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Journal ArticleDOI

Mass spectrometric study of the thermal decomposition of ammonium perchlorate

G. A. Heath, +1 more
- 01 Jan 1964 - 
- Vol. 60, pp 1783-1791
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This article is published in Transactions of The Faraday Society.The article was published on 1964-01-01. It has received 51 citations till now. The article focuses on the topics: Ammonium perchlorate & Thermal decomposition.

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Journal ArticleDOI

Mass‐Spectrometric Study of the Thermal Decomposition of Ammonium Perchlorate

TL;DR: In this paper, the thermal decomposition of 14NH4ClO4, 15NH4CLO4 and deuterated ammonium perchlorate has been investigated mass spectrometrically.
Journal ArticleDOI

The thermochemistry of explosives: a review

TL;DR: The application of traditional thermal analysis techniques as well as specialized thermal techniques to the characterization of explosives is reviewed in this paper, where general references are general references, pressure measurement techniques, gaseous product analysis, DTA, DSC, TG, combined TG-DTA, and miscellaneous techniques as applied to a variety of explosive materials.
Journal ArticleDOI

Layered magnesium diboride and its derivatives as potential catalytic and energetic additives for tuning the exothermicity of ammonium perchlorate

TL;DR: In this article, the effect of layered magnesium diboride (LMDB) and its micro and nano derivatives as catalytic and energetic additives towards the thermal decomposition of ammonium perchlorate (AP) was studied.
Journal ArticleDOI

The Thermal Decomposition of Ammonium Perchlorate-Aluminum Propellants in Presence of Metallic Zinc Particles

TL;DR: In this paper, the thermal decomposition of ammonium perchlorate (AP) with Al and Zn metallic particles was studied at different heating rates in dry air atmosphere and the combustion behavior of AP/Al/Zn propellant was evaluated.
Book ChapterDOI

Ignition and Combustion of Solid Rocket Propellants

TL;DR: In this paper, a model of the combustion mechanism of double-base propellants is presented, which can be visually observed on the surface of the propellant surface, where the initial exothermic decomposition reactions can be analyzed as a single reaction occurring at the surface.
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