Published December 1, 2018 | Version v1
Journal article

Effect of catalysts on the burning rate of phase stabilized ammonium nitrate based composite propellants

  • 1. Space Engineering Rocketry - BIT Mesra (India)

Description

The Ammonium Nitrate based composite propellants are widely used in the applications of tactical missiles and explosives due to its least toxicity and smokeless combustion. The main disadvantage of ammonium nitrate based propellants is its poor burning rate. Hence, it is required to enhance its burning rate for attaining a better performance. One of the several methods of upgrade the burning rate of composite solid propellants is the addition of catalysts to the propellant. The present study aims to investigate the effect of addition of transition metal oxides as the catalysts to the phase-stabilized ammonium nitrate based composite solid propellants and to study its thermal decomposition characteristics. (paper)

Availability note (English)

Available from http://dx.doi.org/10.1088/1757-899X/455/1/012022

Additional details

Publishing Information

Journal Title
IOP Conference Series. Materials Science and Engineering (Online)
Journal Volume
455
Journal Issue
1
Journal Page Range
[8 p.]
ISSN
1757-899X

Conference

Title
2. International Conference on Advancements in Aeromechanical Materials for Manufacturing
Dates
13-14 Jul 2018
Place
Telangana (India)

INIS

Country of Publication
United Kingdom
Country of Input or Organization
International Atomic Energy Agency (IAEA)
INIS RN
52102164
Subject category
S36: MATERIALS SCIENCE; S42: ENGINEERING;
Resource subtype / Literary indicator
Conference
Descriptors DEI
AMMONIUM NITRATES; FUELS; OXIDES; PERFORMANCE; PYROLYSIS; SOLIDS; TOXICITY; TRANSITION ELEMENTS
Descriptors DEC
AMMONIUM COMPOUNDS; CHALCOGENIDES; CHEMICAL REACTIONS; DECOMPOSITION; ELEMENTS; METALS; NITRATES; NITROGEN COMPOUNDS; OXYGEN COMPOUNDS; THERMOCHEMICAL PROCESSES