)                            Perigee                    269.7mi (434.0km)                            Apogee                    274.6mi (441.9km)                            Orbital inclination                    50                            Orbital period                    93.4 min                            Orbits per day                    15.4                            Days in orbit                    2,249 days                            Days occupied                    171 days                            Number of orbits                    34,981                            Distance travelled                    ~890,000,000 mi (1,400,000,000 km)                            Statistics as of Re-entry July 11, 1979              <\/p>\n<p>    Skylab was a space station launched and operated by    NASA and was the United States'    first space station. Skylab orbited Earth from 1973 to 1979,    and included a workshop, a solar observatory, and other    systems. It was launched unmanned by a modified Saturn V rocket, with a    weight of 150,300 pounds (68,175kg).[1]    Three manned missions to the station, conducted between 1973    and 1974 using the Apollo Command\/Service    Module (CSM) atop the smaller Saturn IB, each delivered a    three-astronaut crew. On the last two manned missions, an    additional Apollo \/ Saturn IB stood by ready to rescue the crew    in orbit if it was needed.  <\/p>\n<p>    The station was damaged during launch when the micrometeoroid    shield separated from the workshop and tore away, taking one of    two main solar    panel arrays with it and jamming the other one so that it    could not deploy. 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    was able to save it in the first in-space major repair, by    deploying a replacement heat shade and freeing the jammed solar    panels.  <\/p>\n<p>    Skylab included the Apollo Telescope Mount,    which was a multi-spectral solar observatory, Multiple Docking    Adapter (with two docking ports), Airlock Module with EVA    hatches, and the Orbital Workshop, the main habitable volume.    Electrical power came from solar arrays, as well as 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.  <\/p>\n<p>    Numerous scientific experiments were conducted aboard Skylab    during its operational life, and crews were able to confirm the    existence of coronal holes in the Sun. The Earth Resources Experiment Package    (EREP) was used to view Earth with sensors that recorded data    in the visible, infrared, and microwave spectral regions.    Thousands of photographs of Earth were taken, and records for    human time spent in orbit were extended. Plans were made to    refurbish and reuse Skylab, using the Space Shuttle    to boost its orbit and repair it. However, development of the    Shuttle was delayed, and Skylab reentered Earth's atmosphere    and disintegrated in 1979, with debris striking portions of    Western Australia. Post-Skylab NASA    space laboratory projects included Spacelab, Shuttle-Mir, and    Space Station Freedom (later    merged into the International Space    Station).  <\/p>\n<p>    Rocket engineer    Wernher von Braun, science    fiction writer Arthur C. Clarke, and other early    advocates of manned 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 a large, circular station 250 feet    (75m) in diameter that would rotate to generate artificial gravity and require a fleet    of 7,000-ton (6,500-metric ton) 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 the Moon and Mars    would leave from the station.[2]:25  <\/p>\n<p>    The development of the transistor, the solar cell, and telemetry, led in the    1950s and early 1960s to unmanned 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 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.[2]:5560  <\/p>\n<p>    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 the rapidly forming    NASA. Although concentrating on the Moon missions, von Braun    also detailed an orbiting laboratory built out of a Horizon    upper stage,[3]:23    an idea used for Skylab.[3]:9    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\/Service    Module,[3]:10    or a Gemini capsule[3]:14    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.[3]:1314    A proposal to study the use of a Saturn S-IVB as a manned space laboratory was    documented in 1962 by the Douglas    Aircraft Company.[4]  <\/p>\n<p>    The Department of Defense    (DoD) and NASA cooperated closely in many areas of    space.[2]:198202    In September 1963, NASA and the DoD agreed to cooperate in    building a space station.[3]:17    The DoD wanted its own manned facility, however,[2]:203    and in December it announced Manned Orbital    Laboratory (MOL), a small space station primarily intended    for photo reconnaissance using large telescopes directed by a    two-man 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.[3]:1719[5][6] MOL    competed for funding with a NASA station for the next five    years[3]:15    and politicians and other officials often suggested that NASA    participate in MOL or use the DoD design.[2]:203    The military project led to changes to the NASA plans so that    they would resemble MOL less.[3]:17  <\/p>\n<p>    NASA management was concerned about losing the 400,000 workers    involved in Apollo after landing on the moon in 1969.[3]:20,22    A reason von Braun, head of NASA's Marshall Space Flight Center    during the 1960s, advocated for 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.[2]:61    NASA set up 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 (LEM), a large manned solar    telescope using a LEM as its crew quarters, and small space    stations using a variety of LEM 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).[3]:20  <\/p>\n<p>    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 the LEM 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.  <\/p>\n<p>    In November 1964, von Braun proposed a more ambitious plan to    build a much larger station built from 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-foot    (3.0m) 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 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-foot (10.1 by 13.7m)    living area. Power was to be provided by solar cells lining    the outside of the S-II stage.[3]:22  <\/p>\n<p>    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 LEM and CSM had been canceled, leaving a    number of Saturn IBs free for use. Further work led to the idea    of building a smaller \"wet workshop\" based on the S-IVB,    launched as the second stage of a Saturn IB.  <\/p>\n<p>    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 LEM, 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 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, 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 the S-IV    stage, before it was replaced by the S-IVB.[3]:25  <\/p>\n<p>    On April 1, 1966, MSC sent out contracts to Douglas, Grumman, and McDonnell for the conversion of a    S-IVB spent stage, under the name Saturn S-IVB spent-stage    experiment support module (SSESM).[3]:30    In May, astronauts voiced concerns over the purging of the    stage's hydrogen tank in space. Nevertheless, in late July it    was announced that 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.  <\/p>\n<p>    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 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.[3]:4548    The DoD later canceled MOL in June 1969.[3]:109  <\/p>\n<p>    Design work continued over the next two years, in an era of    shrinking budgets.[7]    (NASA sought $450 million for Apollo Applications in fiscal    year 1967, for example, but received $42 million.)[2]:6465    In August 1967, 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.  <\/p>\n<p>    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.[2]:66    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 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;[3]:109110    the S-IC and S-II lower stages could launch a \"dry workshop\",    with its interior already prepared, directly into orbit.  <\/p>\n<p>    [1]  <\/p>\n<p>    A dry workshop simplified plans for the interior of the    station.[3]:130Industrial design firm Raymond    Loewy\/William Snaith recommended emphasizing habitability and    comfort for the astronauts by, for example, providing a    wardroom for    meals and relaxation,[3]:133134    and a window to view Earth and space, although astronauts who    participated in Skylab planning were dubious about the    designers' focus on areas such as color schemes.[3]:137    Habitability had not previously been an area of concern when    building spacecraft, due to their small volume and brief    mission durations, but the Skylab missions would last for    months.[3]:133    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.[3]:139140  <\/p>\n<p>    Astronauts were uninterested in watching movies on a proposed    entertainment center or playing    games, but did want books and individual music choices.[3]:137    Food was also important; early Apollo crews complained about    its quality, and a NASA volunteer found living on the Apollo    food for four days on Earth to be intolerable; its taste and    composition, in the form of cubes and squeeze tubes, were    unpleasant. Skylab food significantly improved on    its predecessors by prioritizing edibility over scientific    needs.[3]:141142  <\/p>\n<p>    Each astronaut had a private sleeping area the size of a small    walk-in closet, with a curtain, sleeping bag, and    locker.[8]:82    Designers also added a shower[3]:139[8]:80    and a toilet;[3]:152158[8]:30    the latter was both for comfort and to obtain precise urine and    feces samples for examination on Earth.[3]:165  <\/p>\n<p>    Rescuing    astronauts from Skylab was possible in the most likely    emergency circumstances. The crew could use the CSM to quickly    return to Earth if the station suffered serious damage. If the    CSM failed, the spacecraft and Saturn IB for the next Skylab    mission would have been launched with two astronauts to    retrieve the crew; given Skylab's ample supplies, its residents    would have been able to wait up to several weeks for the rescue    mission.[9]  <\/p>\n<p>    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 a result of a NASA    contest.[3]:115    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. A Saturn V originally produced for the    Apollo program  before the cancellation of Apollo 18, 19, and    20  was repurposed and redesigned to launch Skylab.[10] The    Saturn V's upper stage was removed, but with the controlling    Instrument Unit remaining in its    standard position.  <\/p>\n<p>    Skylab was launched on May 14, 1973 by the modified Saturn V.    The launch is sometimes referred to as Skylab 1, or SL-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 the lost micrometeoroid shield further complicated    matters by pinning the remaining solar panel to the side of the    station, preventing its deployment and thus leaving the station    with a huge power deficit.[3]:253255  <\/p>\n<p>    Immediately following Skylab's launch, Pad A at Kennedy Space Center    Launch Complex 39 was deactivated, and construction    proceeded to modify it for the Space Shuttle program, originally    targeting a maiden    launch in March 1979. The manned missions to Skylab would    occur from Launch Pad 39B.  <\/p>\n<p>    Three manned missions, designated SL-2, SL-3 and SL-4, were made to Skylab. The first manned    mission, SL-2, launched on May 25, 1973 atop a Saturn IB and    involved extensive repairs to 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 NASA's \"Mr. Fix    It\" Jack    Kinzler, who won the NASA Distinguished Service    Medal for his efforts. The crew conducted further repairs    via two spacewalks (extra-vehicular activity, or    EVA). The crew stayed in orbit with Skylab for 28 days. Two    additional missions followed, with the launch dates of July 28,    1973 (SL-3) and November 16, 1973 (SL-4), and mission durations    of 59 and 84 days, respectively. The last Skylab crew returned    to Earth on February 8, 1974.  <\/p>\n<p>    Skylab orbited Earth 2,476 times during the 171 days and 13    hours of its occupation during the three manned Skylab    missions. 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.[3]:340    Solar experiments included photographs of eight solar flares, and    produced valuable results[8]:155    that scientists stated would have been impossible to obtain    with unmanned spacecraft.[3]:342344    The existence of the Sun's coronal holes were    confirmed because of these efforts.[3]:357    Many of the experiments conducted investigated the astronauts'    adaptation to extended periods of microgravity.  <\/p>\n<p>    A typical day began at 6 AM Central Time Zone.[3]:307308    Although the toilet was small and noisy, both veteran    astronautswho had endured earlier missions' rudimentary    waste-collection systemsand rookies complimented it.[3]:165,307[8]:80[12]    The first crew enjoyed taking a shower once a week, but found    drying themselves in weightlessness[12]    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    stomach muscles.[3]:306308  <\/p>\n<p>    Breakfast began at 7 AM. Astronauts usually stood to eat, as    sitting in microgravity also strained their stomach muscles.    They reported that their foodalthough greatly improved from    Apollowas 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 the water tank.    After dinner, which was scheduled for 6 PM, 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.[3]:309,334[13]:27  <\/p>\n<p>    Each Skylab mission set a record for the amount of time    astronauts spent in space. The station offered what a later    study called \"a highly satisfactory living and working    environment for crews\", with enough room for personal    privacy.[13]:24    Although it had a dart    set,[14]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.[8]:7980,134135  <\/p>\n<p>    Overview of most major experiments:[15] Skylab    3 carried several more experiments, such as to observe Comet    Kohoutek.  <\/p>\n<p>    Skylab was abandoned after the end of the SL-4 mission in    February 1974, but to welcome visitors the crew left a bag    filled with supplies and left the hatch unlocked.[16]    NASA discouraged any discussion of additional visits due to the    station's age,[3]:335,361    but in 1977 and 1978, when the agency still believed the    Space    Shuttle would be ready by 1979, it completed two studies on    reusing the station.[13]:3-1[16]    By September 1978, the agency believed Skylab was safe for    crews, with all major systems intact and operational.[13]:3-2    It still had 180 man-days of water and 420 man-days of    oxygen, and astronauts could refill both;[16]    the station could hold up to about 600 to 700 man-days of    drinkable water and 420 man-days of food.[13]:27  <\/p>\n<p>    The studies cited several benefits from reusing Skylab, which    one called a resource worth \"hundreds of millions of    dollars\"[13]:113    with \"unique habitability provisions for long duration space    flight.\"[13]:311    Because no more operational Saturn V rockets were available    after the Apollo program, four to five shuttle    flights and extensive space architecture would have been    needed to build another station as large as Skylab's 12,400    cubic feet (350m3) volume.[13]:1-12    to 1-13 Its ample sizemuch greater than that of the    shuttle alone, or even the shuttle plus Spacelab[13]:28was    enough, with some modifications, for up to seven    astronauts[13]:231    of both sexes,[13]:314    and experiments needing a long duration in space;[13]:113    even a movie projector for recreation was possible.[13]:311  <\/p>\n<p>    Proponents of Skylab's reuse also said repairing and upgrading    Skylab would provide information on the results of    long-duration exposure to space for future stations.[16]    The most serious issue for reactivation was stationkeeping, as one of the station's    gyroscopes had    failed[3]:361    and the attitude control    system needed refueling; these issues would need EVA to fix    or replace. The station had not been designed for extensive    resupply. However, although it was originally planned that    Skylab crews would only perform limited maintenance[8]:34    they successfully made major repairs during EVA, such as the    SL-2 crew's deployment of the solar panel[8]:7375    and the SL-4 crew's repair of the primary coolant loop.[3]:317[8]:130[13]:321    The SL-2 crew fixed one item during EVA by, reportedly,    \"hit[ting] it with [a] hammer.\"[8]:89  <\/p>\n<p>    Some studies also said, beyond the opportunity for space    construction and maintenance experience, reactivating the    station would free up shuttle flights for other uses,[13]:113    and reduce the need to modify the shuttle for    long-duration missions.[13]:2-9    to 2-10 Even if the station were not manned again, went    one argument, it would serve as a useful experimental    platform.[13]:261  <\/p>\n<p>    The reactivation would likely have occurred in four    phases:[16]  <\/p>\n<p>    The first three phases would have required about $60 million in    1980s dollars, not including launch costs.  <\/p>\n<p>    After a boost of 6.8 miles (10.9km) by SL-4's Apollo CSM    before its departure in 1974, Skylab was left in a parking orbit    of 269 miles (433km) by 283 miles (455km)[3]:361    that was expected to last until at least the early 1980s, based    on estimates of the 11-year sunspot cycle    that began in 1976.[3]:361[20]    NASA began considering the potential risks of a space station    reentry as early as 1962, but decided to not incorporate a    retrorocket    system in Skylab due to cost and acceptable risk.[3]:127129  <\/p>\n<p>    The spent 49-ton Saturn V S-II stage which had launched Skylab in 1973    remained in orbit for almost two years, and made an    uncontrolled reentry on January 11, 1975.[21] Some    debris, most prominently the five heavy J-2 engines, likely survived to impact in the    North Atlantic Ocean. Although this event did not receive heavy    media or public attention, it was followed closely by NASA and    the Air Force, and helped emphasize the need for improved    planning and public awareness for Skylab's eventual    reentry.[citation    needed]  <\/p>\n<p>    British mathematician Desmond King-Hele of the Royal Aircraft Establishment    predicted that Skylab would de-orbit and crash to earth due to    increased solar activity. NASA    initially denied this but accepted after his calculations were    checked.[citation    needed] Greater-than-expected solar    activity[3]:362    heated the outer layers of Earth's atmosphere and increased    drag on Skylab. By late 1977, NORAD accurately forecast a    reentry in mid-1979;[20]    a National    Oceanic and Atmospheric Administration (NOAA) scientist    criticized NASA for using an inaccurate model for the second    most-intense sunspot cycle in a century, and for ignoring NOAA    predictions published in 1976.[3]:362363  <\/p>\n<p>    The reentry of the USSR's nuclear powered Cosmos 954 in January 1978, and the resulting    radioactive debris fall in northern Canada, drew more attention    to Skylab's orbit. Although Skylab did not contain radioactive    materials, the State Department warned    NASA about the potential diplomatic repercussions of station    debris.[3]:363Battelle Memorial    Institute forecast that up to 25 tons of metal debris could    land in 500 pieces over an area 4,000 miles long and 1,000    miles wide. The lead-lined film vault, for example, might land    intact at 400 feet per second.[22]  <\/p>\n<p>    Ground controllers re-established contact with Skylab in March    1978[20]    and recharged its batteries.[23]    Although NASA worked on plans to reboost Skylab with the    Space    Shuttle through 1978 and the TRS was almost complete, the    agency gave up in December when it became clear that the    shuttle would not be ready in time;[3]:363367[17]    its first flight, STS-1, did not occur until April 1981. Also    rejected were proposals to launch the TRS using one or two    unmanned rockets[16]    or to attempt to destroy the station with missiles.[22]  <\/p>\n<p>    Skylab's demise was an international media event, with    merchandising of T-shirts and hats with bullseyes,[22]    wagering on the time and place of re-entry, and nightly news    reports. The San Francisco    Examiner offered a $10,000 prize for the first piece of    Skylab delivered to its offices; the competing Chronicle offered $200,000 if    a subscriber suffered personal or property damage.[23]    NASA calculated that the odds of station re-entry debris    hitting any human were 1 to 152 and when multiplied by 4    billion becomes 1 in 600 billion for a specific human,[24]    although the odds of debris hitting a city of 100,000 or more    were 1 to 7 and special teams were readied to head to any    country hit by debris and requesting help.[23]  <\/p>\n<p>          We assume that Skylab is on the planet Earth, somewhere.        <\/p>\n<p>    In the hours before re-entry, ground controllers adjusted    Skylab's orientation to try to minimize the risk of re-entry on    a populated area.[23]    They aimed the station at a spot 810 miles (1,300km)    south southeast of Cape Town,    South Africa, and re-entry began at approximately 16:37    UTC, July 11, 1979.[3]:371    The Air Force provided data from a secret tracking system able    to monitor the reentry.[25]    The station did not burn up as fast as NASA expected, however.    Due to a 4% calculation error, debris landed southeast of    Perth, Western    Australia,[3]:371    and was found between Esperance and Rawlinna, from 31 to 34S and 122 to 126E,    about 130150km radius around Balladonia. Residents and    an airline pilot saw dozens of colorful fireworks-like flares    as large pieces broke up in the atmosphere.[22]    The Shire of Esperance facetiously fined    NASA A$400 for littering, a fine which remained    unpaid for 30 years.[26] The    fine was paid in April 2009, when radio show host Scott Barley    of Highway Radio raised the funds from his morning show    listeners and paid the fine on behalf of NASA.[27][28]  <\/p>\n<p>    Seventeen-year-old Stan Thornton found 24 pieces of Skylab at    his home in Esperance. A Philadelphia businessman flew him, his    parents, and his girlfriend to San Francisco, where he collected the    Examiner prize.[3]:371[22]    In a coincidence for the organizers, the annual Miss    Universe pageant was scheduled to be held a few days later,    on July 20, 1979 in Perth. A large piece of Skylab debris was    displayed on the stage.[29]    Analysis of the debris showed that the station had not    disintegrated until 10 miles above the Earth, much lower than    expected.[22]  <\/p>\n<p>    After the demise of Skylab, NASA focused on the reusable    Spacelab module,    an orbital workshop that could be deployed with the Space    Shuttle and returned to Earth. The next American major space    station project was Space Station Freedom,    which was merged into the International Space Station    in 1993, and launched starting in 1998. Shuttle-Mir was another project, and    led to the U.S. funding Spektr, Priroda, and the Mir Docking Module in the    1990s.  <\/p>\n<p>    Skylab 5 would have been a short 20-day mission to conduct    scientific experiments and boost Skylab into a higher orbit.    Vance Brand (commander), William B.    Lenoir (science pilot), and Don Lind (pilot) would have    been the crew for this mission, with Brand and Lind being the    prime crew for the Skylab Rescue flights.[30]    Brand and Lind also trained for a mission that would have aimed    Skylab for a controlled deorbit.[25]  <\/p>\n<p>    In addition to the flown Skylab space station, a second    flight-quality backup Skylab space station had been built    during the program. NASA considered using it for a second    station in May 1973 or later, to be called Skylab B (S-IVB    515), but decided against it. Launching another Skylab with    another Saturn V rocket would have been very costly, and it was    decided to spend this money on the development of the Space    Shuttle instead. The backup is on display at the National Air and Space    Museum in Washington, D.C.  <\/p>\n<p>    A full-size training mock-up once used for astronaut training    is located at the Lyndon B. Johnson Space    Center visitor's center in Houston, Texas.    Another full-size training mock-up is at the U.S. Space & Rocket    Center in Huntsville, Alabama. Originally    displayed indoors, it was subsequently stored outdoors for    several years to make room for other exhibits. To mark the 40th    anniversary of the Skylab program, the Orbital Workshop portion    of the trainer was restored and moved into the Davidson Center    in 2013.[31][32] NASA    transferred the    backup Skylab to the National Air and Space Museum in 1975.    On display in the Museum's Space Hall since 1976, the orbital    workshop has been slightly modified to permit viewers to walk    through the living quarters.[33]  <\/p>\n<p>    The numerical identification of the manned Skylab missions was    the cause of some confusion. Originally, the unmanned launch of    Skylab and the three manned missions to the station were    numbered SL-1 through SL-4. During the    preparations for the manned missions, some documentation was    created with a different scheme -- SLM-1 through    SLM-3for those missions only. William Pogue credits Pete Conrad with    asking the Skylab program director which scheme should be used    for the mission patches, and the astronauts were    told to use 1-2-3, not 2-3-4. By the time NASA administrators    tried to reverse this decision, it was too late, as all the    in-flight clothing had already been manufactured and shipped    with the 1-2-3 mission patches.[34]  <\/p>\n<p>    From 1966 to 1974, the Skylab program cost a total of $2.2    billion or $10 billion in 2010 dollars with inflation. As its    three three-man crews spent 510 total man-days in space, each    man-day cost approximately $20 million in 2010 dollars,    compared to $7.5 million for the International Space    Station.[35]  <\/p>\n<p>            An astronaut mannequin dines aboard the backup Skylab            at the Smithsonian NASM.          <\/p>\n<p>            SkyLab commemorative stamp, Issue of            1974. The commemorative stamp reflects initial repairs            to the station, including the parasol sunshade.          <\/p>\n<p>            Vanguard (T-AGM-19) seen as a            NASA Skylab tracking ship. Note the tracking radar and            telemetry antennas.          <\/p>\n<p>            Robbins Medallions issued for Skylab Missions.          <\/p>\n<p><!-- Auto Generated --><\/p>\n<p>See original here:<br \/>\n<a target=\"_blank\" href=\"https:\/\/en.wikipedia.org\/wiki\/Skylab\" title=\"Skylab - Wikipedia, the free encyclopedia\">Skylab - Wikipedia, the free encyclopedia<\/a><\/p>\n","protected":false},"excerpt":{"rendered":"<p> Skylab Skylab as photographed by its departing final crew (Skylab 4) Station statistics COSPAR ID 1973-027A Call sign Skylab Crew 3 per mission (9 total) Launch May 14, 1973 17:30:00 UTC Launch pad Kennedy Space Center LC-39A Reentry July 11, 1979 16:37:00 UTC near Perth, Australia Mission status Complete; uncontrolled re-entry Mass 150,300lb (68,175kg)[1] w\/o Apollo CSM Length 82.4 feet (25.1m) w\/o Apollo CSM Width 55.8 feet (17.0m) w\/ one solar panel Height 36.3 feet (11.1m) w\/ telescope mount Diameter 21.67 feet (6.6m) Pressurised volume 12,417cuft (351.6m3) Perigee 269.7mi (434.0km) Apogee 274.6mi (441.9km) Orbital inclination 50 Orbital period 93.4 min Orbits per day 15.4 Days in orbit 2,249 days Days occupied 171 days Number of orbits 34,981 Distance travelled ~890,000,000 mi (1,400,000,000 km) Statistics as of Re-entry July 11, 1979 Skylab was a space station launched and operated by NASA and was the United States' first space station. Skylab orbited Earth from 1973 to 1979, and included a workshop, a solar observatory, and other systems. It was launched unmanned by a modified Saturn V rocket, with a weight of 150,300 pounds (68,175kg).[1] Three manned missions to the station, conducted between 1973 and 1974 using the Apollo Command\/Service Module (CSM) atop the smaller Saturn IB, each delivered a three-astronaut crew.  <a href=\"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/transhuman-news-blog\/space-station\/skylab-wikipedia-the-free-encyclopedia\/\">Continue reading <span class=\"meta-nav\">&rarr;<\/span><\/a><\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"closed","ping_status":"closed","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[31],"tags":[],"class_list":["post-67446","post","type-post","status-publish","format-standard","hentry","category-space-station"],"_links":{"self":[{"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/posts\/67446"}],"collection":[{"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/comments?post=67446"}],"version-history":[{"count":0,"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/posts\/67446\/revisions"}],"wp:attachment":[{"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/media?parent=67446"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/categories?post=67446"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/www.euvolution.com\/prometheism-transhumanism-posthumanism\/wp-json\/wp\/v2\/tags?post=67446"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}