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SA-500F was the first complete assembly of something resembling a Saturn V, and model makers quickly patterned their designs after its paint scheme, but engineers changed the black stripe to white in the intertank section of the first stage for flight vehicles after discovering the intertank got too hot from the heat of the Sun. The third stage ...
On Saturday April 25, 2009 Eves launched the 1/10 scale replica of the Saturn V rocket 4,441 feet (1,354 m) into the air, and successfully recovered it. [2] The launch occurred on the eastern shore of the Chesapeake Bay under supervision of the Maryland-Delaware Rocketry Association. The rocket was powered by a matrix of nine motors: eight 13 ...
The CSMs launched in orbit on Saturn IB ranged from 32,558 pounds (14,768 kg) (Apollo–Soyuz), to 46,000 pounds (21,000 kg) (Skylab 4). The omnidirectional antennas sufficed for ground communications during the Earth orbital missions, so the high-gain S-band antenna on the SM was omitted from Apollo 1, Apollo 7, and the three Skylab flights.
The Saturn V reached 400 feet per second (120 m/s) at over 1 mile (1,600 m) in altitude. Much of the early portion of the flight was spent gaining altitude, with the required velocity coming later. The Saturn V broke the sound barrier at just over 1 minute at an altitude of between 3.45 and 4.6 miles (5.55 and 7.40 km). At this point, shock ...
These sensors were connected to the CM and Saturn launch vehicle guidance computers, allowing calculation of dynamic pressure (q) during atmospheric flight and also the angle of attack in the event of an abort. [5] Q-ball cover A styrofoam cover, removed a few seconds before launch, protected the pitot tubes from being clogged by debris. [6]
S-IC-T was planned as a test rocket only and not to be used in the later Apollo program. The Saturn V rocket was used in the Apollo program to depart Earth's gravity. S-IC-T, like all following Saturn V's S-IC rockets used five Rocketdyne F-1 engines. The Rocketdyne F-1 engine was first tested in March 1959 and delivered to NASA in October 1963.
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
In 1999, a full-scale model of the Saturn V rocket was erected, standing nearly twice as tall as the Saturn I. [46] From 1979 to 2023 an unflown Saturn IB rocket owned by MSFC and leased to the museum stood at the Alabama Welcome Center in Ardmore "as a reminder to visitors of Alabama's role in the space program." It was removed and salvaged ...
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