No, like other metals it is a reducer.
Yes, ammonium nitrate is an oxidizer. It can release oxygen when heated, making it a potential source of oxygen for combustion reactions.
Whether a chlorine compound is a Class 2 or Class 3 oxidizer is dependent on the compound and composition. Refer to the NFPA document in the related link for various chlorine compounds and their Hazardous Class rating.
No, alcohol is not an oxidizer itself. However, it can be easily oxidized when it comes into contact with certain substances or processes, leading to the formation of aldehydes or carboxylic acids.
Liquid fluorine is highly reactive, volatile, and dangerous to handle, making it challenging to use as an oxidizer in rocket propulsion systems. Its extreme reactivity with virtually all materials, including metals, poses significant safety risks and technical challenges that outweigh its benefits as an oxidizer. Additionally, alternative oxidizers like liquid oxygen are more widely used due to their proven reliability, storability, and compatibility with conventional materials.
The compound name of Hg2SO4 is mercury(I) sulfate.
UVA acts primarly as the oxidizer
Oxidizer - album - was created in 2004.
An oxidiser, or an oxidising agent. Spelled with a 'z' if you're American.
Clorox bleach is an oxidizer because it tends to cause other substances to lose electrons and undergo oxidation reactions.
Oxidizer
Yes, "Baquashock", "Baquacil Shock", and "Baquacil Shock and Oxidizer" are all synonymous. Baquacil has been changing the names through the evolution but it's the same product. Most companies are now selling it as "Oxidizer (Shock)" - http://www.backyardexpress.com/baquaspa-oxidizer-shock.html
No, it is a reducing agent
oxidizer
No, the fuels used were:boosters - hydrazine (fuel) and dinitrogen tetroxide (oxidizer)first stage - hydrazine (fuel) and dinitrogen tetroxide (oxidizer)second stage - hydrazine (fuel) and dinitrogen tetroxide (oxidizer)
Liquid oxygen (LOX) is commonly used as a liquid oxidizer in rocket engines due to its high oxidizing potential and high density. Hydrogen peroxide is another liquid oxidizer used in some rocket engines and propulsion systems. Nitric acid is also used as a liquid oxidizer in certain applications.
The Redstone rocket was fueled by a mixture of 25% H20 and 75% ethanol, and used liquid oxygen as the oxidizer. Redstone carried 19,000 lbs of fuel and 25,000 of oxidizer. Steam to drive the fuel and oxidizer pumps was produced by the decomposition of hydrogen peroxide (790 lbs of this were carried by Redstone).
A solid rocket engine uses a fuel and an oxidizer. The oxidizer when burned delivers oxygen to the fuel so that it can burn. Most rockets use oxidizers because when the rocket burns it uses so much oxygen that they need a readily available supply.