Most Cited Articles

Open access

ISSN: 2667-1344

Thermal decomposition behavior and kinetic study of nitrocellulose in presence of ternary nanothermites with different oxidizers

Research progress of nitrate ester binders

Elaboration, spectroscopic characterization, and study of the thermal decomposition process of energetic composites based on ammonium perchlorate and dual-biopolymers

Low rank coal for fuel production via microwave-assisted pyrolysis: A review

A review on solid propellant micro-thruster array based on MEMS technology

HTPB propellant binder supplemented with nitro potato starch: Formulation, characterization, and thermal decomposition behavior

Synthesis and oxidation chemistry of highly energetic boron/aluminum/magnesium composites

Synthesis of a new oxa-type cage-like energetic compound 4,4,8,8-tetranitro-2-oxaadamantane

Continuous flow resonance acoustic mixing technology: a novel and efficient strategy for preparation of nano energetic materials

Enhancement of the energetic performance of solid fuels with metal-fluoropolymer additives

Pyrolysis mechanism and evolved gas analysis of a promising energetic carbamate-functionalized microcrystalline cellulose nitrate

Mechanical and thermophysical properties of energetic crystals: evaluation methods and recent achievements

A short review of challenges and prospects of boron-laden solid fuels for ramjet applications

3D printed different polymer fuel grains for hybrid rocket engine

Towards to some published misconceptions about TNT and ɛ-CL20

Combustion features of dispersed aluminum and boron in high-energy composition

Boron-loaded gel fuel as potential fuel for ramjet and scramjet engines- recent advancements

Energetic materials for propulsion applications

Morphology and properties of CL-20/MTNP cocrystal prepared via facile spray drying

Effect of Carbon Nanotubes (CNTs) on the performance of Solid Rocket Propellants (SRPs): A short review

Highly energetic formulations of boron and polytetrafluoroethylene for improved ignition and oxidative heat release

Effects of RDX and HMX on the thermal stability properties of modified double-base propellants

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