Absolutely. Various rocket fuels are rated in "Specific Impulse", which is how much kick you get for how much fuel mass (or weight). This strongly influences the choice of fuels. Hydrogen and Oxygen is VERY high. Methane and Oxygen....not so much.
The three basic parts of a rocket are the rocket engine, which provides thrust for liftoff, the propellant tanks, which store the fuel and oxidizer, and the payload, which is the cargo the rocket is carrying into space.
There are choice of solid liquid and gas fuel propellant. For space discovery rocket it is usually use liquefied hydrogen and oxygen as fuel. Missile and ICBM use solid propellant for long storage time. Choice is depend on the type and need.
Inside a rocket, you will typically find a payload, which is the object the rocket is carrying into space. This could be a satellite, a spacecraft, or scientific instruments. Additionally, there will be a propulsion system, such as engines and fuel tanks, that provide the thrust needed to propel the rocket into space.
Rockets carry their own oxidizer to burn their fuel in space, as there is no oxygen available in space for combustion. The fuel and oxidizer react together in the rocket engine to produce thrust, allowing the rocket to move forward. This allows rockets to function in the vacuum of space where there is no atmospheric oxygen.
Rockets in space carry both the fuel and oxidizer with them into space.
Off course it will. The average bullet contains a propellant and an oxidizer, so a lack of oxygen is not going to be a problem.
The main ingredient of the Space Shuttle Solid Rocket Boosters by weight is Ammonium Perchlorate, at 69.6% of the solid fuel composition. Ammonium perchrlorate serves as the oxidizer in the shuttle SRBs. The next ingredient at 16% is aluminum, which is the primary fuel in the boosters. The remaining percentage is composed of binders and catalyst substances.
Oxidizer in rockets typically comes from liquid oxygen (LOX), which reacts with the fuel to produce combustion and generate thrust. This combination of fuel and oxidizer allows the rocket engines to burn efficiently in the vacuum of space.
The part of the rocket where the flames come out is called the rocket engine or rocket nozzle. This is where the fuel and oxidizer mix and ignite to produce thrust that propels the rocket through the atmosphere or space.
Well, honey, a rocket gets its energy from burning rocket fuel, usually a combination of liquid hydrogen and liquid oxygen. This fiery mix creates a whole lot of thrust that propels the rocket up into the wild blue yonder. So, next time you see a rocket shoot off into space, just remember it's all thanks to some good ol' rocket fuel doing its thing.
As regards the main engines on the rocket, there is an ignitor associated with each rocket motor. An internal "blowtorch" of fuel and oxidizer in each engine is ignited with spark plugs.
The Space Shuttle's External Tank carries 383,000 gallons of liquid hydrogen and 143,000 gallons of liquid oxygen to power the Space Shuttle Main Engines. The SSMEs burn for about 8.5 minutes (510 seconds), which means they consuming about 751 gallons of hydrogen per second and 280 gallons of oxygen per second, or about 1031 gallons of propellant overall per second. As an aside, the Solid Rocket Boosters each carry 1,000,000 pounds of solid propellant (both fuel and oxidizer are combined) and burn for about two minutes. So, that equates to about 16,667 pounds of propellant per second for the SRBs.