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Saturn V Rocket Essay

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The research that I have done is about a space station with a design based off of the Saturn V rocket that I have made. During this paper i will talk about its background, the parts, how it works and how it is different from the ISS (International Space Station). The Saturn V rocket has 3 stages in its launch. The first stage carries around 203,400 gallons (770,000 liters) of kerosene fuel and 318,000 gallons (1.2 million liters) of liquid oxygen needed for combustion. At liftoff the F-1 rocket engines produces 7.5 million pounds of thrust. The Saturn V rocket was a rocket that used the tallest and heaviest rocket for low earth orbit (LEO). It was launched 13 times with no loss of crew or payload. The Saturn V was designed under the direction …show more content…

The Saturn V rockets used for the Apollo missions had three stages. Each stage would burn its engines until it was out of fuel and would then separate from the rocket. The engines on the next stage would fire, and the rocket would continue into space. The first stage had the most powerful engines, since it had the challenging task of lifting the fully fueled rocket off the ground. The first stage lifted the rocket to an altitude of about 68 kilometers or 42 miles. The second stage carried it from there almost into orbit. The third stage placed the Apollo spacecraft into Earth orbit and pushed it toward the moon. The first two stages fell into the ocean after separation. The third stage either stayed in space or hit the moon. Now we will talk about how fast the Saturn V rocket can go. In order for the Saturn V rocket to break free of the Earth’s gravitational pull, it will need to travel approximately 7 miles per second. The fastest speed obtained by a manned vehicle orbiting the moon to Earth in 1969 is 11.08km/s or 24,791 miles per hour. After the launch the Saturn V burned for almost 6 minutes giving it a velocity close to the Earth’s escape velocity of 11.2 km/s or 25,053 miles per

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