the space shuttle uses liquid hydrogen and oxygen from the external tank (the great big orange
cylinder that the orbiter is attached to for launch); and the SRBs (Solid
Rocket Boosters) burn a solid rocket propellant that is a mixture of
powdered aluminum and ammonium perchlorate. These are used only for launch.
The orbiter (what most people think of as "the Space Shuttle") has two
propulsion systems: OMS (Orbital Maneuvering System) used to change orbit and
to return to earth, and the RCS (Reaction Control System) used for station-
keeping and attitude control both burn hydrazine with oxygen.
The oxygen in a rocket can come from either cryogenic liquid oxygen stored onboard the rocket, or from onboard solid rocket fuel that contains its own oxidizer, such as ammonium perchlorate. In both cases, the oxygen is used during the combustion process to react with the fuel and generate thrust.
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.
Rockets are propelled into space using liquid or solid propellants. Liquid propellants typically consist of liquid oxygen or hydrogen as the oxidizer and a fuel such as liquid hydrogen or kerosene. Solid propellants are a mixture of fuel and oxidizer that are combined into a solid form.
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.
Only liquid fuelled rockets (and then only some) rely on oxygen as the oxidizer. It is carried in liquid form in a tank (or tanks). It is them pumped and mixed with the fuel in the combustion chamber where the combustion reaction takes place. The combusion products then exit the rocket nozzle. In solid fuel rockets, the oxidizer (whatever that may be) is usually mixed with the fuel.
liquid Hydrogen + liquid Oxygen
liquid Hydrogen + liquid Oxygen
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.
Liquid hydrogen and liquid oxygen oxidizer.
The oxygen is carried in tanks as a liquid, just as the fuel is.
The oxygen in a rocket can come from either cryogenic liquid oxygen stored onboard the rocket, or from onboard solid rocket fuel that contains its own oxidizer, such as ammonium perchlorate. In both cases, the oxygen is used during the combustion process to react with the fuel and generate thrust.
Yes. Solid rocket fuel contains its own oxidizer.
Liquid oxygen and liquid hydrogen are used as rocket fuel, oxygen gas is used by the astronauts to breath.
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.
gasoline along with liquid oxygen, so the fuel can burn
Rockets are propelled into space using liquid or solid propellants. Liquid propellants typically consist of liquid oxygen or hydrogen as the oxidizer and a fuel such as liquid hydrogen or kerosene. Solid propellants are a mixture of fuel and oxidizer that are combined into a solid form.
liquid fuel