Matches in DBpedia 2016-04 for { <http://wikidata.dbpedia.org/resource/Q719315> ?p ?o }
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- Q719315 abstract "The Saturn IB (pronounced "one B", also known as the Uprated Saturn I) was an American launch vehicle commissioned by the National Aeronautics and Space Administration (NASA) for the Apollo program. It replaced the S-IV second stage of the Saturn I with the much more powerful S-IVB, able to launch a partially fueled Apollo Command/Service Module (CSM) or a fully fueled Lunar Module (LM) into low Earth orbit for early flight tests before the larger Saturn V needed for lunar flight was ready.By sharing the S-IVB upper stage, the Saturn IB and Saturn V provided a common interface to the Apollo spacecraft. The only major difference was that the S-IVB on the Saturn V burned only part of its propellant to achieve Earth orbit, so it could be restarted for translunar injection. The S-IVB on the Saturn IB needed all of its propellant to achieve Earth orbit.The Saturn IB launched two unmanned CSM suborbital flights, one unmanned LM orbital flight, and the first manned CSM orbital mission (first planned as Apollo 1, later flown as Apollo 7). It also launched one orbital mission, AS-203, without a payload so the S-IVB would have residual liquid hydrogen fuel. This mission supported the design of the restartable version of the S-IVB used in the Saturn V, by observing the behavior of the liquid hydrogen in weightlessness.In 1973, the year after the Apollo lunar program ended, three Apollo CSM/Saturn IBs ferried crews to the Skylab space station. In 1975, one last Apollo/Saturn IB launched the Apollo portion of the joint US-USSR Apollo Soyuz Test Project (ASTP). A backup Apollo CSM/Saturn IB was assembled and made ready for a Skylab rescue mission but never flown.The remaining Saturn IBs in NASA's inventory were scrapped after the ASTP mission as no use could be found for them and all heavy lift needs of the US space program could be serviced by the cheaper and more versatile Titan III family.".
- Q719315 countryOrigin Q30.
- Q719315 diameter "6.605016".
- Q719315 failedLaunches "0".
- Q719315 finalFlight "1975-07-15".
- Q719315 height "43.15968".
- Q719315 launchSite Q2175575.
- Q719315 launchSite Q334465.
- Q719315 launchSite Q845774.
- Q719315 lowerEarthOrbitPayload "2.08656E7".
- Q719315 maidenFlight "1966-02-26".
- Q719315 manufacturer Q181114.
- Q719315 manufacturer Q651778.
- Q719315 mass "5.89779792E8".
- Q719315 rocketFunction Q190776.
- Q719315 rocketFunction Q257161.
- Q719315 rocketFunction Q430728.
- Q719315 rocketFunction Q54363.
- Q719315 rocketStages "2".
- Q719315 status "Retired".
- Q719315 successfulLaunches "9".
- Q719315 thumbnail Saturn_IB_launch_configurations.jpg?width=300.
- Q719315 totalLaunches "9".
- Q719315 wikiPageExternalLink 19740021163_1974021163.pdf.
- Q719315 wikiPageExternalLink 19710065502_1971065502.pdf.
- Q719315 wikiPageExternalLink www.apollosaturn.com.
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