For liquid fuel systems it may be: "Liquid hydrogen and liquid oxygen - used in the Space Shuttle main engines * Gasoline and liquid oxygen - used in Goddard's early rockets * Kerosene and liquid oxygen - used on the first stage of the large Saturn V boosters in the Apollo program * Alcohol and liquid oxygen - used in the German V2 rockets * Nitrogen tetroxide/monomethyl hydrazine - used in the Cassini engines".
For solid fuel rocks, it may be a mixture of 72% nitrate, 24% carbon and 4% sulfur. See the link for more info. If you mean the stuff that is used in the giant fuel tank that is attached to a departing space shuttle, then it is almost entirely liquid O2 (liquid oxygen). However "rocket fuel" is defined as: Any of the substances or mixtures of substances that can burn rapidly with controlled combustion to produce large volumes of gas at high pressures and temperatures; includes monopropellants (hydrogen peroxide and hydrazine), liquid bipropellant fuels (organic fuel and oxidizer), and solid propellants (mixed oxidizer-fuel in a propellant grain).
In a model rocket, the oxidizer is typically a solid. Common solid oxidizers used in model rocket propellant include ammonium perchlorate and ammonium nitrate, which are mixed with a fuel to create a combustion reaction. While there are also liquid and gas oxidizers in some rocket designs, solid oxidizers are most prevalent in model rocketry due to their stability and ease of handling.
It can. The design of the fuselage could affect the range: a long fuselage may be less rigid and so reduce the range. However, the fuselage needs to contain all the fuel and if the fuselage is too short the model may not contain much fuel. Alternatively, the fuselage will be short and squat which will reduce its aerodynamics and the increased drag will reduce the range.
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.
Helium is not typically used as a fuel in rockets. It is most commonly used in rocket propulsion systems as a pressurizing agent in liquid fuel rockets to push the fuel into the combustion chamber for efficient burning.
An example of a motor that burns fuel without air is a solid fuel rocket motor. These motors contain both fuel and oxidizer within the fuel itself, allowing combustion to occur without the need for external air.
Modern model rocket fuel is a solid fuel.
Solid fuel
Please see related link below.
Rocket Fuel. Ozone. Air.
There are two main types of rocket engines: Solid fuel and liquid fuel. Liquid fuel rocket engines are usually considered significantly better than solid propulsion units, however, they are also significantly more expensive.
"Model rocket fuel" is basically in the form of single-shot engines. You could, I suppose, strap one to a stick and call it a "bottle rocket", but I don't think it would fly very well (and the engine would likely burn off the stick).
somethinjg that burns good, soaked in gas, and compressed.
Yes, yes it will. How it will respond will depend primarily on the chemicals used.
The fisrt liquid fuel was made in 1926
Rocket fuel is typically stored in fuel tanks within the rocket's structure. The tanks are often made of lightweight materials such as aluminum or composite materials to minimize weight. The fuel may be stored separately from the oxidizer in different tanks, or they may be stored together as a single fuel mixture.
liquid fuel
Thrust (due to solid or liquid fuel burning)