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Thursday 20 August 2026 15:32:46 GMT
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Bro missed one note 🤣✌️ #germany #larp #piano #undertale #megalavonia The Saturn V was a super heavy-lift launch vehicle built by NASA under the direction of Wernher von Braun to send human missions to the Moon.General SpecificationsHeight: 363 feet (111 meters), taller than a 36-story building.Weight: 6.2 million pounds (2.8 million kilograms) when fully fueled.Primary Contractors: Boeing (S-IC first stage), North American Aviation (S-II second stage), Douglas Aircraft Company (S-IVB third stage), and IBM (Instrument Unit).Engines: Built by Rocketdyne division of North American Aviation.Rocket StagesFirst Stage (S-IC):Powered by five F-1 engines burning RP-1 kerosene and liquid oxygen.Generated 7.5 to 7.6 million pounds of thrust.Burned for about 2.5 minutes, lifting the rocket to an altitude of 40 miles.Second Stage (S-II):Powered by five J-2 engines burning liquid hydrogen and liquid oxygen.Generated 1 million pounds of thrust.Burned for about 6 minutes to push the vehicle through the upper atmosphere.Third Stage (S-IVB):Powered by a single J-2 engine using liquid hydrogen and liquid oxygen.Restartable design used first to enter Earth parking orbit and second for trans-lunar injection toward the Moon.Instrument Unit:Located above the third stage, built by IBM to guide and control all active stages during flight.Operational RecordActive Period: 1967 to 1973.Total Launches: 13 successful flights with zero failures carrying crew or payloads, including Apollo missions and the launch of the Skylab space station.
Bro missed one note 🤣✌️ #germany #larp #piano #undertale #megalavonia The Saturn V was a super heavy-lift launch vehicle built by NASA under the direction of Wernher von Braun to send human missions to the Moon.General SpecificationsHeight: 363 feet (111 meters), taller than a 36-story building.Weight: 6.2 million pounds (2.8 million kilograms) when fully fueled.Primary Contractors: Boeing (S-IC first stage), North American Aviation (S-II second stage), Douglas Aircraft Company (S-IVB third stage), and IBM (Instrument Unit).Engines: Built by Rocketdyne division of North American Aviation.Rocket StagesFirst Stage (S-IC):Powered by five F-1 engines burning RP-1 kerosene and liquid oxygen.Generated 7.5 to 7.6 million pounds of thrust.Burned for about 2.5 minutes, lifting the rocket to an altitude of 40 miles.Second Stage (S-II):Powered by five J-2 engines burning liquid hydrogen and liquid oxygen.Generated 1 million pounds of thrust.Burned for about 6 minutes to push the vehicle through the upper atmosphere.Third Stage (S-IVB):Powered by a single J-2 engine using liquid hydrogen and liquid oxygen.Restartable design used first to enter Earth parking orbit and second for trans-lunar injection toward the Moon.Instrument Unit:Located above the third stage, built by IBM to guide and control all active stages during flight.Operational RecordActive Period: 1967 to 1973.Total Launches: 13 successful flights with zero failures carrying crew or payloads, including Apollo missions and the launch of the Skylab space station.

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