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 injection (TLI).
Saturn V - Wikipedia
Projected to place approximately 400,000 pounds (180 t) into orbit, the Ares V would have surpassed the Saturn V in payload capability. An upper stage, the Earth Departure Stage, would have utilized a more advanced version of the J-2 engine, the J-2X. Ares V would have placed the Altair lunar landing vehicle into low Earth orbit.
J002E3 - Wikipedia
J002E3 is an object in space which is thought to be the S-IVB third stage of the Apollo 12 Saturn V rocket. It was discovered on September 3, 2002, by amateur astronomer Bill Yeung.
Rocket Propulsion Evolution: 8.30 - S-IVB Stage
2021年8月1日 · The Saturn S-IVB was the second Saturn IB booster stage and third Saturn V booster stage. While the two versions had much in common, they differed in aft interstage, ullage motor count, and auxiliary propulsion system (APS) details.
NASA SVS | Apollo 13 S-IVB Impact Site - NASA Scientific …
2020年4月6日 · After sending the astronauts out of Earth orbit on a path to the Moon, the detached upper stage of the Saturn V rocket, called the S-IVB (“ess four bee”), was aimed squarely at the Moon. Its impact at 77:56:39.7 mission elapsed time was detected by several scientific instruments left on the surface by Apollo 12.
Saturn V S-IVB Stage at Redstone Airfield - NASA
2014年1月31日 · In January 1968, the Saturn V S-IVB stage that housed the orbital workshop, which was renamed Skylab was unloaded from the Super Guppy, the NASA plane built to carry oversized cargo, at Redstone Airfield in Huntsville, Ala.
Saturn V - Encyclopedia Astronautica
Saturn variant with 4 to 12 Minuteman motors as boosters, Saturn II stage as core, and Saturn IVB upper stage. Saturn II stage would be fitted with lower expansion ratio engines and would ignite at sea level.
Season of Apollo - Part Three - Saturn V - nastarcenter.com
The Saturn V had three stages. Stage 1, called the S-IC, was 138 feet long and 33 feet in diameter. It had five F-1 engines. Each engine generated just over 1.5 million pounds’ thrust, giving the Saturn a lift off thrust of 7.6 million pounds. The power output of the S-IC was about 160 million horsepower.
Saturn V - Project Apollo - NASSP
The largest production model of the Saturn family of rockets, the Saturn V was designed under the direction of Wernher von Braun at the Marshall Space Flight Center in Huntsville, Alabama, with Boeing, North American Aviation, Douglas Aircraft …
Saturn V - Wikiwand
Other plans for the Saturn V called for using a Centaur as an upper stage or adding strap-on boosters. These enhancements would have enabled the launch of large robotic spacecraft to the outer planets or the sending of astronauts to Mars .