Saturn I - Wikipedia
The S-I first stage was powered by eight H-1 rocket engines burning RP-1 fuel with liquid oxygen (LOX) as oxidizer. The propellant tanks consisted of a central Jupiter rocket tank containing LOX, surrounded by a cluster of eight Redstone rocket tanks: four painted white, containing LOX; and four painted black, containing the RP-1 fuel.
Rocketdyne F-1 - Wikipedia
The F-1 is a rocket engine developed by Rocketdyne. The engine uses a gas-generator cycle developed in the United States in the late 1950s and was used in the Saturn V rocket in the 1960s and early 1970s. Five F-1 engines were used in the S-IC first stage of each Saturn V, which served as the main launch vehicle of the Apollo program.
Saturn (rocket family) - Wikipedia
Three variants of the Saturn family which were developed: Saturn I, Saturn IB, and Saturn V The Saturn family of American rockets was developed by a team of former German rocket engineers and scientists led by Wernher von Braun to launch heavy payloads to Earth orbit and beyond.
Rocket Propulsion Evolution: 7 - Saturn I, IB - enginehistory.org
2021年3月1日 · The Saturn I used an S-I first stage that was 80.31 feet high, 21.39 feet in diameter, had a loaded mass of 953,898 lb. Eight Rocketdyne H-1 engines burning RP-1 and LOX provided 1,704,524 lbT and was able to launch a 19,800 lb payload into low earth orbit. Ten Saturn I rockets were built and launched, the first on 27 Oct 1961.
Saturn I and IB Rockets | Historic Spacecraft
The first Saturn rockets to fly were the Saturn I. Between 1961 and 1965, ten Saturn I rockets were launched. All were successful. The first four Saturn I missions were known as block 1. Block 1 missions flew with an S-I first stage, and dummy upper stages. The last six Saturn I missions were known as block 2.
What is the F-1 Engine? • 5 F-1 engines were used as the first stage engines, Saturn V moon rocket • Took the Apollo vehicle (363 ft tall, 6 million lbs): • 50 miles downrange • 40 miles altitude • At Mach 7 • In 2.5 minutes • Burning 4.5 million lbs of propellant
F-1 Rocket Engine | National Air and Space Museum
The F-1 engine, with 1.5 million pounds of thrust, was the powerplant for the first stage of the 363-foot long Saturn V launch vehicle that took astronauts to the Moon for six successful landing missions between 1969 and 1972 in the Project Apollo program.
Rocket Propulsion Evolution: 8.11 - F-1 Engine
2021年5月13日 · F-1 Under Test at MSFC (NASA) The Saturn V could have never achieved its objective of sending humans to Earth’s moon were it not for the F-1 engine. When work on the F-1 began, the most powerful production rocket engine produced around 150,000 lbT.
R-3896-1 (Technical Manual Engine Data) F-1 Rocket Engine
2022年9月7日 · One of the Manuals of the Rocketdyne F-1 Engine that powered the First Stage of the Saturn V, the S-IB.
Saturn I - Encyclopedia Astronautica
2016年7月28日 · With its eight clustered engines developing almost 1.3 million pounds of thrust at launch, the Saturn (SA-1) hurled waterfilled dummy upper stages to an altitude of 84.8 miles and 214.7 miles down range.
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