[{"@context":"http:\/\/schema.org\/","@type":"BlogPosting","@id":"https:\/\/wiki.edu.vn\/en\/wiki41\/s-ic-wikipedia\/#BlogPosting","mainEntityOfPage":"https:\/\/wiki.edu.vn\/en\/wiki41\/s-ic-wikipedia\/","headline":"S-IC – Wikipedia","name":"S-IC – Wikipedia","description":"before-content-x4 S-IC Manufacturer Boeing Country of origin United States Used on Saturn V Height 42\u00a0m (138\u00a0ft) Diameter 10\u00a0m (33\u00a0ft) Gross","datePublished":"2022-09-21","dateModified":"2022-09-21","author":{"@type":"Person","@id":"https:\/\/wiki.edu.vn\/en\/wiki41\/author\/lordneo\/#Person","name":"lordneo","url":"https:\/\/wiki.edu.vn\/en\/wiki41\/author\/lordneo\/","image":{"@type":"ImageObject","@id":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","url":"https:\/\/secure.gravatar.com\/avatar\/c9645c498c9701c88b89b8537773dd7c?s=96&d=mm&r=g","height":96,"width":96}},"publisher":{"@type":"Organization","name":"Enzyklop\u00e4die","logo":{"@type":"ImageObject","@id":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","url":"https:\/\/wiki.edu.vn\/wiki4\/wp-content\/uploads\/2023\/08\/download.jpg","width":600,"height":60}},"image":{"@type":"ImageObject","@id":"https:\/\/upload.wikimedia.org\/wikipedia\/commons\/thumb\/7\/7e\/Ap10-KSC-68C-7912.jpg\/220px-Ap10-KSC-68C-7912.jpg","url":"https:\/\/upload.wikimedia.org\/wikipedia\/commons\/thumb\/7\/7e\/Ap10-KSC-68C-7912.jpg\/220px-Ap10-KSC-68C-7912.jpg","height":"279","width":"220"},"url":"https:\/\/wiki.edu.vn\/en\/wiki41\/s-ic-wikipedia\/","wordCount":5092,"articleBody":"     (adsbygoogle = window.adsbygoogle || []).push({});before-content-x4S-ICManufacturerBoeingCountry of originUnited StatesUsed onSaturn VHeight42\u00a0m (138\u00a0ft)Diameter10\u00a0m (33\u00a0ft)Gross mass5,030,000\u00a0lb (2,280,000\u00a0kg)Empty mass290,000\u00a0lb (130,000\u00a0kg)StatusRetiredTotal launches13Successes(stage only)13First flightNovember 9, 1967 (Apollo 4)Last flightMay 14, 1973 (Skylab 1)Powered by5 F-1Maximum thrust34,500\u00a0kN (7,750,000\u00a0lbf) sea level[1]Specific impulse263 seconds (2.58\u00a0km\/s)Burn time150 sPropellantRP-1\/LOXThe S-IC (pronounced S-one-C[2][3]) was the first stage of the American Saturn V rocket. The S-IC stage was manufactured by the Boeing Company. Like the first stages of most rockets, most of its mass of more than 2,000\u00a0t (4,400,000\u00a0lb) at launch was propellant, in this case RP-1 rocket fuel and liquid oxygen (LOX) oxidizer. It was 42\u00a0m (138\u00a0ft) tall and 10\u00a0m (33\u00a0ft) in diameter. The stage provided 34,500\u00a0kN (7,750,000\u00a0lbf)[1] of thrust at sea level to get the rocket through the first 61\u00a0km (38\u00a0mi) of ascent. The stage had five F-1 engines in a quincunx arrangement. The center engine was fixed in position, while the four outer engines could be hydraulically gimballed to control the rocket.       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4Table of ContentsManufacturing[edit]Stages built[edit]See also[edit]References[edit]External links[edit]Manufacturing[edit]The Boeing Co. was awarded the contract to manufacture the S-IC on December 15, 1961. By this time the general design of the stage had been decided on by the engineers at the Marshall Space Flight Center (MSFC). The main place of manufacture was the Michoud Assembly Facility, New Orleans. Wind tunnel testing took place in Seattle and the machining of the tools needed to build the stages at Wichita, Kansas.       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4MSFC built the first three test stages (S-IC-T, the S-IC-S, and the S-IC-F) and the first two flight models (S-IC-1 and -2).[4]It took roughly seven to nine months to build the tanks and 14 months to complete a stage. The first stage built by Boeing was S-IC-D, a test model.[4]In addition to the four test stages, NASA ordered 15 flight stages (S-IC-1 through -15) to support the initial Apollo program.[4] In July 1967, NASA awarded Boeing a contract to begin long-lead-time item acquisition (such as propellant lines and tank components) for the 16th and 17th S-IC stages. A full contract for the construction of S-IC-16 to S-IC-25 was drafted throughout mid-1967, but stages past S-IC-15 were canceled altogether in October of that year due to budgetary restrictions.[5][6] S-IC-16 to -25 would have been utilized for follow-on Apollo missions, including those from the Apollo Applications Program.The S-IC was composed of five major subsections.       (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4The largest and heaviest single component of the S-IC was the thrust structure, with a mass of 24 short tons (48,000\u00a0lb; 22,000\u00a0kg).[7] It was designed to support the thrust of the five engines and redistribute it evenly across the base of the rocket. There were four anchors which held down the rocket as it built thrust. These were among the largest aluminum forgings produced in the U.S. at the time, 4.3\u00a0m (14\u00a0ft) long and 816\u00a0kg (1,799\u00a0lb) in weight. The four stabilizing fins withstood a temperature of 1,100\u00a0\u00b0C (2,010\u00a0\u00b0F).[8]The five F-1 engines were ignited in 3 staggered events, where the center engine was first ignited, followed by two outer engines, and then the remaining two outer engines. These three ignition events were separated by just 300 milliseconds.[4] This staggered ignition approach lessened the loads on the thrust structure, as an instantaneous ignition of all five engines would impart immense stress on the stage.Above the thrust structure was the fuel tank, containing 730,000\u00a0L (730\u00a0m3; 26,000\u00a0cu\u00a0ft) of RP-1 fuel.[8] The tank itself had a mass of over 12 short tons (24,000\u00a0lb; 11,000\u00a0kg) dry[7] and could release 4,900\u00a0L\/s (4.9\u00a0m3\/s; 170\u00a0cu\u00a0ft\/s). Nitrogen was bubbled through the tank before launch to keep the fuel mixed.[8] During the flight the fuel was pressurized using helium, which was stored in tanks in the liquid oxygen tank above. Both the thrust structure and fuel tank had alternating black and white paint, in order to monitor the vehicle’s roll during flight.Between the fuel and liquid oxygen tanks was the intertank. This contained propellant fill and drain lines for the liquid oxygen tank as well as a portion of the five liquid oxygen feed lines for the engines.The liquid oxygen tank held 1,204,000\u00a0L (1,204\u00a0m3; 42,500\u00a0cu\u00a0ft) of LOX. It raised special issues for the designer. The lines through which the LOX ran to the engine had to be straight (as any bend would slow the flow of LOX, which would necessitate even larger and heavier piping) and therefore had to pass through the fuel tank. This meant insulating these lines inside a tunnel to stop fuel freezing to the outside and also meant adding five extra holes in the top of the fuel tank.[8]Atop the liquid oxygen tank sat the forward skirt, which connected the S-IC to the S-II stage and contained telemetry equipment and LOX tank vent lines.Two solid motor retrorockets were located inside each of the four conical engine fairings. At separation of the S-IC from the flight vehicle, the eight retrorockets fired, blowing off removable sections of the fairings forward of the fins, and backing the S-IC away from the flight vehicle as the engines on the S-II stage were ignited.The propellant tanks of the S-IC were manufactured from 2219-series aluminum panels, while the interstage, forward skirt, and thrust structure were built from 7075-series aluminum. The latter three sections also were corrugated with external stringers, providing additional structural support. The propellant tanks did not feature external stringers, as the tank pressurization provided sufficient rigidity.[4]The S-IC also carried the ODOP transponder to track the flight after takeoff.Cutaway diagram of the S-IC.Saturn V first stages S-1C-10, S-1C-11, and S-1C-9 at Michoud Assembly Facility.Apollo 11 S-IC separation.Stages built[edit]Serial\u00a0numberUseLaunch dateCurrent locationNotesS-IC-TStatic test firingPart of Saturn V display at Kennedy Space Center.[9]First all-up S-IC stage built, nicknamed “T-Bird.” Assembled between 1963-1965. Completed at least 22 test firings between 1965 and 1967 in support of S-IC development and test stand activation.[4]S-IC-SStructural load testing (had no engines).Scrapped after completing testing at MSFC.[4]S-IC-FFacilities testing for checking out launch complex assembly buildings and launch equipment.Returned to MSFC for storage after testing, later scrapped.[4]Conducted propellant tank loading tests at LC-39A using Mobile Launcher 1.S-IC-DGround test dynamics modelU.S. Space & Rocket Center, Huntsville, Alabama 34\u00b042\u203238.7\u2033N 86\u00b039\u203224.2\u2033W\ufeff \/ \ufeff34.710750\u00b0N 86.656722\u00b0W\ufeff \/ 34.710750; -86.656722S-IC-1Apollo 4November 9, 1967Manufactured by MSFC.S-IC-2Apollo 6April 4, 1968Manufactured by MSFC; carried TV and cameras on boattail and forward skirt.S-IC-3Apollo 8December 21, 196830\u00b012\u2032N 74\u00b07\u2032W\ufeff \/ \ufeff30.200\u00b0N 74.117\u00b0W\ufeff \/ 30.200; -74.117Manufactured by Boeing (as with all subsequent stages); weighed less than previously manufactured units allowing 36\u00a0kg more payload.S-IC-4Apollo 9March 3, 196930\u00b011\u2032N 74\u00b014\u2032W\ufeff \/ \ufeff30.183\u00b0N 74.233\u00b0W\ufeff \/ 30.183; -74.233S-IC-5Apollo 10May 18, 196930\u00b011\u2032N 74\u00b012\u2032W\ufeff \/ \ufeff30.183\u00b0N 74.200\u00b0W\ufeff \/ 30.183; -74.200Last flight for S-IC R&D Instrumentation.S-IC-6Apollo 11July 16, 196930\u00b013\u2032N 74\u00b02\u2032W\ufeff \/ \ufeff30.217\u00b0N 74.033\u00b0W\ufeff \/ 30.217; -74.033One or more engines recovered by a team financed by Jeff Bezos.[10]S-IC-7Apollo 12November 14, 196930\u00b016\u2032N 74\u00b054\u2032W\ufeff \/ \ufeff30.267\u00b0N 74.900\u00b0W\ufeff \/ 30.267; -74.900S-IC-8Apollo 13April 11, 197030\u00b011\u2032N 74\u00b04\u2032W\ufeff \/ \ufeff30.183\u00b0N 74.067\u00b0W\ufeff \/ 30.183; -74.067S-IC-9Apollo 14January 31, 197129\u00b050\u2032N 74\u00b03\u2032W\ufeff \/ \ufeff29.833\u00b0N 74.050\u00b0W\ufeff \/ 29.833; -74.050S-IC-10Apollo 15July 26, 197129\u00b042\u2032N 73\u00b039\u2032W\ufeff \/ \ufeff29.700\u00b0N 73.650\u00b0W\ufeff \/ 29.700; -73.650S-IC-11Apollo 16April 16, 197230\u00b012\u2032N 74\u00b09\u2032W\ufeff \/ \ufeff30.200\u00b0N 74.150\u00b0W\ufeff \/ 30.200; -74.150S-IC-12Apollo 17December 7, 197228\u00b013\u2032N 73\u00b053\u2032W\ufeff \/ \ufeff28.217\u00b0N 73.883\u00b0W\ufeff \/ 28.217; -73.883S-IC-13Skylab 1May 14, 1973Engine shutoff changed to 1-2-2 from 1\u20134 to lessen loads on Apollo Telescope Mount.S-IC-14UnusedSaturn V display at Johnson Space Center.Scheduled to fly Apollo 18 in 1974, never flew.[4]S-IC-15UnusedOn display at Michoud Assembly Facility until June 2016 then preserved at INFINITY Space Center in Mississippi.Originally intended to fly Apollo 19 in 1974. Designated but never used as a backup Skylab launch vehicle.[4]S-IC-16Never completedAssembly canceled during long-lead item procurement.[4]S-IC-17Never completedAssembly canceled during long-lead item procurement.[4]See also[edit]References[edit]^ a b Thorne, Muriel, ed. (May 1983). NASA, The First 25 Years: 1958-1983 (PDF). Washington, D.C.: National Aeronautics and Space Administration. p.\u00a069.^ Murray, Charles A.; Cox, Catherine Bly (Jul 1989). Apollo, the race to the moon. Simon and Schuster. p.\u00a054. ISBN\u00a09780671611019.^ Woods, W. David (2011-08-08). How Apollo Flew to the Moon. Springer Science & Business Media. p.\u00a024. ISBN\u00a09781441971791.^ a b c d e f g h i j k l Kyle, Ed. “Saturn Vehicle History”. spacelaunchreport.com. Archived from the original on March 21, 2022.^ “Michoud Assembly Facility January 1, 1967 – December 31, 1967” (PDF). uah.edu. Retrieved 2023-03-18.{{cite web}}:  CS1 maint: url-status (link)^ “Saturn Illustrated Chronology Part 8”. history.nasa.gov. Retrieved 2023-03-18.{{cite web}}:  CS1 maint: url-status (link)^ a b http:\/\/www.apolloexplorer.co.uk\/pdf\/saturnv\/First%20Stage.pdf^ a b c d “chapter 7”. history.nasa.gov. Retrieved 2021-10-23.{{cite web}}:  CS1 maint: url-status (link)^ Casebolt, Barry J. (March 18, 1974). “Headed for Florida Museum \u2014 Veteran Moon Rocket Booster Leaves MSFC”. The Huntsville Times. Huntsville, Alabama.^ Pearlman, Robert Z. (March 22, 2013). “Jeff Bezos’ Salvaged Apollo Rocket Engines Reach Shore After Ocean Recovery”. Space. New York City, New York. Retrieved June 1, 2021.External links[edit]     (adsbygoogle = window.adsbygoogle || []).push({});after-content-x4"},{"@context":"http:\/\/schema.org\/","@type":"BreadcrumbList","itemListElement":[{"@type":"ListItem","position":1,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki41\/#breadcrumbitem","name":"Enzyklop\u00e4die"}},{"@type":"ListItem","position":2,"item":{"@id":"https:\/\/wiki.edu.vn\/en\/wiki41\/s-ic-wikipedia\/#breadcrumbitem","name":"S-IC – Wikipedia"}}]}]