It depends upon the weight of the total vehicle and the payload combined (including the fuel, which needs to be carried upward too). For more information, see the link below the ads.
The Saturn V can carry 385.6 tonnes of propellant according to pg 244 in "The Rocket: The History and Development of Rocket & Missile Technology"
How much fuel will be needed in a rocket will depend on the size of the rocket and where it is going. A rocket that will be traveling into space burns a lot of fuel and will need enough to keep it in orbit for teh desired time.
The Saturn V rocket used for the Apollo 13 mission required approximately 2.5 million liters (660,000 gallons) of fuel. This fuel consisted of liquid oxygen (LOX) as the oxidizer and refined kerosene (RP-1) as the fuel.
It would take approximately 2.9 kilometers per second of delta-v to reach the moon. The amount of fuel needed depends on the specific rocket design, but it is typically a large amount due to the distance and gravitational forces involved in the journey.
It would require a significant amount of fuel to put one pound in space, as rockets need a large amount of fuel to overcome Earth's gravity and reach escape velocity. The exact amount of fuel needed would depend on the specific rocket and launch conditions.
It depends on the weight of the rocket and payload. The Saturn 5 that carried the Apollo moon missions into space carried 5.5 million pounds (2.5 million kilograms) of fuel. Most of the fuel is used to lift the fuel.
How much fuel will be needed in a rocket will depend on the size of the rocket and where it is going. A rocket that will be traveling into space burns a lot of fuel and will need enough to keep it in orbit for teh desired time.
500,000,000
The Saturn V rocket used for the Apollo 13 mission required approximately 2.5 million liters (660,000 gallons) of fuel. This fuel consisted of liquid oxygen (LOX) as the oxidizer and refined kerosene (RP-1) as the fuel.
It would take approximately 2.9 kilometers per second of delta-v to reach the moon. The amount of fuel needed depends on the specific rocket design, but it is typically a large amount due to the distance and gravitational forces involved in the journey.
It would require a significant amount of fuel to put one pound in space, as rockets need a large amount of fuel to overcome Earth's gravity and reach escape velocity. The exact amount of fuel needed would depend on the specific rocket and launch conditions.
It depends on the weight of the rocket and payload. The Saturn 5 that carried the Apollo moon missions into space carried 5.5 million pounds (2.5 million kilograms) of fuel. Most of the fuel is used to lift the fuel.
The amount of fuel a rocket needs to take off depends on its size, payload, and destination. However, rockets are designed to be as fuel-efficient as possible to maximize payload capacity and range. The fuel needed for a rocket launch is carefully calculated by engineers to ensure a successful mission.
At the very bottom is the nozzle, after that is the fuel. Depending on how big the rocket is and how much fuel it needs determines the size of the chamber
The amount of fuel a rocket carries can vary greatly depending on its size, purpose, and destination. For example, the Saturn V rocket used in the Apollo program carried over 3 million kilograms of fuel. Today's Falcon 9 rocket from SpaceX typically carries around 400,000 kilograms of fuel.
The approximate minimum power required to put a manned rocket into space is around 2 million horsepower. This power is needed to overcome Earth's gravity, propel the rocket to the necessary speed to enter orbit, and provide thrust for the journey.
The fuel consumption of a rocket launch can vary, but as a rough estimate, a single rocket launch uses several hundred thousand gallons of fuel.
The amount of fuel needed for space travel can vary greatly depending on the distance, speed, and payload of the spacecraft. However, typically a spacecraft will require a significant amount of fuel to overcome Earth's gravity and reach orbital velocity, with additional fuel needed for course corrections, maneuvers, and deceleration upon reaching the destination.