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.
There are two ways to do that: -- The fuel that the rocket burns has its own oxygen combined with the other chemicals in the fuel. -- The rocket carries oxygen in a separate tank, and mixes it with the fuel in order for the fuel to burn.
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).
solid liquid
It is a solid
A solid.
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.
There are two main types of fuel: solid fuel and liquid fuel. Rocket fuel most use both a fuel and an oxidizer. The solid fuel in most modern rockets uses aluminum powder as fuel, ammonium perchlorate as an oxidizer, and iron oxide as a catalyst. Liquid fuel uses liquid hydrogen as fuel and liquid oxygen as an oxidizer.
There are several types of rocket motors, including solid rocket motors, liquid rocket engines, and hybrid rocket engines. Solid rocket motors use a solid propellant that burns uniformly, providing thrust until the fuel is consumed. Liquid rocket engines utilize liquid fuel and oxidizer, allowing for adjustable thrust and the ability to shut down and restart. Hybrid rocket engines combine aspects of both, using a solid fuel and a liquid oxidizer, offering some advantages in performance and safety.
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.
Rocket propellents are chemical substances that produce thrust by expelling mass at high velocity, enabling rockets to propel themselves in space. They are classified into two main categories: liquid propellents, which consist of a fuel and an oxidizer stored separately and combined in a combustion chamber, and solid propellents, where the fuel and oxidizer are mixed together in a solid form. Additionally, there are hybrid propellents that combine features of both liquid and solid types, using a solid fuel and a liquid oxidizer. The choice of propellant affects the rocket's performance, efficiency, and application.
Yes. Solid rocket fuel contains its own oxidizer.
Some rockets, such as liquid fuel rockets, carry liquid oxygen (LOX) as an oxidizer in a separate tank. The LOX is then mixed with the rocket's fuel and ignited to create thrust. Other rockets, like solid fuel rockets, have an oxidizer mixed into their solid fuel composition.
Missiles are typically propelled by rocket engines that use various types of propellant gases. These gases are generated from the combustion of solid or liquid fuels combined with an oxidizer. In solid rocket motors, the propellant is a mixture of fuel and oxidizer that is preloaded into the casing, while liquid rocket engines burn separate fuel and oxidizer, producing high-pressure gases that are expelled to create thrust. The rapid expansion and ejection of these gases generate the necessary force to propel the missile.
There are solid rocket fuels, and there are liquid rocket fuels.
The two types of rocket fuel are liquid fuel and solid fuel. Liquid fuel rockets use a combination of liquid propellants, such as liquid oxygen and liquid hydrogen, that are mixed and burned to create thrust. Solid fuel rockets have a solid mixture of fuel and oxidizer that is ignited to produce thrust.
In a solid rocket engine, the oxidizer is a chemical component that provides the necessary oxygen for combustion of the fuel. Common oxidizers used include ammonium perchlorate or ammonium nitrate, which are mixed with a fuel to create a propellant that burns to produce thrust. The oxidizer is integral to the solid propellant formulation, enabling the rocket to operate in the absence of atmospheric oxygen.
Rockets typically use either liquid or solid propulsion engines. Liquid engines burn a combination of liquid fuel and oxidizer, allowing for adjustable thrust and the ability to shut down and restart. Solid rocket motors, on the other hand, contain a pre-loaded mixture of fuel and oxidizer that burns once ignited, providing a simpler design but less control over thrust. Some advanced rockets also utilize hybrid engines that combine elements of both liquid and solid propulsion.