ScholarLens Back to search
2002•Journal of Solid Rocket TechnologyRequires access

Study on the thermal decomposition behavior of RDX/AP/HTPB propellant

Cui-Mei Yin

Open publisher page 4 citations

Abstract

The thermal decomposition behavior of RDX/AP/HTPB propellant was studied by pressure differential scanning calorimetry(PDSC).The results show that the thermal decomposition behavior of RDX/AP/HTPB propellant is affected by the change of the propellant component,which mainly represents on the point where the decomposition peak width of RDX contained in RDX/AP/HTPB propellant becomes wider and the thermal decomposition of AP is enhanced.The decomposition of RDX is inhibited while the thermal decomposition of AP is strengthened after Al powder is added into the propellant.

About this research paper

What this paper is about

The thermal decomposition behavior of RDX/AP/HTPB propellant was studied by pressure differential scanning calorimetry(PDSC).The results show that the thermal decomposition behavior of RDX/AP/HTPB propellant is affected by the change of the propellant component,which mainly represents on the point where the decomposition peak width of RDX contained in RDX/AP/HTPB propellant becomes wider and the thermal decomposition of AP is enhanced.The decomposition of RDX is inhibited while the thermal decomposition of AP is strengthened after Al powder is added into the propellant.

Why it matters

OpenAlex reports 4 citations for this work. Citation counts describe recorded attention and do not establish research quality.

Key contribution

A contribution statement is not available in the OpenAlex record.

Method / approach

Method details are not available in the OpenAlex metadata.

Main findings

Findings are not separately available in the OpenAlex metadata.

Limitations

Limitations are not available in the OpenAlex metadata.

Applications

Application details are not available in the OpenAlex metadata.

Available abstract

The thermal decomposition behavior of RDX/AP/HTPB propellant was studied by pressure differential scanning calorimetry(PDSC).The results show that the thermal decomposition behavior of RDX/AP/HTPB propellant is affected by the change of the propellant component,which mainly represents on the point where the decomposition peak width of RDX contained in RDX/AP/HTPB propellant becomes wider and the thermal decomposition of AP is enhanced.The decomposition of RDX is inhibited while the thermal decomposition of AP is strengthened after Al powder is added into the propellant.

Key concepts: Propellant, Thermal decomposition, Decomposition, Differential scanning calorimetry, Materials science, Energetic material, Composite material, Thermal

Related papers

Related paper 1Related paper 2Related paper 3
Back to paper searchBrowse research topicsOriginal source
Study on the thermal decomposition behavior of RDX/AP/HTPB propellant — Research Paper | ScholarLens