False it is Liquid hydrogen.
Most rockets use liquid oxygen (LOX) as an oxidizer to burn fuel, such as liquid hydrogen or kerosene. This combination creates a chemical reaction that produces thrust to propel the rocket.
A Russian Soyuz rocket uses a combination of liquid oxygen and refined kerosene (RP-1) as fuel. This combination provides the necessary energy to power the rocket during its launch into space.
The Saturn V rocket used a combination of liquid oxygen and RP-1, a refined form of kerosene, as fuel. These propellants were used in the first stage of the rocket to provide the thrust needed for liftoff.
The density of rocket fuel can vary depending on the type of fuel being used. For example, the density of liquid hydrogen fuel is about 70.85 kg/m^3, while the density of RP-1 (a type of kerosene) is about 810 kg/m^3. Solid rocket fuel densities can range from about 1,000 to 1,900 kg/m^3.
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.
No. Jet fuel is closely related to kerosene and diesel fuel.
The fuel inside a rocket can vary depending on the type of rocket. Common rocket fuels include liquid hydrogen, liquid oxygen, kerosene, and solid propellants like ammonium perchlorate. These fuels are used to generate the energy needed to propel the rocket into space.
Fuel : for example - kerosene (= jet fuel), alcohol, hydrogen.
Most rockets use liquid oxygen (LOX) as an oxidizer to burn fuel, such as liquid hydrogen or kerosene. This combination creates a chemical reaction that produces thrust to propel the rocket.
Kerosene is a fraction of petroleum that is less volatile than gasoline. Kerosene was first used in lamps as a replacement for whale oil. Its main use now is as jet aircraft fuel (usually JP-1 but there are higher grades), it is also used as fuel in some rocket motors (usually RP-1 but there are higher grades), also kerosene heaters, etc.
A Russian Soyuz rocket uses a combination of liquid oxygen and refined kerosene (RP-1) as fuel. This combination provides the necessary energy to power the rocket during its launch into space.
The Saturn V rocket used a combination of liquid oxygen and RP-1, a refined form of kerosene, as fuel. These propellants were used in the first stage of the rocket to provide the thrust needed for liftoff.
The density of rocket fuel can vary depending on the type of fuel being used. For example, the density of liquid hydrogen fuel is about 70.85 kg/m^3, while the density of RP-1 (a type of kerosene) is about 810 kg/m^3. Solid rocket fuel densities can range from about 1,000 to 1,900 kg/m^3.
Kerosene is a fraction of petroleum that is less volatile than gasoline. Kerosene was first used in lamps as a replacement for whale oil. Its main use now is as jet aircraft fuel (usually JP-1 but there are higher grades), it is also used as fuel in some rocket motors (usually RP-1 but there are higher grades), also kerosene heaters, etc.
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.
The name of a common rocket fuel is liquid hydrogen, which is often used in combination with liquid oxygen. There are also other types of rocket fuels including solid fuels and hybrid fuels, but liquid hydrogen is one of the most commonly used.
Rocket fuel is typically made by combining liquid oxygen (LOX) with a fuel source such as liquid hydrogen, kerosene, or a combination of various chemicals. These components are mixed in specific ratios to optimize performance and efficiency. The fuel is then stored in tanks on the rocket until it is ignited during the launch process.