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FirePhysChem is a peer-reviewed journal published by Elsevier, covering Energetic Materials and Combustion, Rocket and propulsion systems research, Thermal and Kinetic Analysis.
| Publisher | Elsevier |
|---|---|
| Reference style | Numbered (Elsevier) Numbered — [1], [2] in the text [1] A. Smith, B. Jones, C. Lee, A representative article title, FirePhysChem 12 (2023) 45–58.
Formats any DOI in FirePhysChem style. No sign-up. |
| Publishes research in | Energetic Materials and Combustion Rocket and propulsion systems research Thermal and Kinetic Analysis Combustion and Detonation Processes Chemical Thermodynamics and Molecular Structure |
| ISSN | 2667-1344 |
| Citation impact (2-yr) | 2.91 |
| h-index | 25 |
| i10-index | 103 |
| Total citations | 2,848 |
| Open access | Yes |
| Top institutions publishing here | Nanjing University of Science and Technology |
| Journal website | www.sciencedirect.com |
| You get | A submission-ready PDF and the editable LaTeX source — ready to submit. |
Citations each year’s papers have accumulated so far — the most recent years are still building up.
Energetic material is a very essential company of compounds, widely used in various fields, primarily in the military industry and space technologies. These compounds are unique in that they are capable of instantly decomposing to release enormous energy. The chemical diversity of energetic organic compounds is constantly increasing through the combination of various high-nitrogen frameworks…
The applications of thermal analysis technologies in evaluating the thermal properties of energetic materials in China are briefly reviewed. They are widely adopted in the determination of thermal stability, compatibility and thermophysical constants, as well as the study of thermal decomposition kinetics, mechanism and interaction. In addition, some researches of development or innovation, including the…
This paper presents the status of developments worldwide regarding use of hybrid rocket motors for space transportation. Historical roots are presented and reasons for revisiting hybrid technology after a few decades of limited interest are examined. Modern developments in sounding rockets, reusable suborbital systems and launch vehicles are discussed with particular focus on propellant technology.…
This paper discusses the potential use of hydrogen peroxide as oxidizer for solid rocket propulsion. While hydrogen peroxide is a liquid in normal conditions, it may be used in solid rocket motor grains. Use of hydrogen peroxide of HTP class (High Test Peroxide) is proposed. It has been known for many decades but its utilization…
There is a need for dense energetic oxidizers whose composition is restricted to carbon, hydrogen, nitrogen and oxygen atoms as chlorine-free alternative to current oxidizers of energetic materials such as explosives, propellants and pyrotechnics. High nitrogen heterocyclic frameworks containing trinitromethyl units are an attractive and increasingly important class of oxygen-rich compounds. Herein, for the first…
