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The Saturn V dynamic test vehicle, designated SA-500D, is a prototype Saturn V rocket used by NASA to test the performance of the rocket when vibrated to simulate the shaking which subsequent rockets would experience during launch. It was the first full-scale Saturn V completed by the Marshall Space Flight Center (MSFC).
Another ten engines were installed on two ground-test Saturn Vs never intended to fly. The S-IC-T "All Systems Test Stage," a ground-test replica, is on display as the first stage of a complete Saturn V at the Kennedy Space Center in Florida. SA-500D, the Dynamic Test Vehicle, is on display at the U.S. Space and Rocket Center in Huntsville ...
The dynamic test unit was later installed atop the Saturn IB dynamic test stage in Marshall's Saturn I-IB dynamic test stand where it underwent testing as part of the Saturn IB vehicle. A ceremony at Douglas Aircraft Co. Huntington Beach, California facility, Ealry December marked the turnover to NASA of the first S-IV-B stage built by the company.
During these revisions, the team rejected the single engine of the V-2's design and moved to a multiple-engine design. [34] The Saturn V's final design had several key features. F-1 engines were chosen for the first stage, [9] while new liquid hydrogen propulsion system called J-2 for the second and third stage.
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Boeing, Saturn V Launch Vehicle Guidance Equations, SA-504, 15 July 1967; Haeussermann, Walter (July 1970). Description and Performance Of The Saturn Launch Vehicle's Navigation, Guidance And Control System (PDF). NASA TN D-5869. NASA Marshall Spaceflight Center, Saturn V Flight Manual SA-503, 1 November 1968
The new building was so tall that in 1966 when the Saturn V first stage was entering, an observer noted, "Fog and clouds hovered around the top of the 360 foot (110 m) tall test stand most of the day while the 300,000 pounds (140,000 kg) stage was being lifted from its transporter into place inside the stand, said to be the tallest building in ...
The J-2, commonly known as Rocketdyne J-2, was a liquid-fuel cryogenic rocket engine used on NASA's Saturn IB and Saturn V launch vehicles. Built in the United States by Rocketdyne, the J-2 burned cryogenic liquid hydrogen (LH 2) and liquid oxygen (LOX) propellants, with each engine producing 1,033.1 kN (232,250 lb f) of thrust in vacuum.