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High activity from your Location Country  Ukraine   Country Code  UA   Region  Odessa Oblast   City  Odessa   It will take maximum 2 3 minutes and after that youll receive the requested amount in your wallet. Latest Activities 1. BTC0s ago. F. A. Q. Is this tool freeYes, this tool is free and is developed and hosted by our team to help each of you to enjoy the power of bitcoin. How it works our tool Our software is a brand new tool that makes bitcoin mining more faster than any tool on the market. Who we are We are a team of programmers with over 5 years experience in the bitcoin industry. Is this tool safe Our tool is safe because you dont need to download anything and every process is executed on our servers. Copyright 2. 01. All rights reserved. Saturn V Wikipedia. This article is about the rocket. For the fifth moon of Saturn, see Rhea moon. Saturn VThe final manned Saturn V, AS 5. Apollo 1. 7 in December 1. Function. Manufacturer. Web Design Templates Html Css. Country of origin. United States. Project cost6. Cost per launch1. Size. Height. 36. Diameter. 33. 0 ft 1. Mass. 6,5. 40,0. 00 lb 2,9. Stages. 3Capacity. Payload to LEO 9. Payload to TLI1. 07,1. Associated rockets. Family. Saturn. Derivatives. Saturn INT 2. 1Comparable. Launch history. Status. Retired. Launch sites. LC 3. 9, Kennedy Space Center. Total launches. 13. Successes. 12. Failures. Partial failures. Apollo 6First flight. November 9, 1. 96. AS 5. 01note 2Apollo 4Last flight. May 1. 4, 1. 97. 3 AS 5. Skylab 1First stage S ICLength. Diameter. 33. 0 ft 1. Empty mass. 28. 7,0. Gross mass. 5,0. 40,0. Engines. 5 Rocketdyne F 1. Thrust. 7,8. 91,0. N sea level. Specific impulse. Burn time. 16. 5 seconds. Fuel. RP 1LOXSecond stage S IILength. Diameter. 33. 0 ft 1. Empty mass. 88,4. Gross mass. 1,0. 93,9. Engines. 5 Rocketdyne J 2. Thrust. 1,1. 55,8. N vacuum. Specific impulse. Burn time. 36. 0 seconds. Fuel. LH2LOXThird stage S IVBLength. Diameter. 21. 7 ft 6. Empty mass. 29,7. Gross mass. 27. 1,0. Engines. 1 Rocketdyne J 2. Thrust. 22. 5,0. 00 lbf 1,0. N vacuum. Specific impulse. Burn time. 16. 5 3. Fuel. LH2LOXThe Saturn V spoken as Saturn five was an American human ratedexpendablerocket used by NASA between 1. The three stageliquid fueledsuper heavy lift launch vehicle was developed to support the Apollo program for human exploration of the Moon and was later used to launch Skylab, the first American space station. The Saturn V was launched 1. Kennedy Space Center in Florida with no loss of crew or payload. As of 2. 01. 7, updatethe Saturn V remains the tallest, heaviest, and most powerful highest total impulse rocket ever brought to operational status, and holds records for the heaviest payload launched and largest payload capacity to low Earth orbit LEO of 1. Apollo CommandService Module and Lunar Module to the Moon. The largest production model of the Saturn family of rockets, the Saturn V was designed under the direction of Wernher von Braun and Arthur Rudolph at the Marshall Space Flight Center in Huntsville, Alabama, with Boeing, North American Aviation, Douglas Aircraft Company, and IBM as the lead contractors. To dateupdate, the Saturn V remains the only launch vehicle to launch missions to carry humans beyond low Earth orbit. A total of 1. 5 flight capable vehicles were built, but only 1. An additional three vehicles were built for ground testing purposes. A total of 2. 4 astronauts were launched to the Moon, three of them twice, in the four years spanning December 1. December 1. 97. 2. Historical backgroundeditThe origins of the Saturn V rocket begin with the US government bringing Wernher von Braun along with about seven hundred German rocket engineers and technicians to the United States in Operation Paperclip, a program authorized by President Truman in August 1. Germanys rocket expertise, to give the US an edge in the Cold War through development of intermediate range IRBM and intercontinental ballistic missiles ICBM. It was known that Americas rival, the Soviet Union, would also try to secure some of the Germans. Von Braun was put into the rocket design division of the Army due to his prior direct involvement in the creation of the V 2 rocket. Between 1. V 2 to the American engineers. Despite Von Brauns many articles on the future of space rocketry, the US Government continued funding Air Force and Navy rocket programs to test their Vanguard missiles in spite of numerous costly failures. It was not until the 1. Soviet launch of Sputnik 1 atop an R 7. ICBM capable of carrying a thermonuclear warhead to the US,91. Army and the government started taking serious steps towards putting Americans in space. Finally, they turned to von Braun and his team, who during these years created and experimented with the Jupiter series of rockets. The Juno I was the rocket that launched the first American satellite in January 1. NACA the predecessor of NASA to get its foot in the Space Race. The Jupiter series was one more step in von Brauns journey to the Saturn V, later calling that first series an infant Saturn. Saturn developmenteditThe Saturn Vs design stemmed from the designs of the Jupiter series rockets. As the success of the Jupiter series became evident, the Saturn series emerged. C 1 to C 4editBetween 1. Marshall Space Flight Center MSFC designed a series of Saturn rockets that could be used for various Earth orbit or lunar missions. The C 1 was developed into the Saturn I, and the C 2 rocket was dropped early in the design process in favor of the C 3, which was intended to use two F 1 engines on its first stage, four J 2 engines for its second stage, and an S IV stage, using six RL1. NASA planned to use the C 3 as part of the Earth Orbit Rendezvous EOR concept, with at least four or five launches needed for a single lunar mission. But MSFC was already planning an even bigger rocket, the C 4, which would use four F 1 engines on its first stage, an enlarged C 3 second stage, and the S IVB, a stage with a single J 2 engine, as its third stage. The C 4 would need only two launches to carry out an EOR lunar mission. On January 1. NASA announced plans to build the C 5. The three stage rocket would consist of the S IC first stage, with five F 1 engines the S II second stage, with five J 2 engines and the S IVB third stage, with a single J 2 engine. The C 5 was designed for a 9. Moon. 1. 3The C 5 would undergo component testing even before the first model was constructed. The S IVB third stage would be used as the second stage for the C IB, which would serve both to demonstrate proof of concept and feasibility for the C 5, but would also provide flight data critical to development of the C 5. Rather than undergoing testing for each major component, the C 5 would be tested in an all up fashion, meaning that the first test flight of the rocket would include complete versions of all three stages. By testing all components at once, far fewer test flights would be required before a manned launch. The C 5 was confirmed as NASAs choice for the Apollo program in early 1. Saturn V. 1. 3 The C 1 became the Saturn I, and C 1. B became Saturn IB. Von Braun headed a team at the Marshall Space Flight Center in building a vehicle capable of launching a manned spacecraft on a trajectory to the Moon. Before they moved under NASAs jurisdiction, von Brauns team had already begun work on improving the thrust, creating a less complex operating system, and designing better mechanical systems. It was during these revisions that the decision to reject the single engine of the V 2s design came about, and the team moved to a multiple engine design. The Saturn I and IB reflected these changes, but were not large enough to send a manned spacecraft to the Moon. These designs, however, provided a basis for which NASA could determine its best method towards landing a man on the Moon. The Saturn Vs final design had several key design features. Engineers determined that the best engines were the F 1s coupled with the new liquid hydrogen propulsion system called J 2, which made the Saturn C 5 configuration optimal.