
The Saturn V rocket, developed by NASA, was a retired American super heavy-lift launch vehicle used for human exploration of the Moon. It was the most powerful rocket of its time, with a height of 363 feet (111 meters) and a weight of 2.8 million kilograms or 6.2 million pounds when fully fueled. The rocket's first flight took place on November 9, 1967, and it was used for nine crewed flights to the Moon, as well as launching the Skylab space station. With its three stages and liquid fuel, the Saturn V could generate 34.5 million newtons (7.6 million pounds) of thrust at launch, showcasing its immense power and capability to send humans beyond low Earth orbit.
| Characteristics | Values |
|---|---|
| Fully fueled weight | 2,822,171 to 2,965,241 kg (6,221,823 to 6,537,238 lb) or 6.2 million lb |
| Height | 363 feet (111 m) tall |
| Diameter | 33 feet (10 m) |
| Payload capacity | 140,000 kg (310,000 lb) |
| Payload to the Moon | 43,500 kg (95,900 lb) |
| First stage fuel | 203,400 gallons or 770,000 liters of kerosene fuel |
| First stage oxidizer | 318,000 gallons or 1.2 million liters of liquid oxygen |
| First stage thrust | 7,500,000 lbf (33,000 kN) or 7.5 million lb |
| First stage burn time | 150 seconds |
| Second stage burn time | 395 seconds |
| Third stage burn time | 165 seconds (first burn) and 312 seconds (second burn) |
| First crewed flight | Apollo 8 |
| First crewed moon landing | Apollo 11 |
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What You'll Learn

The Saturn V rocket's weight is 6.2 million pounds or 2.8 million kilograms
The Saturn V rocket was a retired American super heavy-lift launch vehicle developed by NASA under the Apollo program for human exploration of the Moon. The rocket was human-rated, had three stages, and was powered by liquid fuel. It stood 363 feet (111 m) tall, about the height of a 36-story building, and was 60 feet (18 m) taller than the Statue of Liberty.
The Saturn V rocket was primarily built of aluminum, with some parts made of titanium and non-metal materials like urethane foam and cork. All the materials were chosen for their low weight and high strength characteristics. The rocket's first flight took place on November 9, 1967, and it was used for nine crewed flights to the Moon, as well as to launch Skylab, the first American space station.
The Saturn V rocket was a powerful machine, with a fully fueled weight of 6.2 million pounds or 2.8 million kilograms. This is the equivalent of about 400 elephants. The rocket generated an impressive 34.5 million newtons (7.6 million pounds) of thrust at launch, creating more power than 85 Hoover Dams.
The first stage of the Saturn V rocket used five F-1 rocket engines and produced 7.5 million pounds (3.4 million kilograms) of thrust. It burned through 20 tons (40,000 pounds) of fuel per second, which is an incredible rate of fuel consumption. The second stage of the rocket used liquid hydrogen and liquid oxygen, with five Rocketdyne J-2 engines. The third stage placed the Apollo spacecraft into Earth orbit and pushed it towards the Moon.
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That's the weight of 400 elephants
The Saturn V rocket was a large rocket developed by NASA to send people to the moon. It was used for nine crewed flights to the Moon and to launch Skylab, the first American space station. Standing at 363 feet (111 metres) tall, it was about the height of a 36-storey building and 60 feet taller than the Statue of Liberty. The rocket was so powerful that it could generate 34.5 million newtons (7.6 million pounds) of thrust at launch, which is more power than 85 Hoover Dams.
When fully fuelled, the Saturn V rocket weighed 6.2 million pounds (2.8 million kilograms). This is the equivalent of about 400 elephants. To put that into context, an average-sized African elephant weighs around 12,000 pounds (5,443 kilograms), while Asian elephants, which tend to be smaller, weigh between 5,000 and 11,000 pounds (2,268 and 4,989 kilograms).
The Saturn V rocket was so heavy that it required an enormous amount of fuel to lift off. A car that gets 30 miles to the gallon could drive around the world around 800 times with the amount of fuel the Saturn V used for a lunar landing mission. This massive rocket was developed at NASA's Marshall Space Flight Center in Huntsville, Alabama, and it remains a testament to human ingenuity and our pursuit of exploration beyond Earth's bounds.
The Saturn V rocket's weight of 6.2 million pounds when fully fuelled is an astonishing feat of engineering and a reminder of the capabilities of human technology. This weight is equivalent to about 400 elephants, highlighting the sheer magnitude and power of this rocket.
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The first stage of the Saturn V uses 203,400 gallons of kerosene fuel
The Saturn V rocket, developed by NASA, was a retired American super heavy-lift launch vehicle used for human exploration of the Moon. Standing at 363 feet (111 metres) tall, it was a powerful rocket that could carry a significant payload.
The first stage of the Saturn V rocket used 203,400 gallons of kerosene fuel, also known as RP-1. This fuel was combined with 318,000 gallons of liquid oxygen, creating a powerful mixture known as kerolox. The kerosene fuel played a crucial role in providing the necessary thrust for the rocket's launch.
The first stage of the Saturn V required a significant amount of fuel to lift the massive rocket off the ground. With a total of five F-1 rocket engines, this stage produced an impressive 7.5 million pounds of thrust at liftoff. The kerosene fuel, being denser than liquid hydrogen, contributed to the overall weight of the rocket's first stage.
The choice of kerosene as the primary fuel for the first stage of the Saturn V had several considerations. While kerosene provided the needed thrust and density, it also had some drawbacks. One issue was the production of soot, which could potentially clog the rocket engines. Additionally, kerosene tends to freeze when in space for extended periods, limiting the operational time of the rocket.
Despite these challenges, the Saturn V rocket's first stage fuel system was designed to provide the necessary power and thrust to lift the rocket and its payload into orbit. The combination of kerosene and liquid oxygen in the first stage set the Saturn V rocket in motion, contributing to its successful missions to the Moon.
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It also uses 318,000 gallons of liquid oxygen
The Saturn V rocket was a launch vehicle developed by NASA under the Apollo programme for human exploration of the Moon. It was first tested in 1967 and was used for nine crewed flights to the Moon. It was the most powerful rocket that had ever flown successfully.
The Saturn V rocket used kerosene and liquid hydrogen fuels across its three stages. The first stage carried 203,400 gallons of kerosene (RP-1) and 318,000 gallons of liquid oxygen. This combination provided the massive thrust needed to lift the rocket off the launchpad. The first stage lifted the rocket to an altitude of about 68 kilometres (42 miles) before the F-1 engines shut down and the first stage fell into the Atlantic Ocean.
The second stage carried 260,000 gallons of liquid hydrogen fuel and 80,000 gallons of liquid oxygen. The second stage carried the rocket almost into orbit. The third stage placed the Apollo spacecraft into Earth orbit and pushed it towards the Moon. The third stage also used liquid hydrogen and liquid oxygen for maximum efficiency in space. This stage was critical for the Trans-Lunar Injection (TLI) burn that sent Apollo astronauts to the Moon.
Liquid hydrogen and oxygen don't freeze in space, unlike kerosene. This makes hydrogen ideal for major burns during flight in space. Kerosene, however, is denser than liquid hydrogen, reducing the volume and weight of the tankage.
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The rocket burns 20 tons of fuel per second
The Saturn V rocket was a powerful rocket built by NASA to send people to the moon. It was used for nine crewed flights to the moon and to launch Skylab, the first American space station. The Saturn V rocket burned 20 tons of fuel per second.
The rocket was developed at NASA's Marshall Space Flight Center in Huntsville, Alabama, and was one of three types of Saturn rockets NASA built. It was the largest production model of the Saturn family of rockets and was designed under the direction of Wernher von Braun. The Saturn V was a retired American super heavy-lift launch vehicle that stood 363 feet (111 m) tall, about the height of a 36-story building, and was 60 feet taller than the Statue of Liberty. Fully fueled for liftoff, the Saturn V weighed about 6.2 million pounds, or 2.8 million kilograms, which is the weight of about 400 elephants.
The Saturn V had three stages, each of which would burn its engines until it ran out of fuel and then separate from the rocket. The engines on the next stage would then fire, and the rocket would continue into space. The first stage had the most powerful engines, as 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 42 miles, while the second stage carried it almost into orbit. The third stage placed the Apollo spacecraft into Earth orbit and propelled it toward the moon.
The Saturn V rocket was human-rated and powered by liquid fuel. It had a low Earth orbit (LEO) payload capacity of about 140,000 kilograms (310,000 lb), and could send about 43,500 kilograms (95,900 lb) to the Moon. The rocket generated 34.5 million newtons (7.6 million pounds) of thrust at launch, creating more power than 85 Hoover Dams. The Saturn V burned a mixture of RP-1 fuel and liquid oxygen as the oxidizer.
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Frequently asked questions
The Saturn V rocket weighed 2.8 million kilograms or 6.2 million pounds when fully fueled for liftoff.
The fully fueled Saturn V rocket weighed about 400 elephants.
The Saturn V rocket's first stage carried 203,400 gallons or 770,000 liters of kerosene fuel and 318,000 gallons or 1.2 million liters of liquid oxygen.
The Saturn V rocket burned 40,000 pounds of fuel per second during launch, which equates to 10 times more fuel than Lindbergh's aircraft used for his entire trip across the Atlantic.
The first flight of the Saturn V rocket was on November 9, 1967, for the Apollo 4 mission.








































