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S-IVB - Wikipedia
The S-IVB (pronounced "S-four-B") was the third stage on the Saturn V and second stage on the Saturn IB launch vehicles. Built by the Douglas Aircraft Company, it had one J-2 rocket engine. For lunar missions it was fired twice: first for Earth orbit insertion after second stage cutoff, and then for translunar … See more
A surplus S-IVB tank, serial number 212, was converted into the hull for Skylab, the first American space station. Skylab was launched on a Saturn V on May 14, 1973, and it eventually … See more
Douglas built two distinct versions of the S-IVB, the 200 series and the 500 series. The 200 series was used by the Saturn IB and differed from the 500 in that it did not have a flared … See more
The second stage of the Ares I rocket and the proposed Earth Departure Stage (EDS) would have had some of the characteristics of the S-IVB stage, as both would have had an uprated J-2 engine, called the J-2X, with the latter performing the same functions … See more
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S-IVB — Wikipédia
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S-IVB - Wikipedia
36 rows · S-IVB (英語 ではエス・フォー・ビーと発音される)は、 アメリカ合衆国 の アポロ計画 で使用された サターンV 型ロケット の第三段および サターンIB 型ロケット の第二段である。 ダグラス 社製造。 J-2ロケットエンジ …
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Saturn IB - Wikipedia
The Saturn IB[a] (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.
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S-IVB (Saturn IB) Overview - heroicrelics.org
The S-IVB, the second stage of the Saturn IB rocket, was the one of the largest liquid hydrogen stages produced in the 1960s. Equipped with one J-2 rocket engine , it produced about 200,000 pounds of thrust.
Category:Saturn S-IVB - Wikimedia Commons
Mar 26, 2024 · English: S-IVB was the third stage on the Saturn V and second stage on the Saturn IB.
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