Published December 1, 2018
| Version v1
Journal article
Effect of catalysts on the burning rate of phase stabilized ammonium nitrate based composite propellants
Creators
- 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/455/1/012022Additional details
Identifiers
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