15588-62-2 Usage
Description
Hydroxyl ammonium perchlorate (HAP), with the chemical formula NH3OHClO4, is a white, crystalline solid that exhibits high solubility in water. It is recognized for its high energy release and stability, making it a valuable compound in various applications.
Uses
Used in Aerospace Industry:
Hydroxyl ammonium perchlorate is used as a rocket propellant for its high energy release, which is crucial for propelling rockets and spacecraft. Its stability ensures reliable performance in space missions.
Used in Propellant Production:
In the manufacturing sector, HAP is utilized in the production of solid rocket propellants, contributing to the development of efficient and potent propulsion systems for various applications.
Used as an Oxidizer:
HAP serves as an oxidizer in industrial and laboratory settings, supporting chemical reactions that require an oxidizing agent for their completion.
Used in Pharmaceutical Research:
Although still under investigation, hydroxyl ammonium perchlorate has been studied for its potential use in pharmaceuticals, indicating a possible role in the development of new medications.
Used in Fuel Cell Technology:
HAP is also being explored as a fuel cell electrolyte, which could enhance the efficiency and performance of fuel cells in energy production applications.
Check Digit Verification of cas no
The CAS Registry Mumber 15588-62-2 includes 8 digits separated into 3 groups by hyphens. The first part of the number,starting from the left, has 5 digits, 1,5,5,8 and 8 respectively; the second part has 2 digits, 6 and 2 respectively.
Calculate Digit Verification of CAS Registry Number 15588-62:
(7*1)+(6*5)+(5*5)+(4*8)+(3*8)+(2*6)+(1*2)=132
132 % 10 = 2
So 15588-62-2 is a valid CAS Registry Number.
InChI:InChI=1/ClHO4.H3NO/c2-1(3,4)5;1-2/h(H,2,3,4,5);2H,1H2
15588-62-2Relevant articles and documents
Some properties of cocrystallizates of hydroxylammonium and hydrazonium perchlorates
Makhonina,Lempert,Nechiporenko
, p. 167 - 170 (2008/10/08)
Anhydrous mixed perchlorates of hydroxylamine and hydrazine were synthesized by coprecipitation from aqueous solutions. Their melting temperatures were determined, the moisture effect on the salt phase states was studied, and thermal analysis of the compounds was performed. The thermal stability of the salts in the temperature range 60 to 80°C and their compatibility with the components of composite propellants were investigated. Copyright
