The three main elements are: FUEL, for solid or liquid engines. This is the part that actually burns. OXIDIZER, for both, as there is not enough oxygen in the fuel cell to cause combustion. Combustion causes expanding gasses and controlled release from the combustion chamber causes thrust. STABILIZER, mostly for solids, and used to maintain a consistent/even burn of the fuel.
The main characteristics of a rocket are the height and the width. That makes the rocket go higher.
A conclusion is a synopsis of the experiment, along with the findings of the experiment. It ties the entire project together.
A liquid-fuel rocket or a liquid rocket is a rocket with an engine that uses propellants in liquid form.
A hybrid rocket is the rocket with a rocket motor that uses propellants in two different states of matter; one liquid or gas and one solid.
R. W. Michel has written: 'Combustion performance and heat transfer characterization of LOX/hydrocarbon type propellants' -- subject(s): Space shuttles, Liquid oxygen, Oxygen-hydrocarbon rocket engines, Cryogenic rocket propellants
A rocket hasn't a chemical equation; for a detailed discussion about propellants see the link below.
Diane L. Linne has written: 'Technical prospects for utilizing extraterrestrial propellants for space exploration' -- subject(s): Auxiliary power supply, Space vehicles 'Carbon monoxide and oxygen combustion experiments' -- subject(s): Liquid propellant rocket engines, Propellant combustion, Liquid oxygen, Carbon monoxide, Propulsion system performance, Spacecraft propulsion, Liquid rocket propellants 'Performance and heat transfer characteristics of a carbon monoxide/oxygen rocket engine' -- subject(s): Fuel, Space vehicles, Propulsion systems, Rockets (Aeronautics)
Most commonly this might be aluminum. Others such as beryllium may be used. For more details please see the wikipedia articles about rocket propellants and solid fuel rockets.
Some books about rockets include "Ignition!: An Informal History of Liquid Rocket Propellants" by John D. Clark, "Rocket Boys" by Homer Hickam, and "SpaceX: Making Humans a Multiplanetary Species" by Martin Giles.
The fuselage of a rocket is the main part of the rocket :)
The two main types of rocket engines are Solid fuel rocket engines and Liquid fuel rocket engines.
Bryce Avary was the main singer in Rocket Summer.
Solid rocket propellants have the highest impulse densities typically 17 lbm-sec/in^3 or greater. Bi-propellant liquid rocket propellants such as Liquid Oxygen/Kerosene also have high density impulse, typically 12 lbm-sec/in^3 while Liquid Oxygen/Liquid Hydrogen have low density impulse below 6 lbm-sec/in^3.