Rockets typically use a variety of propellants, which can be broadly categorized into liquid and solid types. Liquid rockets often use a combination of liquid fuel (like liquid hydrogen or RP-1) and an oxidizer (such as liquid oxygen). Solid rockets utilize a preloaded mixture of fuel and oxidizer in a solid form. The choice of propellant depends on the mission requirements and rocket design.
A rocket's fuel is typically located in large tanks situated within the rocket's body. The fuel is stored separately from the rocket's engines and is used as propellant for thrust during launch and flight.
The rocket to launch Apollo 13 was the Saturn 5 rocket.
according to Boeing the Saturn V contained 5.6 million pounds of propellant (or 960,000 gallons).
A Soviet carrier rocket used to launch spacecraft.
The white smoke seen during a shuttle launch is caused by the ignition of the solid rocket boosters. It consists of exhaust gases and steam produced by the burning of solid propellant.
A rocket's fuel is typically located in large tanks situated within the rocket's body. The fuel is stored separately from the rocket's engines and is used as propellant for thrust during launch and flight.
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The rocket to launch Apollo 13 was the Saturn 5 rocket.
according to Boeing the Saturn V contained 5.6 million pounds of propellant (or 960,000 gallons).
A Soviet carrier rocket used to launch spacecraft.
The white smoke seen during a shuttle launch is caused by the ignition of the solid rocket boosters. It consists of exhaust gases and steam produced by the burning of solid propellant.
The amount of gasoline used by a rocket ship depends on the size and type of rocket. Rockets do not use gasoline as fuel; they typically use liquid hydrogen, liquid oxygen, or solid rocket propellant. The amount of propellant consumed by a rocket is based on factors such as the rocket's size, intended mission, and duration of flight.
Two common types of rocket propellant are liquid propellant and solid propellant. Liquid propellant consists of fuel and oxidizer stored separately and combined in the combustion chamber, allowing for controlled thrust and engine shutoff. Solid propellant, on the other hand, consists of a mixture of fuel and oxidizer that is preloaded into the rocket, providing a simpler design but less control over the burn once ignited. Each type has its advantages and applications in different rocket systems.
The length of time from ignition of propellant to when all propellant has been consumed.
The rocket is launched upward into the sky during a rocket launch.
Ronald Toelle has written: 'A 20k payload launch vehicle fast track development concept using an RD-180 engine and a Centaur upper stage' -- subject(s): Liquid propellant rocket engines, Concurrent engineering, Aerodynamic configurations, Launch vehicle configurations, Payloads, Upper stage rocket engines, Centaur launch vehicle
The propellant